PROG MTTO PC12-45 - copia
81 Pages • 21,603 Words • PDF • 2 MB
Uploaded at 2021-09-24 16:32
This document was submitted by our user and they confirm that they have the consent to share it. Assuming that you are writer or own the copyright of this document, report to us by using this DMCA report button.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45
HOJA DE PRESENTACIÓN
PROGRAMA DE MANTENIMIENTO
AERONAVE: PILATUS PC-12/45
DESARROLLADO CONFORME A LA ISSUE No. 001 REVISIÓN No. 28 de 31/05/2014 DEL “AIRCRAFT MAINTENANCE MANUAL” DEL FABRICANTE, SECCIÓN 4 Y 5
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.1
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45
Índice HOJA DE PRESENTACIÓN .......................................................................................... A2-1 LISTA DE PÁGINAS EFECTIVAS ................................................................................. A2-3 HOJA PARA EL REGISTRO Y CONTROL DE REVISIONES. ..................................... A2-4 INTRODUCCION ............................................................................................................ A2-5 Chapter 04 - AIRWORTHINESS LIMITATIONS ............................................................ A2-6 STRUCTURAL AND COMPONENT LIMITATIONS - AIRWORTHINESS LIMITATIONS .................................................................................................................................... A2-6 Structural Limitations ........................................................................................... A2-6 Component Limitations ........................................................................................ A2-6 Miscellaneous Limitations .................................................................................... A2-7 Component Life ..................................................................................................... A2-8 Inspection Program ............................................................................................... A2-8 Chapter 05 - SCHEDULED/UNSCHEDULED MAINTENANCE SCHEDULED/UNSCHEDULED MAINTENANCE MASTER MAINTENANCE PLAN GENERAL .................................................................................................................... A2-13 100 HOUR INSPECTION - SCHEDULED INSPECTIONS ....................................... A2-42 ANNUAL INSPECTION - SCHEDULED INSPECTIONS ......................................... A2-49 OVERHAUL AND REPLACEMENT SCHEDULE - SCHEDULED INSPECTIONS ..... A2-59 TIME LIMITED INSPECTION REQUIREMENTS - SCHEDULED INSPECTIONS ...... A2-61 INSPECTION ENGINES Y PROPELLER .................................................................... A2-69
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.2
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45
LISTA DE PÁGINAS EFECTIVAS La siguiente es la lista de páginas efectivas del Programa de Mantenimiento aplicable a las aeronaves Marca Pilatus Modelo PC12/45 operada por Pilatus PC12 Center de Mexico, S.A. DE C.V. el poseedor del programa tendrá la obligación de mantenerlo actualizado, para ello revisaran físicamente que el número de páginas coincida con la lista. PAGINA
REVISION
FECHA
PAG. A2-1 PAG. A2-2 PAG. A2-3 PAG. A2-4 PAG. A2-5 PAG. A2-6 PAG. A2-7 PAG. A2-8 PAG. A2-9 PAG. A2-10 PAG. A2-11 PAG. A2-12 PAG. A2-13 PAG. A2-14 PAG. A2-15 PAG. A2-16 PAG. A2-17 PAG. A2-18 PAG. A2-19 PAG. A2-20 PAG. A2-21 PAG. A2-22 PAG. A2-23 PAG. A2-24 PAG. A2-25 PAG. A2-26 PAG. A2-27 PAG. A2-28 PAG. A2-29 PAG. A2-30 PAG. A2-31 PAG. A2-32 PAG. A2-33 PAG. A2-34 PAG. A2-35 PAG. A2-36 PAG. A2-37 PAG. A2-38 PAG. A2-39 PAG. A2-40
ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL
16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAGINA PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG.
A2-41 A2-42 A2-43 A2-44 A2-45 A2-46 A2-47 A2-48 A2-49 A2-50 A2-51 A2-52 A2-53 A2-54 A2-55 A2-56 A2-57 A2-58 A2-59 A2-60 A2-61 A2-62 A2-63 A2-64 A2-65 A2-66 A2-67 A2-68 A2-69 A2-70 A2-71 A2-72 A2-73 A2-74 A2-75 A2-76 A2-77 A2-78 A2-79 A2-80
REVISION
FECHA
16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014
16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014
PAG: A2.3
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45
HOJA PARA EL REGISTRO Y CONTROL DE REVISIONES. REGISTRO Y CONTROL DE REVISIONES
No. DE REVISIÓN
FECHA
FECHA DE INSERCIÓN
INICIALES
ORIGINAL 1 2 3 4 5 6 7 8 9 10
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.4
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45
INTRODUCCION El programa de mantenimiento para la aeronave Pilatus PC-12/45 indicado por el fabricante presenta dos opciones de aplicación, de acuerdo al número de horas de vuelo acumuladas durante un año, si se vuela un alto número de horas durante el año, se recomienda la utilización del programa de inspección progresiva, el cual se divide en 28 “Work Cards”, seis fases y las inspecciones “mini”. Para el caso especifico de las aeronaves de Pilatus PC-12 Center de México, el promedio de horas anuales voladas es bajo, por lo que se opto por el programa de mantenimiento estándar, que consta de una inspección a las 100 horas y una inspección anual. En ambos casos, el programa de mantenimiento es complementado con el control de componentes limitados por tiempo de vida y las inspecciones especiales. TOLERANCIAS PERMISIBLES. 1. Intervalos basados en horas de vuelo: a. Intervalos de 100 horas de vuelo o menos + 10 horas de vuelo. b. Intervalos de más de 100 horas de vuelo + 10 % pero no más de 50 horas de vuelo. 2. Intervalos basados en tiempo calendario a. Intervalos de 1año o menos + 10 % pero no más de un mes. b. Intervalos de más de 1 año + 10 % pero no más de 6 meses. 3. Intervalos basados en ciclos a. Menos de 500 ciclos: + 10 % pero no más de 25 ciclos. b. Más de 500 ciclos: + 10 % pero no más de 500 ciclos. La utilización de las extensiones aquí indicadas no implica que se recorran los tiempos de aplicación de las siguientes inspecciones, sino que se utilizarán los tiempos originales sin contar la extensión aplicada. Estas tolerancias podrán ser aplicadas conforme lo señalado solamente PREVIA AUTORIZACIÓN POR PARTE DE LA DGAC.
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.5
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45
Chapter 04 - AIRWORTHINESS LIMITATIONS
STRUCTURAL AND COMPONENT LIMITATIONS - AIRWORTHINESS LIMITATIONS
Structural Limitations STRUCTURE
LIFE
Fuselage and associated structure
Pre SB 04-009 20,000 flying hours or 27,000 landings, whichever comes first Post SB 04-009 25,000 flying hours or 30,000 landings, whichever comes first Wing structure Pre SB 04-009 20,000 flying hours or 27,000 landings, whichever comes first Post SB 04-009 25,000 flying hours or 30,000 landings, whichever comes first Tail structure Pre SB 04-009 20,000 flying hours or 27,000 landings, whichever comes first Post SB 04-009 25,000 flying hours or 30,000 landings, whichever comes first Beyond 25,000 flying hours or 30,000 landings (whichever comes first) refer to the Supplemental Structural Inspection Document (SSID) at Para 5 and 12-A-05-20-30-00A-280A-A for supplemental structural inspections.
Component Limitations COMPONENT
LIFE
Engine rotor components Engine mounting frame
P&WC SB 14002 (latest revision) Pre SB 04-009 20,000 flying hours or 27,000 landings, whichever comes first Post SB 04-009 25,000 flying hours or 30,000 landings, whichever comes first Beyond 25,000 flying hours or 30,000 landings (whichever comes first) refer to the Supplemental Structural Inspection Document (SSID) at Para 5 and 12-A-05-20-30-00A-280A-A for supplemental structural inspections. Engine mounting frame, replace all bolts, 11,000 flying hours washers and nuts Pitch trim actuator 20,000 flying hours or 27,000 landings, whichever comes first Flap actuator (Part No. 978.73.20.307, 308 20,000 flying hours or 27,000 landings, whichever comes first and 309) (black anodized) Fire extinguisher 10 years (elapsed). See Note 1 below. REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.6
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 COMPONENT
LIFE
Oxygen bottle 15 years (elapsed) NLG drag link right part (Part No. 4,000 landings 532.20.12.140) (Pre SB 32-014) Cargo door lower lug fittings (Qty 3) 13,000 flying hours or 17,000 landings, whichever comes first Pitch trim actuator attachment parts, fail safe plates and their attachment parts (IPC 12-20-00-07). Refer to AMM 12-A-27-40-02- 10,000 flying hours 00A-920A-A for fail safe plate removal/installation. Nose landing gear torque tube (P/N 532.50.- 11,000 flying hours or 15,000 landings or 10 years installed, 12.047) whichever comes first. Note 1: Fire extinguishers that are 10 years or older must be replaced by 30 June 2013.
Miscellaneous Limitations COMPONENT
LIMITATION
PROCEDURE
Cockpit outer side, DV Windows and cabin windows Cockpit inner and outer side, DV windows and cabin windows Windshield LH and RH
If cracked or stress crazing can be felt
Replace
If chipped, cracked (only for inner side windows), scratched, bubbles or delaminated If cracked in inner lamination If cracked in outer lamination
Refer to AMM 12-A-56-00-00-00A-313A-A for limitations
Horizontal stabilizer trim
Every 3,000 flying hours or at Annual Inspection, whichever comes first
NLG drag link right part (P/N 532.20.12.140)
Initially 2,000 flying hours or 2,500 landings (installed) whichever comes first, then every 300 flying hours or 400 landings, whichever comes first. Refer to AVOX Service Information Letter SIL-35-114 latest revision (www.avoxsys.com).
Oxygen bottle
Pitch trim actuator (Part No. 978.73.14.202 and 978.73.14.203) Wing Main Spar Fastener REVISIÓN: ORIGINAL
Replace Only unpressurized flight is permitted up to the next scheduled inspection providing it does not cause visual problems Functional test of Trim Runaway Aural Warning System (FAA CMR) in accordance with AMM 12A-27-40-00-00A-903A-A Inspection/check (refer to AMM 12-A-32-20-0600A-313A-A). Hydrostatic test. Refer to AVOX Service Information Letter SIL-35-114 latest revision (www. avoxsys.com).
5,000 flying hours or 5 years (installed) whichever comes First
Overhaul
Threshold 16000 wing flying hours or
Eddy current inspection, AMM 12-A-57-20-10-
FECHA: 16-JUNIO-2014
PAG: A2.7
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 COMPONENT Holes Strap Rib 6
LIMITATION
PROCEDURE
22500 wing landings, whichever comes first. All wings with no landing records must apply a calculated applicable landings equal to 2 x flying hours. See Notes 1 and 2 below.
00A-353D-A No cracks are permitted. If you find cracks contact Pilatus Aircraft for advice.
Note 1 The inspection is applicable to all aircraft except MSN 170, 222, 233, 234, 237, 240, 244, 250 and 324 which have performed the inspection as part of a fleet leader inspection survey and aircraft that have performed Service Bulletin 04-009 Revision 1 or later Note 2 Wings with more than 15500 flying hours or 22000 landings, whichever comes first, must perform the inspection within the next 500 flying hours or 500 landings, whichever comes first
Component Life TASK NO.
27-50/414 55-10/415 32-20/416 32-30/417 29-10/418
COMPONENT
LIFE (WHICHEVER COMES FIRST) FLYING LANDINGS HOURS
Flaps - Life Limit (discard) Horizontal Stabilizer - Life Limit (discard) NLG Drag Link - Life Limit (discard) MLG Actuator - Life Limit (discard) Nitrogen accumulator - Life Limit (discard)
25,000 25,000 25,000 25,000 25,000
30,000 30,000 30,000 30,000 30,000
Inspection Program TASK NO.
32-10/345 32-10/346 32-10/347
INSPECTION/REFERENCE
Main landing gear – Overhaul CMM 02099 Inspection kit P/N 500.60.12.027 MLG Yoke fitting lugs - Eddy Current Inspection CMM 02099 MLG Trailing Link - Eddy Current Inspection
REVISIÓN: ORIGINAL
Threshold (whichever comes first) flying landings hours
LIFE (WHICHEVER COMES FIRST) flying landings Years hours
25,000
30,000
8,300
10,000
25,000
30,000
8,300
10,000
25,000
30,000
8,300
10,000
FECHA: 16-JUNIO-2014
6
PAG: A2.8
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
52-10/348
52-20/349 52-30/350 53-00/351
53-00/352
53-00/353
53-00/354
53-00/355 53-00/356
53-00/357
53-00/358
53-00/359
53-00/360
53-00/361
55-20/362 27-30/363
27-30/364 27-30/365
INSPECTION/REFERENCE
CMM 02099 Passenger/crew door - Examine all structural elements AMM 12-A-52-10-00-00A-310A-A Emergency door - Examine all structural elements AMM 12-A-52-20-00-00A-310A-A Cargo door - Examine all structural elements AMM 12-A-52-30-00-00A-310A-A Upper Longerons Frame 10 - Eddy Current Inspection AMM 12-A-53-10-06-01A-353A-A Inspection kit P/N 500.60.12.032 Fuselage Frames 10 to 16 - Examine all structural elements AMM 12-A-53-10-00-00A-310A-A Inspection kit P/N 500.60.12.033 Fuselage Frames 16 to 36 - Examine all structural elements AMM 12-A-53-20-00-00A-310A-A Inspection kit P/N 500.60.12.041 Fuselage Frames 36 to 43 - Examine all structural elements AMM 12-A-53-30-00-00A-310A-A Antenna Structure - Examine AMM 12-A-53-00-00-00A-310A-A Antenna - Bottom fuselage skin - Eddy Current Inspection AMM 12-A-53-00-00-00A-353A-A Antenna - Upper fuselage skin - Eddy Current Inspection AMM 12-A-53-00-00-00A-353A-A Upper Flange Carry Through Frames 21 and 24 Examine AMM 12-A-53-20-02-00A-310A-A Inspection kit P/N 500.50.12.327 Frames 21 and 24 Wing Attachments - Eddy Current Inspection AMM 12-A-53-20-02-00A-353A-A Frames 21 and 24 Side Frame Attachments - Eddy Current Inspection AMM 12-A-53-20-02-00A-353A-A Frames 41 and 43 Stabilizer Attachment - Eddy Current Inspection AMM 12-A-53-30-02-00A-353A-A or AMM 12-A-55-30-03-00A-353A-A Elevator - Examine AMM 12-A-55-20-00-00A-310A-A Elevator - Control System - Examine AMM 12-A-27-30-00-00A-310A-A Inspection kit P/N 500.50.12.319 Elevator Control Rods - Eddy Current Inspection AMM 12-A-27-00-01-00A-353A-A Elevator Control Rods - Magnetic Particle Inspection
REVISIÓN: ORIGINAL
Threshold (whichever comes first) flying landings hours
LIFE (WHICHEVER COMES FIRST) flying landings Years hours
32,500
42,000
12,500
15,000
6
32,500
42,000
12,500
15,000
6
32,500
42,000
12,500
15,000
6
25,000
30,000
12,500
15,000
32,500
42,000
12,500
15,000
6
32,500
42,000
12,500
15,000
6
32,500
42,000
12,500
15,000
6
32,500
42,000
12,500
15,000
6
28,300
37,000
8,300
10,000
32,500
42,000
12,500
15,000
30,000
39,000
10,000
12,000
30,000
39,000
10,000
12,000
30,000
39,000
10,000
12,000
32,500
42,000
12,500
15,000
32,500
42,000
12,500
15,000
6
32,500
42,000
12,500
15,000
6
32,500
42,000
12,500
15,000
32,500
42,000
12,500
15,000
FECHA: 16-JUNIO-2014
6
PAG: A2.9
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
27-30/366 55-20/367 55-20/368 55-30/369
55-30/370
55-30/371
55-30/372
55-40/373 27-20/374
27-20/375 27-20/376 55-40-377 56-11/378
57-00/379
57-00/380
57-00/382
57-00/383
INSPECTION/REFERENCE
AMM 12-A-27-00-01-00A-352A-A Elevator Control Lever - Eddy Current Inspection AMM 12-A-27-30-05-00A-353A-A Elevator Drive Lever - Eddy Current Inspection AMM 12-A-55-20-01-00A-353A-A Elevator Hinges - Eddy Current Inspection AMM 12-A-55-20-01-00A-353A-A Vertical Stabilizer - Examine AMM 12-A-55-30-00-00A-310A-A Inspection kit P/N 500.50.12.325 Vertical Stabilizer Main and Rear Spar Attachment to Fuselage - Eddy Current Inspection AMM 12-A-53-30-02-00A-353A-A or AMM 12-A-55-30-03-00A-353A-A Vertical Stabilizer Main Attachment to Horizontal Stabilizer - Eddy Current Inspection AMM 12-A-55-00-00-00A-353A-A Vertical Stabilizer Pitch Trim Actuator Fitting and Attachment - Eddy Current Inspection AMM 12-A-55-30-02-00A-353A-A Rudder - Examine AMM 12-A-55-40-00-00A-310A-A Rudder Control System - Examine AMM 12-A-27-20-00-00A-310A-A Inspection kit P/N 500.50.12.318 Rudder Bellcranks - Eddy Current Inspection AMM 12-A-27-20-04-00A-353A-A Rudder Cable Quadrant Shear Spigot - Examine AMM 12-A-27-20-05-00A-310A-A Rudder Hinges - Eddy Current Inspection AMM 12-A-55-40-05-00A-353A-A Windshield LH and RH and Cockpit Side Windows Examine with windshield and side windows removed AMM 12-A-56-11-01-00A-310A-A and AMM 12-A-56-11-02-00A-310A-A and AMM 12-A-53-10-16-00A-310A-A Inspection kit P/N 500.50.12.326 Wing - Examine all structural elements Rib 1 to Rib 20 AMM 12-A-57-00-00-00A-310A-A Wing Main and Rear Spar to Fuselage Attachment Eddy Current Inspection AMM 12-A-57-00-03-00A-353A-A and AMM 12-A-57-00-03-01A-353A-A Inspection kit P/N 500.60.12.004 wing attachment Inspection kit P/N 500.60.12.007 double bush Wing Rear Spar at Rib 8 Flap Arm Attachment - Eddy Current Inspection AMM 12-A-57-20-10-00A-353C-A Wing Main Spar Fastener Holes Rib 1 thru Rib 6 -
REVISIÓN: ORIGINAL
Threshold (whichever comes first) flying landings hours
LIFE (WHICHEVER COMES FIRST) flying landings Years hours
32,500
42,000
12,500
15,000
32,500
42,000
12,500
15,000
32,500
42,000
12,500
15,000
32,500
42,000
12,500
15,000
32,500
42,000
12,500
15,000
32,500
42,000
12,500
15,000
32,500
42,000
12,500
15,000
32,500
42,000
12,500
15,000
6
32,500
42,000
12,500
15,000
6
32,500
42,000
12,500
15,000
32,500
42,000
12,500
15,000
32,500
42,000
12,500
15,000
32,500
42,000
12,500
15,000
6
30,000
39,000
10,000
12,000
6
30,000
39,000
10,000
12,000
25,000
30,000
12,500
15,000
25,000
30,000
3,300
4,000
FECHA: 16-JUNIO-2014
6
6
PAG: A2.10
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
57-00/384
57-00/385
27-50/386
27-50/387
27-50/388
27-50/389
27-50/390
27-50-391
27-50/392
57-60/393 27-10/394
27-10/395
INSPECTION/REFERENCE
Eddy Current Inspection AMM 12-A-57-20-10-00A-353A-A Inspection kit P/N 500.60.12.030 or Inspection kit P/N 500.60.12.020 Wing Main Spar Fastener Holes Strap Rib 6 - Eddy Current Inspection AMM 12-A-57-20-05-00A-353A-A Inspection kit P/N 500.60.12.031 or Inspection kit P/N 500.60.12.043 Wing Rear Spar Fastener Holes Rib 2 thru Rib 3 Eddy Current Inspection AMM 12-A-57-20-10-00A-353B-A Flap Mechanism - Examine AMM 12-A-27-51-00-00A-310A-A Inspection kit P/N 500.60.12.021 Inspection kit P/N 500.60.12.022 Inspection kit P/N 500.60.12.023 Inspection kit P/N 500.60.12.024 Inspection kit P/N 500.60.12.025 Flap Drive Arm (not removed) - Eddy Current Inspection AMM 12-A-27-51-00-00A-353A-A Flap Drive Arm (removed) - Eddy Current Inspection AMM 12-A-27-51-01-00A-353A-A AMM 12-A-27-51-02-00A-353A-A AMM 12-A-27-51-03-00A-353A-A Flap Support Arm - Eddy Current Inspection AMM 12-A-27-51-01-00A-353A-A AMM 12-A-27-51-02-00A-353A-A AMM 12-A-27-51-03-00A-353A-A Flap Cove Rib FIttings - Eddy Current Inspection AMM 12-A-27-51-01-00A-353A-A AMM 12-A-27-51-02-00A-353A-A AMM 12-A-27-51-03-00A-353A-A Flap Aft Links - Eddy Current Inspection AMM 12-A-27-51-01-00A-353A-A AMM 12-A-27-51-02-00A-353A-A AMM 12-A-27-51-03-00A-353A-A Flap Bellcranks - Eddy Current Inspection AMM 12-A-27-51-01-00A-353A-A AMM 12-A-27-51-02-00A-353A-A AMM 12-A-27-51-03-00A-353A-A Aileron - Examine AMM 12-A-57-60-00-00A-310A-A Aileron Control System - Examine AMM 12-A-27-10-00-00A-310A-A Inspection kit P/N 500.50.12.314 Inspection kit P/N 500.50.12.315 Inspection kit P/N 500.50.12.316 Inspection kit P/N 500.60.12.015 (MSN 684 - 999) Inspection kit P/N 500.60.12.016 (MSN 684 -999) Aileron Cable Segment - Eddy Current Inspection AMM 12-A-27-10-09-00A-353A-A
REVISIÓN: ORIGINAL
Threshold (whichever comes first) flying landings hours
LIFE (WHICHEVER COMES FIRST) flying landings Years hours
25,000
30,000
3,300
4,000
25,000
30,000
12,500
15,000
30,000
39,000
10,000
12,000
25,000
30,000
2,500
3,000
30,000
39,000
10,000
12,000
30,000
39,000
10,000
12,000
30,000
39,000
10,000
12,000
30,000
39,000
10,000
12,000
30,000
39,000
10,000
12,000
32,500
42,000
12,500
15,000
6
32,500
42,000
12,500
15,000
6
32,500
42,000
12,500
15,000
FECHA: 16-JUNIO-2014
6
PAG: A2.11
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
27-10/396 27-10/397 27-10/398
27-30/400 71-00/401
INSPECTION/REFERENCE
Aileron Control Rods - Eddy Current Inspection AMM 12-A-27-00-01-00A-353A-A Aileron Control Rods - Magnetic Particle Inspection AMM 12-A-27-00-01-00A-352A-A Aileron Bellcranks - Eddy Current and Magnetic Particle Inspections AMM 12-A-27-10-08-00A-353A-A AMM 12-A-27-10-08-00A-353B-A AMM 12-A-27-10-08-00A-352B-A Aileron Hinge Points - Eddy Current Inspection AMM 12-A-57-60-06-00A-353A-A Engine Mount - Magnetic Particle Inspection AMM 12-A-71-00-05-00A-352A-A Inspection kit P/N 500.60.12.006
Threshold (whichever comes first) flying landings hours
LIFE (WHICHEVER COMES FIRST) flying landings Years hours
32,500
42,000
12,500
15,000
32,500
42,000
12,500
15,000
32,500
42,000
12,500
15,000
32,500
42,000
12,500
15,000
26,600
35,000
6,600
8,000
SUPPLEMENTAL STRUCTURAL Do these supplemental structural inspections to increase the life of the airframe above more than 25000 flying hours or 30000 landings:
TASK NO.
INSPECTION/REFERENCE
Threshold (whichever comes first) flying landings hours
LIFE (WHICHEVER COMES FIRST) flying landings Years hours
27-00/402
Bonding leads to all Flight Control Surfaces – Examine
32,500
42,000
12,500
15,000
6
32-20/403
NLG - Overhaul CMM 02100 Overhaul Kit P/N 500.60.12.029 NLG Steering Mechanism - Examine AMM 12-A-32-50-00-00A-310A-A Passenger/Crew Door Piano Hinge - Eddy Current Inspection AMM 12-A-52-00-01-00A-353A-A Passenger/Crew Door Skin - Eddy Current Inspection AMM 12-A-52-10-01-00A-353A-A Cargo Door Piano Hinge - Eddy Current Inspection AMM 12-A-52-30-00-01A-353A-A Cargo Door Skin - Eddy Current Inspection AMM 12-A-52-30-01-00A-353A-A Frame 40 - Eddy Current Inspection AMM 12-A-53-30-02-00A-353A-A Vertical Stabilizer Forward Attachment to Frame 40 Eddy Current Inspection AMM 12-A-55-30-03-00A-353A-A Rudder Trim Tab - Examine
25,000
30,000
8,300
10,000
6
32,500
42,000
8,300
10,000
6
32,500
42,000
12,500
15,000
25,000
30,000
12,500
15,000
32,500
42,000
12,500
15,000
25,000
30,000
12,500
15,000
32,500
42,000
12,500
15,000
32,500
42,000
12,500
15,000
32,500
42,000
12,500
15,000
32-50/404 52-10/405
52-10/406 52-30/407 52-30/408 53-00/419 55-30/420
55-40/410
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
6
6
6
PAG: A2.12
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
57-60/411
57-00/412 57-00/413
INSPECTION/REFERENCE
AMM 12-A-55-40-00-00A-310A-A Aileron Trim Tab - Examine AMM 12-A-57-60-04-00A-310A-A Inspection kit P/N 500.50.12.317 or Inspection kit P/N 500.60.12.039 and Inspection kit P/N 500.60.12.040 Wing Tips - Examine AMM 12-A-57-33-00-00A-310A-A Wing Skin around drain holes - Eddy Current Inspection AMM 12-A-57-20-01-00A-353A-A
Threshold (whichever comes first) flying landings hours
LIFE (WHICHEVER COMES FIRST) flying landings Years hours
32,500
42,000
12,500
15,000
6
32,500
42,000
12,500
15,000
6
25,000
30,000
2,500
3,000
Chapter 05 - SCHEDULED/UNSCHEDULED MAINTENANCE SCHEDULED/UNSCHEDULED MAINTENANCE MASTER MAINTENANCE PLAN - GENERAL The Master Maintenance Plan lists all maintenance tasks from the Airworthiness Limitations (AL) DM, time limits DM, 100 Hour inspection DM, annual inspection DM and the Progressive Inspection (PI). The tasks are listed in ATA chapter (given in the task number) order. The purpose of this Master Maintenance Plan is to provide the operator/maintainer a complete overview of the maintenance which is applicable for the PC-12/45. This plan is intended as a tool to assist the operator/maintainer in planning. Each task has a unique task number. This number is only used in the Master Maintenance Plan and Progressive Inspection program for task identification.
TASK NO.
ITEMS / DESCRIPTION
00-00/45
Aircraft Do the corrosion and corrosion protection inspections AMM 12-A-20-40-00-00A-901A-A Airworthiness Directives and Service Bulletins reviewed and complied with as required Check Chapter 4 and Chapter 5 - Overhaul and Replacement Schedule and Time Limited Inspection Requirements reviewed and any additional requirements are complied with Check Access panels 42AB, 42AT and 32CT Install Access panels 42AB, 42AT and 32CT Remove Access panels 11AR, 11BL, 11BR, 12AZ, 12AB, 12BB, 12BL, 12BR, 12BZ, 12CL, 12CR, 12CZ, 12DZ,
00-00/121 00-00/122
06-00/119 06-00/123 06-00/218
REVISIÓN: ORIGINAL
INTERVAL/ LIMITATIONS
FECHA: 16-JUNIO-2014
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y Y
PAG: A2.13
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
06-00/219
07-10/160
07-10/161
10-10/428
11-00/220
12-20/124
12-20/125 12-20/126 21-20/127
21-20/221
21-30/46
21-30/47
21-30/48 21-30/49 21-40/50
INTERVAL/ LIMITATIONS
AL
TIME LIMITS
12EL, 12ER, 12EZ, 12FZ, 12HZ, 21GZ, 21JZ, 21PZ, 21QZ, 31AB, 31AL, 31BL, 32AB, 32AL, 32BL, 32BT, 32CL, 33ET, 41AT, 42AT, 42AB, 51KB, 51MB, 51NB, 52KB, 52MB, 52NB, 52OB, 52PB, 52RB, 52TB, 52SB, 61KB, 61MB, 61NB, 62KB, 62MB, 62NB, 62OB, 62PB, 62RB, 62SB, 62TB Open/remove and examine. Make sure the drain holes are clear. AMM 12-A-06-20-00-00A-040A-A Access panels 11AR, 11BL, 11BR, 12AZ, 12AB, 12BB, 12BL, 12BR, 12BZ, 12CL, 12 CR, 12CZ, 12DZ, 12EL, 12ER, 12EZ, 12FZ, 12HZ, 21GZ, 21JZ, 21PZ, 21QZ, 31AB, 31BL, 32AL, 32AB, 32AL, 32BL, 32BT, 32CL, 33ET, 41AT, 42AT, 42AB, 51KB, 51MB, 51NB, 52KB, 52MB, 52NB, 52OB, 52PB, 52RB, 52TB, 52SB, 61KB, 61MB, 61NB, 62KB, 62MB, 62NB, 62OB, 62PB, 62RB, 62SB, 62TB Close or install Aircraft Lower to the ground, remove jacks and disconnect from ground AMM 12-A-07-10-00-00A-901A-A Aircraft Lift on jacks and connect the aircraft to ground AMM 12-A-07-10-00-00A-901A-A External Protective Covers Examine. Replace if any part of the cover is missing, damaged, torn or does not install properly Placards and markings Examine and attach new placards if necessary AMM 12-A-11-20-00-00A-901A-A and 12-A-11-30-00-00A040A-A Aircraft Wash the exterior, including the landing gear and flap compartments AMM 12-A-12-20-01-00A-902A-A Windshields and windows Clean AMM 12-A-12-20-02-00A-902A-A Cockpit and cabin Clean AMM 12-A-12-20-03-00A-902A-A ECS emergency shut-off system ECS EMER shut-off valve - operational test; max pull force 22.5 lbf (100N) and make sure ram air scoop is completely open ECS and bleed air ducts, pipelines, equipment and associated clamps in the engine compartment Examine Pressurization system Adjustment/Test AMM 12-A-21-30-00-00A-903A-A Pressurization outflow valve and safety valve Remove and clean AMM 12-A-21-30-01-00A-250A-A
Cabin altitude switch Functional test AMM 12-A-21-30-07-00A-903A-A Cabin differential pressure switch Functional test AMM 12-A-21-30-08-00A-903A-A Water separator condenser
REVISIÓN: ORIGINAL
1500 flying hours or 2 Years whichever comes first 1500 flying hours or 2 Years whichever comes first (installed)
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
5 years (installed)
Y
5 years (installed)
Y
500 flying hours
Y
FECHA: 16-JUNIO-2014
100 HOUR
Y
PAG: A2.14
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
21-40/51 21-40/52 21-40/53
21-40/54
21-40/55 21-40/56 21-40/128
21-50/58 21-50/59
21-50/223 21-50/433
22-10/60
22-10/233
22-20/129 22-20/130 22-20/226 24-20/227 24-30/19
24-30/20
INTERVAL/ LIMITATIONS
Clean AMM 12-A-21-40-02-00A-250A-A Overtemperature switch Functional test AMM 12-A-21-40-06-00A-903A-A Duct overtemperature switch Functional test AMM 12-A-21-60-05-00A-903A-A Secondary heaters thermal protection switches (MSN 101-320 without a modified auxiliary heating system) Operational test AMM 12-A-21-40-09-00A-903A-A Secondary heaters thermal protection switches (MSN 321-999 and aircraft with a modified auxiliary heating system) Operational test AMM 12-A-21-40-00-00A-903A-A Cold air unit Re-oil AMM 12-A-21-40-01-00A-902A-A Heat exchanger matrix Inspection/check AMM 12-A-21-40-01-00A-313A-A Flight compartment foot heater (if installed) thermal protection switch Operational test AMM 12-A-21-40-11-00A-903A-A Vapor cycle compressor motor (if installed) Inspection/check AMM 12-A-21-50-03-00A-313A-A Vapor cycle compressor motor drive belt (if Installed) Check for tension AMM 12-A-21-50-00-00A-903A-A or 12-A-21-50-00-00A-903B-A Vapor cycle cooling system (if installed) Examine the cooling unit Vapor cycle compressor condenser module (including motor) (if installed) Clean per OSCMM
Servo mount (pitch, roll and yaw) Remove for clutch check AMM 12-A-22-10-00-00A313A-A Pitch, roll, and yaw actuators and capstan control cables Examine Angle of Attack (AOA) transmitters Examine Stick pusher system Check AMM 12-A-22-20-00-00A-903A-A Stick pusher system Functional test AMM 12-A-22-20-00-00A-903A-A AC electrical system Operational test AMM 12-A-24-20-00-00A-903A-A Starter/generator Overhaul P/N 978.91.23.421 P/N 978.91.23.422 P/N 978.91.23.431 P/N 978.91.23.433 P/N 978.91.23.441 Generator 2 drive assembly aft bearing (smaller inner
REVISIÓN: ORIGINAL
AL
TIME LIMITS
5 years (installed)
Y
5 years (installed)
Y
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
500 flying hours
Y
Y
500 flying hours
Y
Y
500 Ops Hr
Y
500 Ops Hr
Y
Initially at each scheduled inspection, then based on field experience the interval can be adjusted to a more effective interval 1000 flying hours or 12 months whichever comes first (installed)
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
1000 flying hours
Y
10000 flying hours
Y
FECHA: 16-JUNIO-2014
Y Y
Y
Y
Y
PAG: A2.15
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
24-30/21
24-30/61 24-30/62
24-30/63 24-30/64
24-30/65 24-30/66
24-30/67
24-30/68
24-30/69
24-30/131
24-30/132
24-30/228
24-40/229 24-50/70
INTERVAL/ LIMITATIONS
diameter) (Pre SB 24-010) Discard Generator 2 drive assembly aft bearing (smaller inner diameter) (Post SB 24-010 and MSN 231 - 999) Discard Starter/generator brushes Brush check AMM 12-A-24-30-01-00A-313A-A Generator 1 and 2 ground points Battery 1 and 2 (if installed) ground points Examine the corrosion protective layer AMM 12-A-2430-00-00A-901A-A Generator 2 (Part No. 524.32.12.158 Mod. B) brushes Inspection/check AMM 12-A-24-30-02-00A-313A-A Generator 2 (Part No. 524.32.12.158 Mod. A, Mod. C and above) brushes Inspection/check AMM 12-A-24-30-02-00A-313A-A Generator 2 drive assembly housing (Pre SB 24-010) Inspection/check AMM 12-A-24-30-04-00A-313A-A Generator 2 drive assembly housing (Post SB 24-010 and MSN 231 - 999) Inspection/check AMM 12-A-24-30-04-00A-313A-A NiCad battery or batteries (if 2nd battery installed) (Part No. 976.17.31.301) Remove and service AMM 12-A-24-30-07-00A-920AA and CMM NiCad battery or batteries (if 2nd battery installed) (Part No. 976.17.31.302) Remove and service AMM 12-A-24-30-07-00A-920AA and CMM Lead acid battery or batteries (if 2nd battery installed) Remove and do a capacity test AMM 12-A-24-30-0700A-920A-A and CMM
Generator 2 drive belt Examine and adjustment/test AMM12-A-24-30-0300A-903A-A or 12-A-24-30-03-00A-903B-A Battery (Batteries - if 2nd battery installed) Examine and operational test AMM12-A-24-30-0000A-903A-A or 12-A-24-30-00-00A-903B-A External power Operational test AMM12-A-24-30-00-00A-903A-A or 12-A-24-30-00-00A-903B-A External Power Unit (EPU) receptacle Examine Emergency power supply (if installed) Remove and Cap test AMM 12-A-24-52-51-00A-920A-
REVISIÓN: ORIGINAL
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
3000 flying hours
Y
200 flying hours
Y
2 years
Y
100 flying hours
Y
400 flying hours
Y
500 flying hours
Y
Y
1000 flying hours
Y
Y
Y
Y
Y
Y
Y
Y
100 flying hours or 3 month whichever comes first (installed) 400 flying hours or 12 month whichever comes first (installed) Initially at 1000 flying hours or 12 months (installed) whichever comes first. If capacity above 90% then every 600 flying hours or 6 months. If capacity is between 85% and 90% then every 300 flying hours or 3 months. If capacity is below 85% replace.
12 months (installed)
FECHA: 16-JUNIO-2014
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
PAG: A2.16
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
24-60/133 25-10/134 25-10/135 25-10/230
25-10/293
25-10/294 25-10/296
25-10/297
25-10/300
25-20/136 25-20/137 25-20/295 25-20/298 25-20/299
25-20/302
25-60/231
25-60/232 25-63/23
INTERVAL/ LIMITATIONS
A Cockpit circuit breaker panels and switch panels Examine Crew seat belts Examine Crew seats Examine as far as posible with seats installed Pilots relief tube system (if installed) Clean and leak check AMM 12-A-25-10-05-00A-920AA Crew seat cushion (Part No.0A318-0203 installed on IPECO Seat Part No's. 959.30.01.135 and 136) Discard Crew seat belts Overhaul Crew seats Remove MSN 101-660 AMM 12-A-25-10-01-00A-920A-A MSN 661-999 AMM 12-A-25-10-05-00A-920A-A Crew seats Install MSN 101-660 (AMM 12-A-25-10-01-00A-920A-A MSN 661-999 AMM 12-A-25-10-05-00A-920A-A Crew seats Remove cushions, covers and shells (Ref. CMM) and examine seat. Install cushions, covers and shells. Note: The CMM Document No’s. are given in AMM 12-A-25-10-01-00A-920A-A and 12-A-25-10-05-00A920A-A Passenger seat belts and extensions Examine Passenger seats Examine Passenger seat belts and extensions Overhaul Passenger seats Passenger seats Remove AMM 12-A-25-20-01-00A-920A-A, 12-A-2521-01-00A-920A-A, 12-A-25-22-01-00A-920A-A Install AMM 12-A-25-20-01-00A-920A-A, 12-A-25-2101-00A-920A-A, 12-A-25-22-01-00A-920A-A Passenger seats Examine as far as possible with seats installed. Move the recline mechanism and swivel function (executive seat only) through its full motion and check for correct operation. If necessary, refer to the applicable supplier CMM (CMM 25-20-07 for executive seats and CMM 25-20-99 for standard seats). ELT Operational test AMM12-A-25-63-00-00A-903A-A or 12-A-25-63-10-00A-903A-A or 12-A-25-63-20-00A903A-A or 12-A-25-63-30-00A-903A-A ELT installation Examine ELT battery Discard
REVISIÓN: ORIGINAL
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
3 years (elapsed for factory new or spare part new from EASA Form 1 date)
Y
12 years (elapsed)
Y
Y
12 years (elapsed)
Y Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
After 1 hour of use or as shown on the
FECHA: 16-JUNIO-2014
Y
Y
Y
Y
Y
Y
PAG: A2.17
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
INTERVAL/ LIMITATIONS
25-63/434
ELT Nav Interface Unit Serial Memory Module Discard Note 1Units which have already operated more than the allowed period must be replaced within 500 flying hours or 6 months, whichever comes first. Fire extinguisher Life limit Fire extinguisher Content check Flight control cables including auto pilot and stick pusher cables Inspection/check AMM 12-A-27-00-00-00A-313A-A
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
battery label
26-20/2 26-20/24 27-00/71
27-00/138 27-00/402
27-10/139 27-10/234
27-10/235 27-10/236
27-10/237
27-10/238
27-10/394
Aileron, elevator and rudder controls Operate, make sure full and free travel Bonding leads to all Flight Control Surfaces Examine
Y
10 years (elapsed)
Y
12 months (elapsed)
Y
2000 flying hours or 5 years whichever comes first (installed)
Y
Y
Y Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes firs
Aileron LH and RH Examine Aileron LH and RH rods and levers Examine Spray PTFE Teflon Spray OKS 571 (or equivalent) around the aileron pushrod guide roller sleeves at all three locations in each wing Aileron electrical bonding straps Examine Aileron controls Examine the control cables and pulleys as far as possible. Move the mechanism so that you can see all parts of the cables and make sure the safety clips are fully engaged in the turnbuckles Aileron cable tension Check MSN 101-683 AMM12-A-27-10-00-00A-903A-A MSN 684-999 AMM 12-A-27-10-00-00A-903B-A Ailerons Functional test MSN 101-683 AMM 12-A-27-10-00-00A-903A-A MSN 684-999 AMM 12-A-27-10-00-00A-903B-A Aileron Control System Examine AMM 12-A-27-10-00-00A-310A-A
REVISIÓN: ORIGINAL
16000 flying hours or 10 years whichever comes first (installed)
Y
Y
Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours
FECHA: 16-JUNIO-2014
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
PAG: A2.18
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
27-10/395
27-10/396
27-10/397
27-10/398
27-15/239
27-20/140
27-20/240 27-20/241
INTERVAL/ LIMITATIONS
Aileron Cable Segment Eddy Current Inspection AMM 12-A-27-10-09-00A-353A-A
Aileron Control Rods Eddy Current Inspection AMM 12-A-27-00-01-00A-353A-A
Aileron Control Rods Magnetic Particle Inspection AMM 12-A-27-00-01-00A-352A-A
Aileron Bellcranks Eddy Current and Magnetic Particle Inspections AMM 12-A-27-10-08-00A-353A-A AMM 12-A-27-10-08-00A-353B-A AMM 12-A-27-10-08-00A-352B-A
or 15,000 landings or 6 years, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first
Aileron trim Functional test MSN 101-683 AMM 12-A-27-15-00-00A-903A-A MSN 684-999 AMM 12-A-27-15-00-00A-903B-A Rudder Examine, in particular the cover plate (Part No. 555.40.12.215) on the bottom of the rudder to make sure it is not bent and there are no signs of interference with the rudder stop. Rudder static dischargers Examine Rudder controls Examine the control cables and pulleys as far as possible. Move the mechanism so that you can see all
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
y
Y
PAG: A2.19
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
27-20/242
27-20/243
27-20/244
27-20/245 27-20/246 27-20/374
27-20/375
27-20/376
27-20/431
INTERVAL/ LIMITATIONS
parts of the cables and make sure the safety clips are fully engaged in the turnbuckles Aileron/rudder interconnect system, MSN 101-683 Make sure the locking mechanism is fully engaged with the flaps at 40° and the moving parts (piston and housing) are lubricated. If necessary apply grease P04-002 with a brush. Retract the flaps to 0° and make sure the locking mechanism is fully disengaged. Rudder cable tension Check AMM12-A-27-20-00-00A-903A-A or 12-A-2720-00-00A-903B-A Rudder Functional test AMM12-A-27-20-00-00A-903A-A or 12-A-27-20-00-00A-903B-A Rudder trim Functional test AMM12-A-27-25-00-00A-903A-A Rudder electrical bonding straps Examine Rudder Control System Examine AMM 12-A-27-20-00-00A-310A-A
Rudder Bellcranks Eddy Current Inspection AMM 12-A-27-20-04-00A-353A-A
Rudder Cable Quadrant Shear Spigot Examine AMM 12-A-27-20-05-00A-310A-A
Rudder control cables tension Check after replacement of any rudder control system cables (Autopilot, and/or rudder) AMM 12-A-27-20-00-00A-903A-A
REVISIÓN: ORIGINAL
Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first At the next scheduled inspection, but not later than 150 flying hours
FECHA: 16-JUNIO-2014
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
y
Y
Y
Y
PAG: A2.20
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
27-30/141
Elevators Examine Elevator electrical bonding straps Examine Elevator static dischargers Examine Elevator controls Examine the control cables and pulleys as far as possible. Move the mechanism so that you can see all parts of the cables and make sure the safety clips are fully engaged in the turnbuckles Elevator cable tension Check AMM12-A-27-30-00-00A-903A-A Elevator Functional test AMM12-A-27-30-00-00A-903A-A Elevator control cables tension Check after replacement of any elevator control system cables (autopilot, stick pusher and/or elevator) AMM 12-A-27-30-00-00A-903A-A
27-30/247 27-30/248 27-30/249
27-30/250 27-30/251 27-30/334
27-30/363
27-30/364
27-30/365
27-30/366
Elevator - Control System Examine AMM 12-A-27-30-00-00A-310A-A
Elevator Control Rods Eddy Current Inspection AMM 12-A-27-00-01-00A-353A-A
Elevator Control Rods Magnetic Particle Inspection AMM 12-A-27-00-01-00A-352A-A
Elevator Control Lever Eddy Current Inspection AMM 12-A-27-30-05-00A-353A-A
REVISIÓN: ORIGINAL
INTERVAL/ LIMITATIONS
At the next Scheduled inspection, but not later than 150 flying hours Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat
FECHA: 16-JUNIO-2014
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
y
Y
PAG: A2.21
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
27-30/400
27-40/1
INTERVAL/ LIMITATIONS
Aileron Hinge Points Eddy Current Inspection AMM 12-A-57-60-06-00A-353A-A
Horizontal stabilizer trim Functional test of trim runaway aural warning system (FAA CMR) AMM12-A-27-40-00-00A-903A-A
27-40/3
Pitch trim actuator Life limit
27-40/25 27-40/26
27-40/142
27-40/252
27-40/291
27-40/292
27-40/307
27-50/4
27-50/27
27-50/28
27-50/29
Pitch trim actuator (Part No. 978.73.14.201) Overhaul Pitch trim actuator (Part No. 978.73.14.202 and 978.73.14.203) Overhaul Horizontal stabilizer trim Operational test of trim interrupt and alternate trim switches AMM 12-A-27-40-00-00A-903A-A Horizontal stabilizer trim actuator top and bottom attachments Examine Horizontal stabilizer trim Operational test of trim system AMM 12-A-27-40-0000A-903A-A Horizontal stabilizer trim Functional test of trim system AMM 12-A-27-40-0000A-903A-A Pitch trim actuator attachment parts, fail safe plates and their attachment parts (IPC 12-20-00-07) Life limit Flap actuators (black anodized) (Part No. 978.73.20.307, 308 and 309) Life limit Flap power drive unit (Part No. 978.73.20.001 and 002) Discard Flap power drive unit (Part No. 978.73.20.0-03) Overhaul
Flap actuators (white colored) (Part No’s 978.73.20.302, 303, 304, 305 and 306)
REVISIÓN: ORIGINAL
12,500 flying hours or 15,000 landings, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first 3000 flying hours or at Annual Inspection whichever comes first 20000 flying hours or 27000 landings whichever comes first
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
1500 flying hours
Y
5000 flying hours or 5 years whichever comes first (installed)
y
Y
Y
Y
10000 flying hours 20000 flying hours or 27 000 landings whichever comes first 4500 flying hours since new, or last overhaul 10000 flying hours or 13500 landings whichever comes first 4500 flying hours
FECHA: 16-JUNIO-2014
Y
Y
Y
Y
Y
Y
PAG: A2.22
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
27-50/30
27-50/31
27-50/72
27-50/73
27-50/74
27-50/75
27-50/76
27-50/77
27-50/143 27-50/144
27-50/253 27-50/254 27-50/255
27-50/386
INTERVAL/ LIMITATIONS
Discard Flap actuators (black anodized) (Part No. 978.73.20.307, 308 and 309) Overhaul Flap flexible drive shafts (Part No’s 945.02.02-.203, 204, 205 and 206) Discard Flap flexible drive shafts (Post SB 27-003) (Part No’s 945.02.02.201 and 202) Remove, clean, inspect and lubricate inner core AMM 12-A-27-50-00-00A-902A-A Flap actuators (white colored) (Part No’s 978.73.20.302, 303, 304, 305 and 306) Lubricate AMM 12-A-27-50-00-00A-902A-A Flap actuators (black anodized) (Part No. 978.73.20.307, 308 and 309) Lubricate AMM12-A-27-50-00-00A-902A-A Flap actuators (white colored) (Part No’s 978.73.20.302, 303, 304, 305 and 306) Backlash check AMM12-A-27-50-03-00A-313A-A Flap actuators (black anodized) (Part No. 978.73.20.307, 308 and 309) Backlash check AMM12-A-27-50-03-00A-313B-A
Flap electrical system (MSN 101-400 Pre SB 27-013) Do the flap electrical system maintenance practices tests AMM12-A-27-50-00-00A-901A-A Flaps Lower to 40° Flaps and flap support mechanism - examine. For Flap drive arms, refer to AMM 12-A-27-51-00-00A313A-A. Flaps electrical bonding straps Examine Flap motor, actuators and flexible drive shafts Examine Flaps Functional test and asymmetry monitor test. Pre SB 27-013 AMM 12-A-27-50-00-00A-903A-A Post SB 27-013 and MSN 401-999 AMM 12-A-27-5000-00A-903B-A Flap Mechanism Examine AMM 12-A-27-51-00-00A-310A-A
REVISIÓN: ORIGINAL
AL
5000 flying hours or 7000 landings Whichever comes first 10000 flying hours or 13500 landings Whichever comes first
ANNUAL
PI
Y
Y
400 flying hours or 12 month whichever comes first (installed) 150 flying hours or 12 month whichever comes first (installed) 600 flying hours or 12 month whichever comes first (installed) Annual inspection or 1000 flying hours or 1300 landings whichever comes first (installed)
Y
Y
Y
Y
Y
Y
Y
200 flying hours
FECHA: 16-JUNIO-2014
100 HOUR
Y
2000 flying hours
Threshold 30,000 flying hours or 39,000 landings, whichever comes first. Repeat 10,000 flying hours or 12,000 landings or 6 years, whichever comes
TIME LIMITS
Y Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
PAG: A2.23
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
27-50/387
Flap Drive Arm (not removed) Eddy Current Inspection AMM 12-A-27-51-00-00A-353A-A
27-50/388
27-50/389
27-50/390
27-50/391
27-50/392
Flap Drive Arm (removed) Eddy Current Inspection AMM 12-A-27-51-01-00A-353A-A AMM 12-A-27-51-02-00A-353A-A AMM 12-A-27-51-03-00A-353A-A
Flap Support Arm Eddy Current Inspection AMM 12-A-27-51-01-00A-353A-A AMM 12-A-27-51-02-00A-353A-A AMM 12-A-27-51-03-00A-353A-A
Flap Cove Rib FIttings Eddy Current Inspection AMM 12-A-27-51-01-00A-353A-A AMM 12-A-27-51-02-00A-353A-A AMM 12-A-27-51-03-00A-353A-A
Flap Aft Links Eddy Current Inspection AMM 12-A-27-51-01-00A-353A-A AMM 12-A-27-51-02-00A-353A-A AMM 12-A-27-51-03-00A-353A-A
Flap Bellcranks Eddy Current Inspection AMM 12-A-27-51-01-00A-353A-A AMM 12-A-27-51-02-00A-353A-A AMM 12-A-27-51-03-00A-353A-A
REVISIÓN: ORIGINAL
INTERVAL/ LIMITATIONS first Threshold 25,000 flying hours or 30,000 landings, whichever comes first. Repeat 2,500 flying hours or 3,000 landings, whichever comes first Threshold 30,000 flying hours or 39,000 landings, whichever comes first. Repeat 10,000 flying hours or 12,000 landings, whichever comes first Threshold 30,000 flying hours or 39,000 landings, whichever comes first. Repeat 10,000 flying hours or 12,000 landings, whichever comes first Threshold 30,000 flying hours or 39,000 landings, whichever comes first. Repeat 10,000 flying hours or 12,000 landings, whichever comes first Threshold 30,000 flying hours or 39,000 landings, whichever comes first. Repeat 10,000 flying hours or 12,000 landings, whichever comes first Threshold 30,000 flying hours or 39,000 landings, whichever comes first. Repeat 10,000 flying hours
FECHA: 16-JUNIO-2014
AL
TIME LIMITS
100 HOUR
ANNUAL
Y
Y
Y
Y
Y
Y
PAG: A2.24
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PI
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
INTERVAL/ LIMITATIONS
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
or 12,000 landings, whichever comes first 28-10/145 28-10/146
28-10/306 28-20/32 28-20/147 28-20/148
28-20/149
28-20/150 28-20/256
28-40/78
29-10/151
29-10/152
29-10/153
29-10/257
29-10/258
29-10/259
Fuel tank filler caps Examine Fuel Remove a sample from each drain valve and examine for water Fuel cross vent and outward check valve Operational test AMM12-A-28-10-01-00A-903A-A Engine driven pump Overhaul Fuel tank vent valve and flame arrestor Operational test AMM12-A-28-20-07-00A-903A-A Fuel filter element Remove and clean AMM12-A-28-20-01-00A-920A-A and 12-A-28-20-01-00A-250A-A Firewall shutoff valve Operate FUEL EMERG SHUTOFF lever and make sure firewall shutoff valve opens and closes fully to each dead stop. Make sure movement is free and check if initial pull out force at lever outer end is below 10 lbf (44.5 N) Engine driven pump Examine Fuel system components Examine as far as possible with panels in Task 0600/218 opened/removed Fuel low level warning system Operational test MSN 101-105 AMM12-A-28-40-00-00A-903A-A MSN 106-999 AMM12-A-28-40-00-00A-903B-A Low pressure filter blockage indicator Make sure that it has not come out. If indicator found out, do the inspection/check procedure AMM12-A-2910-04-00A-313A-A Hydraulic system MSN 101-230 - check fluid sensor and level using maintenance switch box. Fill as necessary AMM 12-A29-00-00-00A-902A-A. MSN 231-999 - make sure fluid level indicator on the reservoir tank shows full. Fill as necessary AMM 12-A29-00-00-00A-902B-A Reservoir tank Make sure nitrogen pressure is correct. Pressurize as necessary MSN 101-230 AMM12-A-29-00-00-00A-902A-A MSN 231-999 AMM12-A-29-00-00-00A-902B-A Power pack Examine, specially for leaks and cracks on the end plates and where motor is attached Nitrogen accumulator Check nitrogen pressure and fill as necessary AMM 12-A-29-10-02-00A-901A-A Power pack electric motor shaft seal drain fluid collector bottle (Post SB 29-002 and MSN 181-999) Remove, clean and re-install
REVISIÓN: ORIGINAL
1000 flying hours
Y
3500 flying hours
Y
1000 flying hours or 4 years whichever comes first (installed)
FECHA: 16-JUNIO-2014
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
PAG: A2.25
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
30-10/79
Airfoil de-icers Apply a surface coating of Age Master No. 1 in accordance with the manufacturers instructions Wing and horizontal stabilizer airfoil de-ice boots Inspection/check AMM 12-A-30-10-00-00A-313A-A Inertial separation system Operational test. MSN 101-320 and 322-400 AMM 12-A-30-20-00-00A903A-A MSN 321 and 401-999 AMM 12-A-30-20-00-00A903B-A Airfoil de-ice system Functional test AMM 12-A-30-10-00-00A-903A-A Engine air intake de-ice lip Examine, look for signs of gas leaks - none are permitted Air by-pass door and operating mechanism Examine and lubricate with minimum quantity of P10001 Probes de-ice system Operational test. Single P-S system AMM 12-A-30-30-10-00A-903A-A Dual system and P-S indicator AMM 12-A-30-30-2000A-903A-A MSN 321 and 401-999 AMM 12-A-30-30-20-00A903B-A Windshield de-ice system Operational test AMM 12-A-30-40-00-00A-903A-A or 12-A-30-40-00-00A-903B-A Propeller de-ice system Inspection/check AMM 12-A-30-60-00-00A-313A-A Propeller de-ice system Operational test AMM 12-A-30-60-00-00A-903A-A CAWS CACU clock battery (MSN 321 and 401 - 999) Discard Main and nose wheel bearings Lubricate AMM 12-A-12-20-06-00A-902A-A
30-10/154 30-10/155
30-10/260 30-20/156
30-20/261
30-30/157
30-40/262
30-60/158 30-60/159 31-50/34 32-10/80
32-10/81
32-10/162 32-10/163 32-10/164 32-10/165
32-10/263 32-10/264
INTERVAL/ LIMITATIONS
Main landing gear axles and bushes (PC-12/45 and PC-12/47 aircraft) Inspection/Check AMM 12-A-32-10-00-00A-313A-A
6 month
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
2 years (installed) Tire change or 12 month whichever comes first (installed) 2000 flying hours or 12 months whichever comes first (installed)
Main landing gear Lubricate AMM 12-A-12-20-04-00A-902A-A Main landing gear legs Examine Main landing gear compartments Examine Main landing gear shock struts Check nitrogen pressure AMM 12-A-32-10-00-00A902A-A Main landing gear electrical bonding straps Examine Main landing gear left and right axle bolt (Pre SB 32006) Remove and examine. Replace if damaged. Install a serviceable bolt
REVISIÓN: ORIGINAL
AL
FECHA: 16-JUNIO-2014
Y
Y
Y
Y
PAG: A2.26
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
INTERVAL/ LIMITATIONS
32-10/345
Main landing gear Overhaul CMM 02099
Threshold 25,000 flying hours or 30,000 landings, whichever comes first. Repeat 8,300 flying hours or 10,000 landings or 6 years, whichever comes first Threshold 25,000 flying hours or 30,000 landings, whichever comes first. Repeat 8,300 flying hours or 10,000 landings, whichever comes first Threshold 25,000 flying hours or 30,000 landings, whichever comes first. Repeat 8,300 flying hours or 10,000 landings, whichever comes first
32-10/346
32-10/347
32-20/5
32-20/166
32-20/167 32-20/168
32-20/169 32-20/265 32-20/266
32-20/305
32-20/335
32-20/336
MLG Yoke fitting lugs Eddy Current Inspection CMM 02099
MLG Trailing Link Eddy Current Inspection CMM 02099
NLG drag link right part (Part No. 532.20.12.140) (Pre SB 32-014) Life limit Nose landing gear leg shock strut Check nitrogen pressure AMM 12-A-32-20-00-00A902A-A Nose landing gear Lubricate AMM 12-A-12-20-04-00A-902A-A Nose landing gear leg and steering mechanism Examine, in particular the steering rod end (Part No. 532.20.12.134) for the complete retention of bearing into the steering rod end housing. Nose landing gear compartment Examine Nose landing gear electrical bonding straps Examine Nose landing gear spring strut Part No. 532.20.12.250 Remove, clean and lubricate AMM12-A-32-20-03-00A920A-A and 12-A-32-20-03-00A-250A-A Nose landing gear actuator fuselage attachment fitting (Part No. 553.10.12.326) Examine, if cracks are found replace attachment fitting SRM 12-A-53-00-01-00A-663A-A Nose landing gear torque tube (Part No. 532.50.12.047) Life limit NLG drag link right part (P/N 532.20.12.289 or 532.20.12.140)
REVISIÓN: ORIGINAL
4000 landings
11000 flying hours or 15000 landings or 10 years, whichever comes first Initially 2000 flying hours or 2500
FECHA: 16-JUNIO-2014
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
PAG: A2.27
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
32-20/403
32-30/170
32-40/171
32-40/172
32-40/173
32-40/174
32-40/175
32-40/176
32-50/404
33-40/177
33-41/178
ITEMS / DESCRIPTION
INTERVAL/ LIMITATIONS
Inspection/check AMM 12-A-32-20-06-00A-313A-A
landings (installed) whichever comes first, then every 300 flying hours or 400 landings, whichever comes first. Threshold 25,000 flying hours or 30,000 landings, whichever comes first. Repeat 8,300 flying hours or 10,000 landings or 6 years, whichever comes first
NLG Overhaul CMM 02100
Extension and retraction system Functional test of extension and retraction system and emergency extension system AMM 12-A-32-30-0000A-903A-A Mainwheels Examine. Rotate wheels, make sure bearing movement is smooth and free and no excessive play exists Mainwheel tires Examine and check tire pressure AMM 12-A-12-1004-00A-902A-A Nosewheel Examine. Rotate wheel, make sure bearing movement is smooth and free and no excessive play exists Nosewheel tire Examine and check tire pressure AMM12-A-12-10-0400A-902A-A Brake system Apply the parking brake. Examine the brake units. Make sure that pad wear indicators protrude from housing. Fluid reservoir Check and replenish if necessary AMM 12-A-12-1002-00A-902A-A NLG Steering Mechanism Examine AMM 12-A-32-50-00-00A-310A-A
Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 8,300 flying hours or 10,000 landings or 6 years, whichever comes first
Exterior lighting Operational test. MSN 101-320 and 322-400 AMM12-A-33-40-00-00A903A-A MSN 321 and 401-999 AMM 12-A-33-40-00-00A903B-A Landing lights
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
PAG: A2.28
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
33-42/179 33-43/180 33-44/181 33-46/182 34-00/183 34-00/184 34-11/82
34-11/185 34-11/186 34-11/268
34-14/83
34-21/84 34-25/85 34-54/86
35-10/6 35-10/7
35-10/187 35-10/188 35-10/269 35-10/270 35-20/87 52-10/88
INTERVAL/ LIMITATIONS
Examine Taxi lights Examine Navigation and strobe lights Examine Recognition lights (if installed) Examine Beacon lights (if installed) Examine Communications and navigation antennas Examine Cockpit instruments and avionic equipment Examine Static system Leak check. Single system AMM 12-A-34-11-10-00A-903A-A Dual system AMM 12-A-34-11-20-00A-903A-A Pitot tube Examine Static ports Examine Pitot and static system Drain. Single system AMM 12-A-34-11-00-00A-040A-A Dual system AMM 12-A-34-11-20-00A-901A-A Altimeter Check calibration at an approved center in accordance with the regulation in force (Ref. FAR Part 91 411) Standby magnetic compass Check swing AMM 12-A-34-21-00-00A-903A-A Attitude Heading Reference System (AHRS) Check swing AMM 12-A-34-25-00-00A-903A-A Transponder system (single and dual systems) Functional test AMM 12-A-34-54-00-00A-903A-A or 12-A-34-54-00-00A-903B-A Oxygen bottle Life limit Oxygen bottle Hydrostatic test. Refer to AVOX Service Information Letter SIL-35-114 latest revision (www.avoxsys.com).
High pressure relief indicator (green disk) Make sure that it is not damaged Oxygen system Check contents Oxygen pipelines and equipment Examine Oxygen system Operational test AMM 12-A-35-00-00-00A-903A-A Passenger oxygen masks Inspection/check AMM 12-A-35-20-00-00A-313A-A Passenger/crew door Examine with trim removed AMM 12-A-25-21-03-00A920A-A or 12-A-25-22-03-00A-920A-A Examine the top step area around the insulation mat
REVISIÓN: ORIGINAL
AL
2 years
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
2 years (installed)
Y
2 years (installed)
Y
2 years (installed)
Y
2 years (installed)
Y
15 years (elapsed)
Y
Refer to AVOX Service Information Letter SIL-35-114 latest revision (www.avoxsys.com).
Y
Y Y
3 years (installed)
Y
2000, 4000, 6000 flying hours or 2, 4, 6 years whichever comes first
Y
FECHA: 16-JUNIO-2014
Y Y
Y
Y
Y
PAG: A2.29
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
52-10/189
52-10/190
52-10/191
52-10/192
52-10/271
52-10/348
52-10/405
52-10/406
52-20/272 52-20/349
INTERVAL/ LIMITATIONS
for corrosion. If corrosion is found, write to Pilatus for a specific repair Examine door hinge pin and hinges AMM 12-A-52-1000-00A-313A-A Passenger/crew door seal Clean with a dry cloth, examine and apply P09-002 french chalk Passenger/crew door shoot bolts and door frame fittings Examine Passenger/crew door handle lock pin Make sure movement is free Passenger/crew door hinges Examine and lubricate as necessary with minimum quantity of P10-001 Lubricant Passenger/crew door, counterbalance and cable support brackets Examine Passenger/crew door Examine all structural elements AMM 12-A-52-10-00-00A-310A-A
Passenger/Crew Door Piano Hinge Eddy Current Inspection AMM 12-A-52-00-01-00A-353A-A
Passenger/Crew Door Skin Eddy Current Inspection AMM 12-A-52-10-01-00A-353A-A
Emergency door Examine (door removed) Emergency door Examine all structural elements AMM 12-A-52-20-00-00A-310A-A
REVISIÓN: ORIGINAL
Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first. Threshold 25,000 flying hours or 30,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first.
Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500
FECHA: 16-JUNIO-2014
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
PAG: A2.30
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
52-30/8
INTERVAL/ LIMITATIONS flying hours or 15,000 landings or 6 years, whichever comes first 13000 flying hours or 17000 landings whichever comes first
Cargo door lower lug fittings (qty 3) Life limit
52-30/89
52-30/193
52-30/194
52-30/195
52-30/273
52-30/274 52-30/350
52-30/407
52-30/408
Cargo door Examine with trim removed AMM 12-A-25-21-03-00A920A-A or 12-A-25-22-03-00A-920A-A. Examine door hinge pin and hinges AMM 12-A-52-3000-00A-313A-A Cargo door seal Clean with a dry cloth, examine and apply P09-002 french chalk Cargo door shoot bolts, door frame fittings and hooks Examine. Make sure the hook roller bushes are free to rotate. For roller bush wear limits refer to AMM 12-A52-30-00-00A-313A-A Cargo door hinges Examine and lubricate as necessary with minimum quantity of P10-001 Lubricant Emergency door seal Clean with a wet cloth, dry and examine and apply P09-002 french chalk Cargo door Examine Cargo door Examine all structural elements AMM 12-A-52-30-00-00A-310A-A
Cargo Door Piano Hinge Eddy Current Inspection AMM 12-A-52-30-00-01A-353A-A
Cargo Door Skin Eddy Current Inspection AMM 12-A-52-30-01-00A-353A-A
REVISIÓN: ORIGINAL
AL
FECHA: 16-JUNIO-2014
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
2000, 4000, 6000 flying hours or 2, 4, 6 years whichever comes first
Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first. Threshold 25,000 flying hours or 30,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever
TIME LIMITS
Y
Y
Y
Y
PAG: A2.31
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
INTERVAL/ LIMITATIONS
52-70/275
Door warning system Operational test AMM 12-A-52-70-00-00A-903A-A Fuselage and associated structure (Pre SB 04-009) Life Limit
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
comes first.
53-00/9
53-00/90
53-00/91
53-00/92
53-00/93
53-00/94
53-00/196
53-00/276 53-00/277
53-00/278
53-00/279 53-00/280
53-00/324
53-00/337 53-00/351
Front pressure bulkhead Examine with insulation on engine and cockpit sides removed. If insulation on cockpit side is wet, remove, dry and reinstall insulation Fuselage internal bottom surface Examine frames 10, 21, 24, 36 and frames adjacent to doors and to emergency exit, with insulation removed. If corrosion is found, examine all fuselage bottom surface with insulation removed. If insulation is wet, remove, dry and reinstall insulation Rear pressure bulkhead Examine with trim removed
Structure around windows Examine
Door frames and emergency exit frame Examine. If insulation is installed in the door frames and is wet, remove and discard it (no longer installed on production) Fuselage external surface Examine. For aircraft that experience stone damage to the belly skin, visually examine affected areas for cracks. Rear pressure Bulkhead Examine Floor top and bottom surface and seat rails Examine as far as possible with carpet and floor panels in Task 06-00/8 removed Baggage/freight net mounting plates attachment bolts and surrounding structure Examine for corrosion Baggage compartment Examine Rear fuselage internal structure Examine as far as possible, in particular examine battery mounting tray for corrosión Fuselage and associated structure (Post SB 04-009) Life limit
Carry through frames 21 and 24 Inspection/Check AMM 12-A-53-20-02-00A-313A-A Upper Longerons Frame 10 Eddy Current Inspection AMM 12-A-53-10-06-01A-353A-A
REVISIÓN: ORIGINAL
20000 flying hours or 27000 landings whichever comes first 2000, 4000, 6000 flying hours or 2, 4, 6 years whichever comes first
Y
Y
2000, 4000, 6000 flying hours or 2, 4, 6 years whichever comes first
Y
2000, 4000, 6000 flying hours or 2, 4, 6 years whichever comes first 2000, 4000, 6000 flying hours or 2, 4, 6 years whichever comes first 2000, 4000, 6000 flying hours or 2, 4, 6 years whichever comes first
Y
Y
Y
Y
25000 flying hours or 30000 landings whichever comes first
Threshold 25,000 flying hours or 30,000 landings, whichever comes first.
FECHA: 16-JUNIO-2014
Y
Y
PAG: A2.32
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
53-00/352
53-00/353
53-00/354
53-00/355
53-00/356
53-00/357
Fuselage Frames 10 to 16 Examine all structural elements AMM 12-A-53-10-00-00A-310A-A
Fuselage Frames 16 to 36 Examine all structural elements AMM 12-A-53-20-00-00A-310A-A
Fuselage Frames 36 to 43 Examine all structural elements AMM 12-A-53-30-00-00A-310A-A
Antenna Structure Examine AMM 12-A-53-00-00-00A-310A-A
Antenna - Bottom fuselage skin Eddy Current Inspection AMM 12-A-53-00-00-00A-353A-A
Antenna - Upper fuselage skin Eddy Current Inspection AMM 12-A-53-00-00-00A-353A-A
REVISIÓN: ORIGINAL
INTERVAL/ LIMITATIONS Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first Threshold 28,300 flying hours or 37,000 landings, whichever comes first. Repeat 8,300 flying hours or 10,000 landings, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes
FECHA: 16-JUNIO-2014
AL
TIME LIMITS
100 HOUR
ANNUAL
Y
Y
Y
Y
Y
Y
PAG: A2.33
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PI
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
53-00/358
53-00/359
53-00/360
53-00/361
53-00/419
55-00/10
INTERVAL/ LIMITATIONS
Upper Flange Carry Through Frames 21 and 24 Examine AMM 12-A-53-20-02-00A-310A-A
Frames 21 and 24 Wing Attachments Eddy Current Inspection AMM 12-A-53-20-02-00A-353A-A
Frames 21 and 24 Side Frame Attachments Eddy Current Inspection AMM 12-A-53-20-02-00A-353A-A
Frames 41 and 43 Stabilizer Attachment Eddy Current Inspection AMM 12-A-53-30-02-00A-353A-A or AMM 12-A-55-30-03-00A-353A-A
Frame 40 Eddy Current Inspection AMM 12-A-53-30-02-00A-353A-A
Tail structure (Pre SB 04-009) Life limit
REVISIÓN: ORIGINAL
first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 30,000 flying hours or 39,000 landings, whichever comes first. Repeat 10,000 flying hours or 12,000 landings or 6 years, whichever comes first Threshold 30,000 flying hours or 39,000 landings, whichever comes first. Repeat 10,000 flying hours or 12,000 landings, whichever comes first Threshold 30,000 flying hours or 39,000 landings, whichever comes first. Repeat 10,000 flying hours or 12,000 landings, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first 20000 flying hours or 27000 landings
FECHA: 16-JUNIO-2014
AL
TIME LIMITS
100 HOUR
ANNUAL
Y
Y
Y
Y
Y
Y
PAG: A2.34
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PI
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
55-00/325
55-10/95
55-10/96
55-10/197 55-10/319 55-20/362
55-20/367
55-20/368
55-30/198
55-30/199
55-30/281
INTERVAL/ LIMITATIONS
Tail structure (Post SB 04-00-9) Life limit
Horizontal stabilizer internal surfaces and horizontal/vertical stabilizer interface Examine as far as possible with panels removed Vertical stabilizer internal surfaces Examine as far as posible with panels removed
Horizontal stabilizer external surface Examine Horizontal/vertical stabilizer attachment Inspection/Check AMM 12-A-55-00-00-00A-361A-A Elevator Examine AMM 12-A-55-20-00-00A-310A-A
Elevator Drive Lever Eddy Current Inspection AMM 12-A-55-20-01-00A-353A-A
Elevator Hinges Eddy Current Inspection AMM 12-A-55-20-01-00A-353A-A
whichever comes first 25000 flying hours or 30000 landings whichever comes first 2000, 4000, 6000 flying hours or 2, 4, 6 years whichever comes first 2000, 4000, 6000 flying hours or 2, 4, 6 years whichever comes first
Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first
Vertical stabilizer external surface Examine, specially around rear spar top rivets. If cracks are found refer to SRM 12-A-55-00-01-00A664A-A for repair procedure Vertical stabilizer rear spar strap and lower aft fairing shear plate (Pre SB 55-002) Examine, if wear is found refer to SB 55-002 Vertical stabilizer electrical bonding straps Examine
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
PAG: A2.35
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
INTERVAL/ LIMITATIONS
55-30/369
Vertical Stabilizer Examine AMM 12-A-55-30-00-00A-310A-A
Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings,
55-30/370
55-30/371
55-30/372
55-30/420
55-40/373
Vertical Stabilizer Main and Rear Spar Attachment to Fuselage Eddy Current Inspection AMM 12-A-53-30-02-00A-353A-A or AMM 12-A-55-30-03-00A-353A-A
Vertical Stabilizer Main Attachment to Horizontal Stabilizer Eddy Current Inspection AMM 12-A-55-00-00-00A-353A-A
Vertical Stabilizer Pitch Trim Actuator Fitting and Attachment Eddy Current Inspection AMM 12-A-55-30-02-00A-353A-A
Vertical Stabilizer Forward Attachment to Frame 40 Eddy Current Inspection AMM 12-A-55-30-03-00A-353A-A
Rudder Examine AMM 12-A-55-40-00-00A-310A-A
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
AL
TIME LIMITS
100 HOUR
ANNUAL
Y
Y
Y
Y
y
Y
PAG: A2.36
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PI
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
55-40/377
55-40/410
56-10/200 56-11/12 56-11/13
56-11/14 56-11/15
56-11/332
56-11/378
56-20/201 57-00/11
INTERVAL/ LIMITATIONS whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first
Rudder Hinges Eddy Current Inspection AMM 12-A-55-40-05-00A-353A-A
Rudder Trim Tab Examine AMM 12-A-55-40-04-00A-310A-A
Windshield LH and RH Examine AMM 12-A-56-00-00-00A-313A-A Cockpit outer side, DV windows and cabin windows Replace Cockpit inner and outer side, DV windows and cabin windows Refer to AMM 12-A-56-00-00-00A-313A-A for limits
Windshield LH and RH Replace Windshield LH and RH Only unpressurized flight is permitted up to the next scheduled inspection providing it does not cause visual problems Cockpit side windows Inspection/check AMM 12-A-56-11-02-00A-313A-A
Windshield LH and RH and Cockpit Side Windows Examine with windshield and side windows removed AMM 12-A-56-11-01-00A-310A-A and AMM 12-A-56-11-02-00A-310A-A and AMM 12-A-53-10-16-00A-310A-A
Cockpit and cabin windows Examine AMM 12-A-56-00-00-00A-313A-A Wing structure (Pre SB 04-009) Life limit
REVISIÓN: ORIGINAL
If cracked or stress crazing Can be felt If chipped, cracked (only for inner side windows), scratched, bubbles or delaminated If cracked in inner lamination If cracked in outer lamination 11000 flying hours or 10 years whichever comes first (installed) Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first
20000 flying hours or 27000 landings whichever comes first
FECHA: 16-JUNIO-2014
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
PAG: A2.37
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
INTERVAL/ LIMITATIONS
57-00/97
Wing internal surfaces and flap compartment Examine as far as possible with all wing panels removed
2000, 4000, 6000 flying hours or 2, 4, 6 years whichever comes first 2000, 4000, 6000 flying hours or 2, 4, 6 years whichever comes first 11000 flying hours or 10 years whichever comes first
57-00/98
57-00/99
57-00/202 57-00/282 57-00/283
57-00/284 57-00/326
57-00/379
57-00/380
57-00/382
57-00/383
Landing gear compartments Examine, especially main and rear spar parts
Wing to fuselage attachments Examine attachment fittings with wings removed AMM 12-A-57-00-00-00A-313A-A Wing external surfaces Examine Wing tip static dischargers Examine Wing internal surfaces and flap compartment Examine as far as possible with panels in Task 0600/218 opened/removed Wing to fuselage Attachments Examine as far as posible Wing structure (Post SB 04-00-9) Life limit
Wing Examine all structural elements Rib 1 to Rib 20 AMM 12-A-57-00-00-00A-310A-A
Wing Main and Rear Spar to Fuselage Attachment Eddy Current Inspection AMM 12-A-57-00-03-00A-353A-A and AMM 12-A-57-00-03-01A-353A-A
Wing Rear Spar at Rib 8 Flap Arm Attachment Eddy Current Inspection AMM 12-A-57-20-10-00A-353C-A
Wing Main Spar Fastener Holes Rib 1 thru Rib 6 Eddy Current Inspection
REVISIÓN: ORIGINAL
25000 flying hours or 30000 landings whichever comes first Threshold 30,000 flying hours or 39,000 landings, whichever comes first. Repeat 10,000 flying hours or 12,000 landings or 6 years, whichever comes first Threshold 30,000 flying hours or 39,000 landings, whichever comes first. Repeat 10,000 flying hours or 12,000 landings or 6 years, whichever comes first Threshold 25,000 flying hours or 30,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 25,000 flying hours or
FECHA: 16-JUNIO-2014
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
PAG: A2.38
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
57-00/384
57-00/385
57-00/412
57-00/413
57-00/427
57-60/393
ITEMS / DESCRIPTION
INTERVAL/ LIMITATIONS
AMM 12-A-57-20-10-00A-353A-A
30,000 landings, whichever comes first. Repeat 3,300 flying hours or 4,000 landings, whichever comes first Threshold 25,000 flying hours or 30,000 landings, whichever comes first. Repeat 3,300 flying hours or 4,000 landings, whichever comes first Threshold 25,000 flying hours or 30,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 25,000 flying hours or 30,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 25,000 flying hours or 30,000 landings, whichever comes first. Repeat 2,500 flying hours or 3,000 landings, whichever comes first. Threshold 16,000 wing flying hours or 22,500 wing landings, whichever comes first. Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6
Wing Main Spar Fastener Holes Strap Rib 6 Eddy Current Inspection AMM 12-A-57-20-05-00A-353A-A
Wing Rear Spar Fastener Holes Rib 2 thru Rib 3 Eddy Current Inspection AMM 12-A-57-20-10-00A-353B-A
Wing Tips Examine AMM 12-A-57-33-00-00A-310A-A
Wing Skin around drain holes Eddy Current Inspection AMM 12-A-57-20-01-00A-353A-A
Wing Main Spar Fastener Holes Strap Rib 6 Eddy Current Inspection AMM 12-A-57-20-10-00A-353D-A
Aileron Examine AMM 12-A-57-60-00-00A-310A-A
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
AL
TIME LIMITS
100 HOUR
ANNUAL
Y
Y
Y
Y
Y
Y
PAG: A2.39
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PI
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
57-60/411
61-00/100
61-10/37
61-10/203
61-10/285
61-20/286
71-00/16
71-00/17
71-00/38
71-00/101
71-00/102
71-00/106
71-00/107
INTERVAL/ LIMITATIONS years, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first 400 flying hours or 12 month whichever comes first (Ref Hartzell SL 61) (installed) 4000 flying hours or 6 years whichever comes first (Ref Hartzell SL 61) (installed)
Aileron Trim Tab Examine AMM 12-A-57-60-04-00A-310A-A
Propeller Lubricate AMM 12-A-12-20-05-00A-902A-A
Propeller Overhaul
Propeller blades Examine. Repair blades as necessary Ref. Hartzell MM Propeller hub Remove spinner dome and examine propeller hub. Install spinner dome AMM 12-A-61-10-01-00A-920A-A Propeller governor, Overspeed governor and beta controls Examine Engine mounting frame (Pre SB 04-009) Life limit
Engine mounting frame, replace all bolts, washers and nuts Life limit Engine shock mount assemblies Overhaul Power plant torque limiter Operational test AMM 12-A-71-00-00-00A-903H-A
Power plant performance Operational test AMM 12-A-71-00-00-00A-903I-A
Oil pressure transducer electrical connector (Pre SB 79-004) Clean AMM 12-A-71-00-03-00A-250A-A Engine torque and stick pusher torque transducer electrical connectors Clean AMM 12-A-71-00-03-00A-250A-A
REVISIÓN: ORIGINAL
AL
TIME LIMITS
100 HOUR
Y
Y
Y
20000 flying hours or 27000 landings whichever comes first
Y
11000 flying Hours
Y
FECHA: 16-JUNIO-2014
PI
Y
Y
At engine overhaul, but not later than 5000 flying hours 500 flying hours or 12 months whichever comes first (installed) 500 flying hours or 12 months whichever comes first (installed) 500 flying hours or 12 months whichever comes first (installed) 500 flying hours or 12 months whichever comes first (installed)
ANNUAL
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
PAG: A2.40
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
71-00/204
Power plant Post inspection ground run tests AMM 12-A-71-00-0000A-903A-A Engine tubular mounting frame and shockmounts Examine. Replace shockmount if cracks in elastomer are more than 1 in (25,4 mm) long and/or 0.06 in (1,5 mm) deep Power plant and accessories Examine. Refer to P&WC EMM 72-00-00 Periodic inspection and do the 100 hour and minor inspection ítems Engine drain mast and tank Examine for fuel leaks (no leaks permitted) and drain (no excessive leaks) Power plant Inspection ground run - note defects. NOTE: A pre inspection ground run is not a pre-requisite but may be useful to determine any repair work needed to maintain the airworthiness of the aircraft AMM 12-A71-00-00-00A-903A-A Engine tubular mounting frame firewall attachment fittings Examine with firewall insulation blanket removed as necessary. If cracked, blistered or flaking paint is found on the mounting frame refer to SRM 12-A-5420-02-00A-664A-A Engine mounting frame (Post SB 04-009) Life limit
71-00/205
71-00/206
71-00/209
71-00/287
71-00/301
71-00/327
71-00/401
71-00/432
71-10/207
71-10/208 72-00/18 72-00/39
72-00/308 74-00/288
INTERVAL/ LIMITATIONS
Engine Mount Magnetic Particle Inspection AMM 12-A-71-00-05-00A-352A-A
Powerplant and accessories Refer to P&WC EMM 72-00-00 Periodic Inspection and do the time limited inspection items Engine cowlings ENG 43AL and ENG 43AR Open and examine, particularly for condition of rubbing strips and fasteners. Lubricate the hinges with a minimum of material P10-001C Engine cowlings ENG 43AL and ENG 43AR Close Engine rotor components Life limit Engine Overhaul Engine accessories Overhaul Ignition system Operational test AMM 12-A-74-00-00-00A-903A-A
REVISIÓN: ORIGINAL
25000 flying hours or 30000 landings whichever comes first Threshold 26,600 flying hours or 35,000 landings, whichever comes first. Repeat 6,600 flying hours or 8,000 landings, whichever comes first
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
P&WC SB 14002 3500 flying hours P&-WC SB 14-603 latestrevision P&WC SB 14603 latest revision
FECHA: 16-JUNIO-2014
Y Y Y
PAG: A2.41
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
76-00/210
Engine controls in engine compartment Examine Beta slip ring carbon block Make sure gap is not more than 0.01in (0.2- 5mm) Cockpit control quadrant Caution Do not move PCL into the reverse range PCL - move between idle and max and make sure movement is full and free. Condition lever - Do the operational test AMM 12-A-76-10-00-00A-903A-A. Manual override lever - move between off and max and make sure movement is full and free. Cockpit control quadrant Power control - operational test AMM 12-A-76-10-0000A-903A-A Manual override - operational test AMM 12-A-76-2000-00A-903A-A Cockpit control quadrant Examine Propeller feathering microswitches Functional test AMM 12-A-76-10-02-00A-903A-A
76-00/211 76-00/212
76-00/303
76-00/304 76-10/117
77-00/213
78-00/214 79-00/215
79-20/43 79-20/289
79-20/290
INTERVAL/ LIMITATIONS
Engine instrument system Operational test. MSN 101-111 (AMM 12-A-77-40-00-00A-903A-A MSN 112-320 and 322-400 AMM 12-A-77-40-00-00A903B-A MSN 321 and 401-999 AMM 12-A-77-40-00-00A903C-A Exhaust stubs Examine Oil filler cap/dipstick Energize aircraft electrical system AMM 12-A-24-0000-00A-901A-A. Remove filler cap, examine and make sure the seal is in good condition. Set and hold AIR/GROUND switch to GROUND and make sure after 60 seconds the CAWS OIL QTY caption comes on. Install filler cap and make sure the locking mechanism operates correctly. Oil cooler Overhaul Engine oil cooler Examine. Make sure outlet door has full and free movement Oil system chip detector indication system Operational test AMM 12-A-79-30-01-00A-903A-A
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y 3000 flying hours or 12 months whichever comes first
At engine overhaul
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
100 HOUR INSPECTION - SCHEDULED INSPECTIONS General 1. The terms used for the item inspection requirements are defined in 12-A-05-20-00-00A-018A-A
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.42
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Certain inspection items in the 100 hour inspection sheets are marked with an asterisk *. These items are applicable when the aircraft is inspected in conformity with the requirements of FAA Parts 43 and 91 only. 2. 100 Hour Inspection
Ac No. Chapt/Task 2.2 Job Set Up 27-50/143 12-20/124 12-20/125 12-20/126 06-00/123 71-10/207
AF Hrs. Item
Flaps - lower to 40° Aircraft - Wash the aircraft exterior, including the landing gear and flap compartments (12-A-12-20-01-00A-902A-A) Windshields and windows - clean (12-A-12-20-02-00A902A-A) Cockpit and cabin - clean (12-A-12-20-03-00A-902A-A) Access panels 42AB, 42AT and 32CT – remove (12-A-06-2000-00A-040A-A) Engine cowlings ENG 43AL and ENG 43AR - open and examine, particularly for condition of rubbing strips and fasteners. Lubricate the hinges with a minimum of P10001CWD40
INTERVAL
100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection
100 Hour Inspection
2.3 Procedure 10-10/428
22-20/129 22-20/130 24-30/131
*24-30/132 *24-60/133 *25-10/134 *25-10/135 *25-20/136 25-20/302
REVISIÓN: ORIGINAL
Parking, Mooring & Storing External protective covers - Examine. Replace if any part of the cover is missing, damaged, torn or does not install properly. Auto Flight Angle of Attack (AOA) transmitters – examine Stick pusher system - check (12-A-22-20-00-00A-903A-A) Electrical Power Generator 2 drive belt - examine and adjustment/test, AMM 12-A-24-30-03-00A-903A-A or 12-A-24-30-03-00A903B-A Battery (Batteries - if 2nd battery installed) - examine and operational test, AMM 12-A-24-30-00-00A-903A-A Cockpit circuit breaker panels and switch panels – Examine Equipment and Furnishings Crew seat belts – examine Crew seats - examine as far as possible with seats Installed Passenger seat belts and extensions - examine Passenger seats - examine as far as possible with seats installed. Move the recline mechanism and swivel function (executive seat only) through its full motion and check for correct operation. If necessary, refer to the applicable supplier CMM (CMM 25-20-07 for executive seats and CMM 25-20-99 for standard seats). FECHA: 16-JUNIO-2014
100 Hour Inspection
100 Hour Inspection 100 Hour Inspection
100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection
100 Hour Inspection
PAG: A2.43
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Ac No. Chapt/Task
*27-00/138 27-10/139 27-20/140
27-30/141 27-40/142 27-40/291 27-50/144
28-10/145 28-10/146 28-20/148 28-20/149
28-20/150 28-20/147
29-10/151
29-10/152
29-10/153
REVISIÓN: ORIGINAL
AF Hrs. Item Flight Controls Aileron, elevator and rudder controls - operate, make sure full and free travel Aileron LH and RH – examine Rudder - Examine, in particular the cover plate (Part No. 555.40.12.215) on the bottom of the rudder to make sure it is not bent and there are no signs of interference with the rudder stop. Elevators – examine Horizontal stabilizer trim - operational test of trim interrupt and alternate trim switches (12-A-27-40-00-00A-903A-A) Horizontal stabilizer trim - operational test of trim system (12-A-27-40-00-00A-903A-A) Flaps and flap support mechanism - examine. For Flap drive arms, refer to AMM 12-A-27-51-00-00A-313A-A. Fuel Fuel tank filler caps – examine Fuel - remove a sample from each drain valve and examine for wáter Fuel filter element - remove and clean, AMM 12-A-28-2001-00A-920A-A and 12-A-28-20-01-00A-250A-A Firewall shut-off valve - operate FUEL EMERG SHUTOFF lever and make sure firewall shutoff valve opens and closes fully to dead stop. Make sure movement is free and check if initial pull out force at lever outer end is below 10 lbf (44.5 N) Engine Driven fuel Pump (EDP) – examine Fuel tank vent valve and flame arrestor - operational test, AMM 12-A-28-20-07-00A-903A-A Hydraulic Power Low pressure filter blockage indicator - make sure that it has not come out. If indicator found out, do the inspection/check procedure, AMM 12-A-29-10-04-00A313A-A Hydraulic system, MSN 101-230 - check fluid sensor and level using maintenance switch box. Fill as necessary, AMM 12-A-29-00-00-00A-902A-A MSN 231-999 - make sure fluid level indicator on the reservoir tank shows full. Fill as necessary, AMM 12-A-29-00-00-00A-902B-A Reservoir tank - make sure nitrogen pressure is correct. Pressurize as necessary, MSN 101-230 AMM 12-A-29-0000-00A-902A-A, MSN 231-999 AMM 12-A-29-00-00-00AFECHA: 16-JUNIO-2014
INTERVAL
100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection
100 Hour Inspection
100 Hour Inspection 100 Hour Inspection
100 Hour Inspection
100 Hour Inspection
100 Hour Inspection
PAG: A2.44
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Ac No. Chapt/Task
30-10/154 30-20/155
30-20/156 30-30/157
30-60/158 30-60/159
*07-10/161 32-10/162 32-10/163 32-10/164 *32-10/165 32-10/264
32-20/167 32-20/168
32-20/169 *32-20/166 *32-30/170
*32-40/171 REVISIÓN: ORIGINAL
AF Hrs. Item 902B-A Ice and Rain Protection Wing and horizontal stabilizer airfoil de-ice boots inspection/check, AMM 12-A-30-10-00-00A-313A-A Inertial separation system - operational test. MSN 101-320 and 322-400, AMM 12-A-30-20-00-00A-903A-A. MSN 321 and 401-999, AMM 12-A-30-20-00-00A-903B-A Engine air intake de-ice lip - look for signs of gas leaks none are permitted Probes de-ice system - operational test. Single P-S system, AMM 12-A-30-30-10-00A-903A-A. Dual system and P-S indicator, AMM 12-A-30-30-20-00A-903A-A. MSN 321 and 401-999, AMM12-A-30-30-20-00A-903B-A Propeller de-ice system - inspection/check, AMM 12-A-3060-00-00A-313A-A Propeller de-ice system - operational test, AMM 12-A-3060-00-00A-903A-A Landing Gear Aircraft lift on jacks, AMM 12-A-07-10-00-00A-901A-A Main landing gear - for lubrication, AMM 12-A-12-20-0400A-902A-A
INTERVAL
100 Hour Inspection 100 Hour Inspection 100 Hour Inspection
100 Hour Inspection
100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection
Main landing gear legs – examine
100 Hour Inspection
Main landing gear compartments – examine Main landing gear shock struts - check nitrogen pressure (12-A-32-10-00-00A-902A-A) Main landing gear left and right axle bolt (Pre SB 32-006) remove and examine. Replace if damaged. Install a serviceable bolt. Nose landing gear - for lubrication, AMM 12-A-12-20-0400A-902A-A Nose landing gear leg and steering mechanism - examine, in particular the steering rod end (Part No. 532.20.12.134) for the complete retention of bearing into the steering rod end housing. Nose landing gear compartment – examine Nose landing gear shock strut - check nitrogen pressure, AMM 12-A-32-20-00-00A-902A-A Extension and retraction system - functional test of extension and retraction system and emergency extension system (12-A-32-30-00-00A-903A-A) Mainwheels - examine. Rotate wheels, make sure bearing
100 Hour Inspection
FECHA: 16-JUNIO-2014
100 Hour Inspection 100 Hour Inspection 100 Hour Inspection
100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection PAG: A2.45
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Ac No. Chapt/Task
32-40/172 *32-40/173 32-40/174 32-40/175
32-40/176 *07-10/160
33-40/177
33-41/178 33-42/179 33-43/180 33-44/181 33-46/182 34-00/183 *34-00/184 34-11/185 34-11/186 35-10/187 35-10/188 52-10/189 52-10/190 52-10/191 52-10/192
REVISIÓN: ORIGINAL
AF Hrs. Item movement is smooth and free and no excessive play exists Mainwheel tires - examine and check tire pressure (12-A12-10-04-00A-902A-A) Nosewheel - examine. Rotate wheel, make sure bearing movement is smooth and free and no excessive play exists Nosewheel tire - examine and check tire pressure (12-A-1210-04-00A-902A-A) Brake system - apply the parking brake. Examine the brake units. Make sure that pad wear indicators protrude from housing. Fluid reservoir - replenish if necessary (12-A-12-10-02-00A902A-A) Aircraft - lower to the ground, remove jacks and disconnect from ground (12-A-07-10-00-00A-901AA) Lighting Exterior lighting - operational test. MSN 101-320 and 322400 (AMM 12-A-33-40-00-00A-903A-A). MSN 321 and 401999 (AMM 12-A-33-40-00-00A-903B-A) Landing lights – examine Taxi lights – examine Navigation and strobe lights - examine Recognition lights (if installed) – examine Beacon lights (if installed) – examine Navigation Communications and navigation antennas – examine Cockpit instruments and avionic equipment – examine Pitot-tube – examine Static ports – examine Oxygen High pressure relief indicator (green disk) – make sure that it is not damaged Oxygen system - check contents Doors Passenger/crew door seal - clean with a dry cloth, examine and apply P09-002 french chalk Passenger/crew door shoot bolts and door frame fittings – examine Passenger/crew door handle lock pin - make sure movement is free Passenger/crew door hinges - examine and lubricate as necessary with minimum quantity of CPCtemporary (Pt. No. P10-001) FECHA: 16-JUNIO-2014
INTERVAL
100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection
100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection
PAG: A2.46
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Ac No. Chapt/Task 52-30/193 52-30/194
52-30/195
53-00/196
55-10/197 55-30/198
55-30/199
56-10/200 56-20/201
57-00/202 61-10/203
*71-00/205
71-00/206
71-00/209
74-00/288 REVISIÓN: ORIGINAL
AF Hrs. Item Cargo door seal - clean with a dry cloth, examine and apply French chalk (Pt. No. P09-002) Cargo door shoot bolts, door frame fittings and hooks examine. Make sure the hook roller bushes are free to rotate. For roller bush wear limits refer to AMM 12-A-5230-00-00A-313A-A Cargo door hinges - examine and lubricate as necessary with minimum quantity of P10-001 Lubricant Fuselage Fuselage external surface - examine. For aircraft that experience stone damage to the belly skin, visually examine affected areas for cracks. Stabilizers Horizontal stabilizer external surface – examine Vertical stabilizer external surface - examine, specially around rear spar top rivets. If cracks are found refer to SRM 12-A-55-00-01-00A-664A-A for repair procedure Vertical stabilizer rear spar strap and lower aft fairing shear plate (Pre SB 55-002) - examine, if wear is found refer to SB 55-002. Windows Windshield LH and RH - examine, AMM 12-A-56-00-00-00A313A-A Cockpit and cabin windows - examine, AMM 12-A-56-0000-00A-313A-A Wing Wing external surfaces – examine Propeller Propeller blades - examine. Repair blades as necessary Ref. Hartzell MM Power Plant Engine tubular mounting frame and shockmounts examine. Replace shockmount if cracks in elastomer are more than 1 in (25,4 mm) long and/or 0.06 in (1,5 mm) deep Power plant and accessories - examine. Refer to P&WC EMM 72-00-00 Periodic inspection and do the 100 hour and minor inspection ítems Engine drain mast and tank - for fuel leaks (no leaks permitted) and drain (no excessive leaks) Ignition Ignition system - operational test (12-A-74-00-00-00AFECHA: 16-JUNIO-2014
INTERVAL
100 Hour Inspection
100 Hour Inspection
100 Hour Inspection
100 Hour Inspection
100 Hour Inspection 100 Hour Inspection
100 Hour Inspection
100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection
100 Hour Inspection
100 Hour Inspection 100 Hour Inspection 100 Hour Inspection PAG: A2.47
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Ac No.
AF Hrs. Item
Chapt/Task
INTERVAL
903A-A) Engine Controls 76-00/2107600/210 76-00/211 76-00/304 76-00/212
77-00/213
78-00/214 79-00/215
79-30/290 2.3 Job Close Up 06-00/119 71-10/208 71-00/204 00-00/121 00-00/122
REVISIÓN: ORIGINAL
Engine controls in engine compartment – examine Beta slip ring carbon block - make sure gap is not more than 0.01in (0.25mm) Cockpit control quadrant – examine
100 Hour Inspection 100 Hour Inspection 100 Hour Inspection
CAUTION Do not move PCL into the reverse range PCL - move between idle and max and make sure movement is full and free. Condition lever - Do the operational test (12-A-76-10-00-00A-903A-A). Manual override lever - move between off and max and make sure movement is full and free. Engine Indication Engine instrument system - operational test MSN 101-111 (AMM 12-A-77-40-00-00A-903A-A) MSN 112-320 and 322400 (AMM 12-A-77-40-00-00A-903B-A) MSN 321 and 401999 (AMM 12-A-77-40-00-00A-903C-A) Exhaust Exhaust stubs – examine Oil Oil filler cap/dipstick - energize aircraft electrical system, AMM 12-A-24-00-00-00A-901A-A. Remove filler cap, examine and make sure the seal is in good condition. Set and hold AIR/GROUND switch to GROUND and make sure after 60 seconds the CAWS OIL QTY caption comes on. Install filler cap and make sure the locking mechanism operates correctly. Oil system chip detector indication system - operational test, AMM 12-A-79-30-01-00A-903A-A Access panels 42AB, 42AT and 32CT – Install Engine cowlings ENG43AL and ENG 43AR – close Power plant - post inspection ground run (12-A-71-00-0000A-903A-A) Airworthiness Directives and Service Bulletins reviewed and complied with as required Chapter 4 and Chapter 5 - Overhaul and Replacement Schedule, and Time Limited Inspection Requirements sections reviewed and any additional requirements are complied with FECHA: 16-JUNIO-2014
100 Hour Inspection
100 Hour Inspection
100 Hour Inspection
100 Hour Inspection
100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection
100 Hour Inspection
PAG: A2.48
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Ac No. Chapt/Task
INTERVAL
AF Hrs. Item
ANNUAL INSPECTION - SCHEDULED INSPECTIONS 1. General The terms used for the item inspection requirements are defined in DM 12-B-05-20-00-00A-018A-A.
Note
2.
The scope of the 100 flying hour inspection is included in the Annual Inspection. Note that some 100 flying hour inspection items are not called for in the Annual Inspection, but similar more detailed tasks replace them. Preparation
Ac No. Chapt/Task 71-00/287
27-50/143 12-20/124 12-20/125 12-20/126 25-10/296
25-20/298 07-10/161 06-00/218
REVISIÓN: ORIGINAL
AF Hrs. Item Power plant inspection ground run - note defects. A preinspection ground run is not a prerequisite but may be useful to determine any repair work necessary to maintain airworthiness of the aircraft. Flaps - lower to 40° Aircraft - Wash the aircraft exterior, including the landing gear and flap compartments (12-A-12-20-01-00A-902A-A) Windshields and windows - clean (12-A-12-20-02-00A902A-A) Cockpit and cabin - clean (12-A-12-20-03-00A-902-A-A) Crew seats - remove MSN 101-660, AMM 12-A-25-10-01-00A-920A-A, MSN 661-999, AMM 12-A-25-10-05-00A-920A-A Passenger seats - remove, AMM 12-A-25-20-01-00A-920AA, 12-A-25-21-01-00A-920A-A, 12-A-25-22-01-00A-920A-A Aircraft - Lift on jacks (12-A-07-10-00-00A-901A-A) Connect the aircraft to ground. Open/remove and examine the following panels:11AL, 11AR, 11BL, 11BR, 12AL, 12AR, 12AZ, 12AB, 12BB, 12BL, 12BR, 12BZ, 12CL, 12CR, 12CZ, 12DZ, 12EL, 12ER, 12EZ, 12FL, 12FR, 12FZ, 12HZ, 21GZ, 21JZ, 21PZ, 21QZ,31AB, 31AL, 31BL, 32AB, 32AL, 32BL, 32BT, 32CL, 32CT, 32DL, 33ET, 41AT, 42AT, 42AB, 51KB, 51MB, 51NB, 52KB, 52MB, 52NB, 52OB, 52PB, 52RB, 52TB, 52SB, 61KB, 61MB, 61NB, 62KB, 62MB, 62NB, 62OB, 62PB, 62RB, 62SB, 62TB. Make sure the drain holes are clear, AMM 12-A-06-20-00-00AFECHA: 16-JUNIO-2014
INTERVAL
Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection
Annual Inspection
PAG: A2.49
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Ac No. Chapt/Task
71-10/207
10-10/428
11-00/220
21-20/221 21-20/127
21-40/53
21-40/54
21-40/128
21-50/223
22-10/233 22-20/129 22-20/226
24-20/227 24-30/331 REVISIÓN: ORIGINAL
AF Hrs. Item 040A-A Engine cowlings ENG 43AL and ENG 43AR - open and examine, particularly for condition of rubbing strips and fasteners. Lubricate the hinges with a minimum of material P10-001CWD40. 3 Annual Inspection Parking, Mooring & Storing External protective covers - Examine. Replace if any part of the cover is missing, damaged, torn or does not install properly. Placards and Markings Placards and markings - examine. Attach new placards if necessary (12-A-11-20-00-00A-040A-A) and (1-2-A-11-3000-00A-040A-A) Air Conditioning ECS and bleed air ducts, pipelines, equipment and associated clamps in the engine compartment – examine ECS EMER shut-off valve - operational test; max pull force 22.5 lbf (100N) and make sure ram air scoop is completely open Secondary heaters thermal protection switches (MSN 101320 without a modified auxiliary heating system) operational test, AMM 12-A-21-40-09-00A-903A-A Secondary heaters thermal protection switches (MSN 321999 and aircraft with a modified auxiliary heating system) operational test, AMM 12-A-21-40-00-00A-903A-A Flight compartment foot heater (if installed) thermal protection switch - operational test, AMM 12-A-21-40-1100A-903A-A Vapor cycle cooling system (if installed) - examine the cooling unit Auto Flight Pitch, roll, and yaw actuators and capstan control cables – examine Angle of Attack (AOA) transmitters – examine Stick pusher system - functional test (12-A-22-20-00-00A903A-A) Electrical Power AC electrical system - operational test, AMM 12-A-24-2000-00A-903A-A Generator 2 drive belt - examine and adjustment/test, FECHA: 16-JUNIO-2014
INTERVAL
Annual Inspection
Annual Inspection
Annual Inspection
Annual Inspection Annual Inspection
Annual Inspection
Annual Inspection
Annual Inspection Annual Inspection
Annual Inspection Annual Inspection Annual Inspection
Annual Inspection Annual Inspection PAG: A2.50
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Ac No. Chapt/Task
24-30/132
24-40/229 24-60/133 25-10/134 25-10/230 25-10/300
25-20/136 25-20/137 25-60/232 27-10/139 27-10/234
27-10/235 27-10/236
27-10/237
27-10/238
27-15/239
27-20/140
REVISIÓN: ORIGINAL
AF Hrs. Item AMM 12-A-24-30-03-00A-903A-A or 12-A-24-30-03-00A903B-A Battery (Batteries - if 2nd battery installed) - examine and operational test, AMM 12-A-24-30-00-00A-903A-A or 12-A24-30-00-00A-903B-A External Power Unit (EPU) receptacle – examine Cockpit circuit breaker panels and switch panels – examine Equipment and Furnishings Crew seat belts – examine Pilots relief tube system (if installed) - clean and leak check, AMM 12-A-25-10-05-00A-920A-A Crew seats - remove cushions, covers and shells (Ref. CMM) and examine seat. Install cushions, covers and shells. Note 2 The CMM Document No’s. are given in Chap 25-10-01 and 25-10-05. Passenger seat belts and extensions – examine Passenger seats – examine ELT installation – examine Flight Controls Aileron LH and RH – examine Aileron LH and RH rods and levers - examine Spray PTFE Teflon Spray OKS 571 (or equivalent) around the aileron pushrod guide roller sleeves at all three locations in each wing Aileron electrical bonding straps – examine Aileron controls - examine the control cables and pulleys as far as possible. Move the mechanism so that you can see all parts of the cables and make sure the safety clips are fully engaged in the turnbuckles Aileron cable tension - check MSN 101-683, AMM 12-A-27-10-00-00A-903A-A MSN 684-999, AMM 12-A-27-10-00-00A-903B-A Ailerons - functional test MSN 101-683, AMM 12-A-27-10-00-00A-903A-A MSN 684-999, AMM 12-A-27-10-00-00A-903B-A Aileron trim - functional test MSN 101-683, AMM 12-A-27-15-00-00A-903A-A MSN 684-999, AMM 12-A-27-15-00-00A-903B-A Rudder - Examine, in particular the cover plate (Part No. 555.40.12.215) on the bottom of the rudder to make sure it is not bent and there are no signs of interference with the FECHA: 16-JUNIO-2014
INTERVAL
Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection
Annual Inspection
Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection
Annual Inspection
Annual Inspection
Annual Inspection
Annual Inspection
PAG: A2.51
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Ac No. Chapt/Task
27-20/246 27-20/240 27-20/241
27-20/242
27-20/243 27-20/244 27-20/245 27-30/141 27-30/247 27-30/248 27-30/249
27-30/250 27-30/251 27-40/142
27-40/292 27-40/252 27-50/144 27-50/253 27-50/254 27-50/255
REVISIÓN: ORIGINAL
AF Hrs. Item rudder stop. Rudder electrical bonding straps – examine Rudder static dischargers – examine Rudder controls - examine the control cables and pulleys as far as possible. Move the mechanism so that you can see all parts of the cables and make sure the safety clips are fully engaged in the turnbuckles Aileron/rudder interconnect system, MSN 101-683 - make sure the locking mechanism is fully engaged with the flaps at 40° and the moving parts (piston and housing) are lubricated. If necessary apply grease P04-002 with a brush. Retract the flaps to 0° and make sure the locking mechanism is fully disengaged Rudder cable tension - check, AMM 12-A-27-20-00-00A903A-A or 12-A-27-20-00-00A-903B-A Rudder - functional test, AMM 12-A-27-20-00-00A-903A-A or 12-A-27-20-00-00A-903B-A Rudder trim - functional test, AMM 12-A-27-25-00-00A903A-A Elevators – examine Elevators electrical bonding straps – examine Elevators static dischargers – examine Elevator controls - examine the control cables, pulleys, rods and connections as far as possible. Move the mechanism so that you can see all parts of the cables and rods. Make sure the safety clips are fully engaged in the turnbuckles. Elevator cable tension - check, AMM 12-A-27-30-00-00A903A-A Elevator - functional test, AMM 12-A-27-30-00-00A-903A-A Horizontal stabilizer trim - operational test of trim interrupt and alternate trim switches, AMM 12-A-27-40-00-00A903A-A Horizontal stabilizer trim - functional test of trim system, AMM 12-A-27-40-00-00A-903A-A Horizontal stabilizer trim actuator top and bottom attachments - examine Flaps and flap support mechanism - examine. For flap drive arms, refer to AMM 12-A-27-51-00-00A-313A-A. Flap electrical bonding straps – examine Flap motor, actuators and flexible drive shafts – examine Flaps - functional test and asymmetry monitor test. Pre SB 27-013, AMM 12-A-27-50-00-00A-903A-A FECHA: 16-JUNIO-2014
INTERVAL
Annual Inspection Annual Inspection Annual Inspection
Annual Inspection
Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection
Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection PAG: A2.52
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Ac No. Chapt/Task
28-10/145 28-10/146 28-20/148 28-20/149
28-20/256 28-20/150 28-20/147
29-10/257 29-10/151
29-10/152
29-10/258 29-10/153
29-10/259
30-10/154
REVISIÓN: ORIGINAL
AF Hrs. Item Post SB 27-013 and MSN 401-999, AMM 12-A-27-50-0000A-903B-A Fuel Fuel tank filler caps – examine Fuel - remove a sample from each drain valve and examine for wáter Fuel filter element - remove and clean, AMM 12-A-28-2001-00A-920A-A and 12-A-28-20-01-00A-250A-A Firewall shutoff valve - operate FUEL EMERG SHUTOFF lever and make sure firewall shutoff valve opens and closes fully to each dead stop. Make sure movement is free and check if initial pull out force at lever outer end is below 10 lbf (44.5 N) Fuel system components - examine Engine Driven fuel Pump (EDP) – examine Fuel tank vent valve and flame arrestor - operational test, AMM 12-A-28-20-07-00A-903A-A Hydraulic Power Power pack - examine, specially for leaks and cracks on the end plates and where motor is attached Low pressure filter blockage indicator - make sure that it has not come out. If indicator found out, do the inspection/checkprocedure, AMM 12-A-29-10-04-00A313A-A Hydraulic system, MSN 101-230 - check fluid sensor and level using maintenance switch box. Fill as necessary, AMM 12-A-29-00-00-00A-902A-A. MSN 231-999 - make sure fluid level indicator on the reservoir tank shows full. Fill as necessary, AMM 12-A-2900-00-00A-902B-A Nitrogen accumulator - check nitrogen pressure and fill as necessary, AMM 12-A-29-10-02-00A-901A-A Reservoir tank - make sure nitrogen pressure is correct. Pressurize as necessary MSN 101-230, AMM 12-A-29-00-00-00A-902A-A MSN 231-999, AMM 12-A-29-00-00-00A-902B-A Power pack electric motor shaft seal drain fluid collector bottle (Post SB 29-002 and MSN 181-999) - remove, clean and re-install Ice and Rain Protection Wing and horizontal stabilizer airfoil de-ice boots inspection/check, AMM 12-A-30-10-00-00A-313A-A FECHA: 16-JUNIO-2014
INTERVAL
Annual Inspection Annual Inspection Annual Inspection
Annual Inspection
Annual Inspection Annual Inspection Annual Inspection
Annual Inspection
Annual Inspection
Annual Inspection
Annual Inspection
Annual Inspection
Annual Inspection
Annual Inspection
PAG: A2.53
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Ac No. Chapt/Task 30-10/155
30-10/260 30-20/261 30-20/156 30-30/157
30-40/262 30-60/158 30-60/159
32-10/163 32-10/162 32-10/164 32-10/263 32-10/165 32-10/264
32-20/168
32-20/167 32-20/169 32-20/265 32-20/166
REVISIÓN: ORIGINAL
AF Hrs. Item Inertial separation system - operational test. MSN 101-320 and 322-400, AMM 12-A-30-20-00-00A903A-A MSN 321 and 401-999, AMM 12-A-30-20-00-00A-903B-A Airfoil de-ice system - functional test, AMM 12-A-30-10-0000A-903A-A Air by-pass door and operating mechanism - examine and lubricate with minimum quantity of P10-001 Engine air intake de-ice lip - look for signs of gas leaks none are permitted Probes de-ice system - operational test. Single P-S system, AMM 12-A-30-30-10-00A-903A-A Dual system and P-S indicator, AMM 12-A-30-30-20-00A903A-A MSN 321 and 401-999, AMM 12-A-30-30-20-00A-903B-A Windshield de-ice system - operational test, AMM 12-A-3040-00-00A-903A-A or 12-A-30-40-00-00A-903B-A Propeller de-ice system - inspection/check, AMM 12-A-3060-00-00A-313A-A Propeller de-ice system - operational test, AMM 12-A-3060-00-00A-903A-A Landing Gear Main landing gear legs – examine Main landing gear - for lubrication, AMM 12-A-12-20-0400A-902A-A Main landing gear compartments – examine Main landing gear electrical bonding straps – examine Main landing gear shock struts - check nitrogen pressure, AMM 12-A-32-10-00-00A-902A-A Main landing gear left and right axle bolt (Pre SB 32-006) remove and examine. Replace if damaged. Install a serviceable bolt Nose landing gear leg and steering mechanism - examine, in particular the steering rod end (Part No. 532.20.12.134) for the complete retention of bearing into the steering rod end housing. Nose landing gear - for lubrication, AMM 12-A-12-20-0400A-902A-A Nose landing gear compartment – examine Nose landing gear electrical bonding straps – examine Nose landing gear leg shock strut - check nitrogen pressure, AMM 12-A-32-20-00-00A-902A-A FECHA: 16-JUNIO-2014
INTERVAL
Annual Inspection
Annual Inspection Annual Inspection Annual Inspection
Annual Inspection
Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection
Annual Inspection
Annual Inspection Annual Inspection Annual Inspection Annual Inspection
PAG: A2.54
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Ac No. Chapt/Task 32-20/266
32-20/305
32-30/170
32-40/171 32-40/172 32-40/173 32-40/174 32-40/175
32-40/176
33-40/177
33-41/178 33-42/179 33-43/180 33-44/181 33-46/182 34-00/183 34-00/184 34-11/268
34-11/185 34-11/186
REVISIÓN: ORIGINAL
AF Hrs. Item Nose landing gear spring strut Part No. 532.20.12.250 remove, clean and lubricate, AMM 12-A-32-20-03-00A920A-A and 12-A-32-20-03-00A-250A-A Nose landing gear actuator fuselage attachment fitting (Part No. 553.10.12.326) - examine, if cracks are found replace attachment fitting, SRM 12-A-53-00-01-00A-663A-A Extension and retraction system - functional test of extension and retraction system and emergency extension system, AMM 12-A-32-30-00-00A-903A-A Mainwheels - examine. Rotate wheels, make sure bearing movement is smooth and free and no excessive play exists Mainwheel tires - examine and check tire pressure, AMM 12-A-12-10-04-00A-902A-A Nosewheel - examine. Rotate wheel, make sure bearing movement is smooth and free and no excessive play exists Nosewheel tire - examine and check tire pressure, AMM 12-A-12-10-04-00A-902A-A Brake system - apply the parking brake. Examine the brake units. Make sure that pad wear indicators protrude from housing. Fluid reservoir - replenish if necessary, AMM 12-A-12-1002-00A-902A-A Lighting Exterior lighting - operational test. MSN 101-320 and 322-400, AMM 12-A-33-40-00-00A903A-A MSN 321 and 401-999, AMM 12-A-33-40-00-00A-903B-A Landing lights – examine Taxi lights – examine Navigation and strobe lights – examine Recognition lights (if installed) – examine Beacon lights (if installed) – examine Navigation Communications and navigation antennas – examine Cockpit instruments and avionic equipment – examine Single pitot and static system - drain, AMM 12-A-34-11-0000A-040A-A Dual pitot static systems - drain, AMM 12-A-34-11-20-00A901A-A Pitot-tubes – examine Static ports – examine Oxygen FECHA: 16-JUNIO-2014
INTERVAL
Annual Inspection
Annual Inspection
Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection
Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection
PAG: A2.55
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Ac No. Chapt/Task 35-10/187 35-10/269 35-10/270
52-10/271 52-10/189 52-10/190 52-10/192
52-10/191 52-20/272 52-30/273 52-30/274 52-30/193 52-30/194
52-30/195 52-70/275
53-00/196
53-00/276 53-00/277
53-00/278 53-00/279 REVISIÓN: ORIGINAL
AF Hrs. Item High pressure relief indicator (green disk) – make sure that it is not damaged Oxygen pipelines and equipment – examine Oxygen system - operational tests, AMM 12-A-35-00-0000A-903A-A Doors Passenger/crew door, counterbalance and cable support brackets – examine Passenger/crew door seal - clean with a wet cloth, dry and examine and apply French chalk (Pt. No. P09-002) Passenger/crew door shoot bolts and door frame fittings examine Passenger/crew door hinges - examine and lubricate as necessary with minimum quantity of CPC temporary (Pt. No. P10-001) Passenger/crew door handle lock pin - make sure movement is free Emergency door - examine (door removed) Emergency door seal - clean with a wet cloth, dry, examine and apply material French chalk (Pt. No. P09-002) Cargo door – examine Cargo door seal - clean with a wet cloth, dry and examine and apply French chalk (Pt. No. P09-002) Cargo door shoot bolts, door frame fittings and hooks examine. Make sure the hook roller bushes are free to rotate. For roller bush wear limits refer to AMM 12-A-5230-00-00A-313A-A Cargo door hinges - examine and lubricate as necessary with minimum quantity of CPC-temporary (Pt. No. P10-001) Door warning system - operational test, AMM 12-A-52-7000-00A-903A-A Fuselage Fuselage external surface - examine. For aircraft that experience stone damage to the belly skin, visually examine affected areas for cracks. Rear pressure bulkhead – examine Floor top and bottom surface and seat rails – examine as far as possible with carpet and floor panels in item 0600/218 removed Baggage/freight net mounting plates attachment bolts and surrounding structure - examine for corrosión Baggage compartment – examine FECHA: 16-JUNIO-2014
INTERVAL
Annual Inspection Annual Inspection Annual Inspection
Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection
Annual Inspection
Annual Inspection Annual Inspection
Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection PAG: A2.56
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Ac No. Chapt/Task 53-00/280
53-00/337
55-10/197 55-10/319 55-30/198
55-30/199
55-30/281 56-10/200 56-20/201
57-00/202 57-00/282 57-00/283 57/00/284 61-10/203 61-10/285
61-20/286
71-00/205
71-00-301
REVISIÓN: ORIGINAL
AF Hrs. Item Rear fuselage internal structure - examine as far as possible, in particular examine battery mounting tray for corrosión Carry through frames 21 and 24 - Inspection/Check, AMM 12-A-53-20-02-00A-313A-A Stabilizers Horizontal stabilizer external surface – examine Horizontal/vertical stabilizer attachment Inspection/Check, AMM 12-A-55-00-00-00A-361A-A Vertical stabilizer external surface - examine, specially around rear spar top rivets. If cracks are found refer to SRM 12-A-55-00-01-00A-664A-A for repair procedure Vertical stabilizer rear spar strap and lower aft fairing shear plate (Pre SB 55-002) - examine, if wear is found refer to SB 55-002 Vertical stabilizer electrical bonding straps – examine Windows Windshield LH and RH - examine, AMM 12-A-56-00-00-00A313A-A Cockpit and cabin windows - examine, AMM 12-A-56-0000-00A-313A-A Wing Wing external surfaces – examine Wing tip static dischargers – examine Wing internal surfaces and flap compartment – examine as far as possible with panels in item 06-00/218 removed Wing to fuselage attachments - examine as far as Posible Propeller Propeller blades - examine. Repair blades as necessary Ref. Hartzell MM Propeller hub - remove spinner dome and examine propeller hub. Install spinner dome, AMM 12-A-61-10-0100A-920A-A Propeller governor, overspeed governor and beta controls examine Power Plant Engine tubular mounting frame and shockmounts examine. Replace shockmount if cracks in elastomer are more than 1 in (25,4 mm) long and/or 0.06 in (1,5 mm) deep Engine tubular mounting frame firewall attachment fittings - examine with firewall insulation blanket removed as FECHA: 16-JUNIO-2014
INTERVAL
Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection
Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection
Annual Inspection
Annual Inspection PAG: A2.57
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Ac No. Chapt/Task
71-00/206
71-00/209
74-00/288
76-00/210 76-00/211 76-00/304 76-00/303
78-00/214 79-00/215
79-20/289 79-30/290 Job Close Up 25-10/297
25-20/299 06-00/219
REVISIÓN: ORIGINAL
AF Hrs. Item necessary. If cracked, blistered or flaking paint is found on the mounting frame refer to SRM 12-A-54-20-00-00A-663AA Power plant and accessories - examine. Refer to P&WC EMM 72-00-00 Periodic inspection and do the 100 hour and minor inspection items Engine drain mast and tank - for fuel leaks (no leaks permitted) and drain (no excessive leaks) Ignition Ignition system - operational test, AMM 12-A-74-00-0000A-903A-A Engine Controls Engine controls in engine compartment – examine Beta slip ring carbon block - make sure gap is not more than 0.01in (0.25mm) Cockpit control quadrant - examine. Power controls - operational test, AMM 12-A-76-10-0000A-903A-A Manual override - operational test, AMM 12-A-76-20-0000A-903A-A Exhaust Exhaust stubs – examine Oil Oil filler cap/dipstick - energize aircraft electrical system, AMM 12-A-24-00-00-00A-901A-A. Remove filler cap, examine and make sure the seal is in good condition. Set and hold AIR/GROUND switch to GROUND and make sure after 60 seconds the CAWS OIL QTY caption comes on. Install filler cap and make sure the locking mechanism operates correctly. Engine oil cooler - examine. Make sure outlet door has full and free movement Oil system chip detector indication system - operational test, AMM 12-A-79-30-01-00A-903A-A Crew seats - install MSN 101-660, AMM 12-A-25-10-01-00A-920A-A MSN 661-999, AMM 12-A-25-10-05-00A-920A-A Passenger seats - install, AMM 12-A-25-20-01-00A-920A-A, 12-A-25-21-01-00A-920A-A, 12-A-25-22-01-00A-920A-A Close/install the following panels:11AL, 11AR, 11BL, 11BR, 12AB, 12BB, 12AL, 12AR, 12AZ, 12BB, 12BL, 12BR, 12BZ, FECHA: 16-JUNIO-2014
INTERVAL
Annual Inspection Annual Inspection
Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection
Annual Inspection Annual Inspection
Annual Inspection
Annual Inspection Annual Inspection
Annual Inspection Annual Inspection Annual Inspection
PAG: A2.58
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Ac No.
71-10/208 07-10/160 71-00/204 24-30/228 25-60/231 00-00/121 00-00/122
INTERVAL
AF Hrs. Item
Chapt/Task
12CL, 12CR, 12CZ, 12DZ, 12EL, 12ER, 12EZ, 12FL, 12FR, 12FZ, 12HZ, 21GZ, 21JZ, 21PZ, 21QZ,31AB, 31AL, 31BL, 32AB, 32AL, 32BL, 32BT, 32CL, 32CT, 32DL, 33ET, 41AT, 42AT, 42AB, 51KB, 51MB, 51NB, 52KB, 52MB, 52NB, 52OB, 52PB, 52RB, 52TB, 52SB, 61KB, 61MB, 61NB, 62KB, 62MB, 62NB, 62OB, 62PB, 62RB, 62SB, 62TB. Engine cowlings ENG43AL and ENG 43AR – close Aircraft - lower to the ground and remove the jacks, AMM 12-A-07-10-00-00A-901A-A Power plant - post inspection ground run, AMM 12-A-7100-00-00A-903A-A External power - operational test, AMM 12-A-24-30-0000A-903A-A or 12-A-24-30-00-00A-903B-A ELT - operational test, AMM 12-A-25-63-01-00A-920A-A Airworthiness Directives and Service Bulletins reviewed and complied with as required Chapter 4 and Chapter 5 - Overhaul and Replacement Schedule, and Time Limited Inspection Requirements sections reviewed and any additional requirements are complied with
Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection
Annual Inspection
OVERHAUL AND REPLACEMENT SCHEDULE - SCHEDULED INSPECTIONS Procedure 1 Overhaul and Replacement Schedule COMPONENT
DISCARD INTERVAL
Chapter 24 - Electrical Power Starter-generator P/N 978.91.23.421 REVISIÓN: ORIGINAL
OVERHAUL INTERVAL
1000 flying hours
FECHA: 16-JUNIO-2014
PAG: A2.59
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 COMPONENT P/N 978.91.23.422 P/N 978.91.23.431 P/N 978.91.23.433 P/N 978.91.23.441 Generator 2 drive assembly aft bearing (smaller inner diameter) (Pre SB 24-010) Generator 2 drive assembly aft bearing (smaller inner diameter) (Post SB 24-010 and MSN 231-999) Chapter 25 - Equipment and Furnishings ELT battery Crew seat cushion (Part No.0A318-0203 installed on IPECO Seat Part No's. 959.30.01.135 and 136) Crew seat belts Passenger seat belts and extensions Chapter - 26 Fire Protection Fire extinguisher Chapter 27 - Flight controls Flap power drive unit (Part No’s 978.73.20.001 and 002) Flap power drive unit (Part No 978.73.20.003) Flap linear actuators (white colored) (Part No’s 978.73.20.302/303/304/305 and 306) Flap linear actuators (black anodized) (Part No’s 978.73.20.307/308 and 309) Flap flexible drive shafts (Part No’s 945.02.02.203/204/205 and 206) Chapter 28 – Fuel Engine driven pump Chapter 31 - Indicating/Recording MSN 321 and 401-999. CAWS CACU clock battery Chapter 61 – Propeller Propeller Chapter 71 - Power plant Engine shock mount assemblies
DISCARD INTERVAL
OVERHAUL INTERVAL
10000 flying hours 3000 flying hours
After one hour of use or as shown on the battery label 3 years (elapsed for factory new or spare part new from EASA Form 1 date) -
12 years (elapsed) 12 years (elapsed) 12 months contents check (elapsed)
4500 flying hours since new or last overhaul -
10000 flying hours or 13500 landings whichever comes first
4500 flying hours
5000 flying hours or 7000 landings whichever comes first 10000 flying hours or 13500 landings whichever comes first -
3500 flying hours
2 years (installed)
-
4000 flying hours or 6 years (Ref. Hartzell SL 61) (installed)
-
At engine overhaul, but not later than 5000 flying hours
Chapter 72 – Engine REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.60
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 COMPONENT Engine
DISCARD INTERVAL
3500 flying hours (Ref. P&WC SB 14603, latest revision) Ref. P&WC SB 14603, latest revision
-
Engine accessories
OVERHAUL INTERVAL
-
TIME LIMITED INSPECTION REQUIREMENTS - SCHEDULED INSPECTIONS Procedure 1 Time Limited Inspection Requirements ITEM Aircraft
Chapter 21 - Air Conditioning Cold air unit Heat exchanger matrix Overtemperature switch Duct overtemperature switch Water separator condenser Cabin altitude switch Cabin differential pressure switch Pressurization outflow valve and safety valve Pressurization system Vapor cycle compressor motor drive belt (if Installed)
REVISIÓN: ORIGINAL
INSPECTION REQUIREMENT
INTERVAL
Do the corrosion and corrosion protection inspections (AMM 12-A20-40-00-00A-901A-A)
AMM 12-A-20-40-00-00A-901A-A
Re-oil (AMM 12-A-21-40-01-00A902A-A) Inspection/check (AMM 12-A-21-4001-00A-313A-A) Remove and test (AMM 12-A-21-4006-00A-903A-A) Remove and test (AMM 12-A-21-6005-00A-903A-A) Clean (AMM 12-A-21-40-02-00A250A-A) Functional test (AMM 12-A-21-3007-00A-903A-A) Functional test (AMM 12-A-21-3008-00A-903A-A) Remove and clean (AMM 12-A-2130-01-00A-250A-A) Adjustment/test (AMM 12-A-21-3000-00A-903A-A) Check for tension (AMM 12-A-21-5000-00A-903A-A or 12-A-21-50-0000A-903B-A)
500 flying hours
FECHA: 16-JUNIO-2014
500 flying hours 5 years (installed) 5 years (installed) 500 flying hours 5 years (installed) 5 years (installed) 1500 flying hours or 2 years whichever comes first (installed) 1500 flying hours or 2 years whichever comes first 500 system operating Hours
PAG: A2.61
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 ITEM Vapor cycle compressor motor (if installed) Vapor cycle compressor condenser module (including motor) (if installed)
Chapter 22 - Auto Flight Servo mount (pitch, roll and yaw) Chapter 24 - Electrical Power NiCad battery or batteries (if 2nd battery installed) (Part No. 976.17.31.301) NiCad battery or batteries (if 2nd battery installed) (Part No. 976.17.31.302) Lead acid battery or batteries (if 2nd battery installed)
Starter/generator brushes Generator 2 (Part No. 524.32.12.158 Mod. B) brushes Generator 2 (Part No. 524.32.12.158 Mod. A, Mod. C and above) brushes Generator 2 drive assembly housing (Post SB 24-010 and MSN 231-999) Emergency Power Supply (if installed)
Generator 1 and 2 ground points Battery 1 and 2 (if installed) ground points Emergency Power Supply
ELT Nav Interface Unit Serial Memory Module
REVISIÓN: ORIGINAL
INSPECTION REQUIREMENT Inspection/check (AMM 12-A-21-5003-00A-313A-A) Clean per OSCMM
INTERVAL 500 system operating hours Initially at each scheduled inspection, then based on field experience the interval can be adjusted to a more effective level
Remove for clutch check (AMM 12-A22-10-00-00A-313A-A)
1000 flying hours or 12 months installed, whichever comes first
Remove and service (AMM 12-A-2430-07-00A-920A-A and CMM) Remove and service (AMM 12-A-2430-07-00A-920A-A and CMM) Remove and do a capacity test (AMM 12-A-24-30-07-00A-920A-A and CMM)
100 flying hours or 3 months whichever comes first (installed) 400 flying hours or 12 months whichever comes first (installed) Initially at 1000 flying hours or 12 months (installed) whichever comes first. If capacity above 90% then every 600 flying hours or 6 months. If capacity is between 85% and 90% then every 300 flying hours or 3 months. If capacity is below 85% replace.
Examine for wear (AMM 12-A-24-3001-00A-313A-A) Examine for wear (AMM 12-A-24-3002-00A-313A-A) Inspection/check (AMM 12-A-24-3004-00A-313A-A) Inspection/check (AMM 12-A-24-3004-00A-313A-A) Remove and do a capacity test (AMM 12-A-24-52-51-00A-920A-A and CMM) Examine the corrosion protective layer (AMM 12-A-24-30-00-00A901A-A). Remove and do a capacity test AMM 12-B-24-52-51-00-A-920A-A and CMM Discard
FECHA: 16-JUNIO-2014
200 flying hours 100 flying hours 500 flying hours 1000 flying hours 12 months (installed)
2 years
12 months (installed)
16000 flying hours or 10 years (installed), whichever comes first. Note 1
PAG: A2.62
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 ITEM
INSPECTION REQUIREMENT
INTERVAL Units which have already operated more than the allowed interval must be replaced within 500 flying hours or 6 months, whichever comes first.
Chapter 27 - Flight Controls Bonding leads to all Flight Control Surfaces
Flight control cables including auto pilot and stick pusher cables Rudder control cables tensión
Examine
Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first. 2000 flying hours or 5 years whichever comes first (installed)
Flap actuators (white colored) (Part No’s 978.73.20.302, 303, 304, 305 and 306) Flap actuators (black anodized) (Part No. 978.73.20.307, 308 and 309) Flap actuators (white colored) (Part No’s 978.73.20.302, 303, 304, 305 and 306)
Examine (AMM 12-A-27-00-00-00A313A-A) Check after replacement of any rudder control system cables (Autopilot and/or rudder) AMM 12-A-27-20-00-00A-903A-A Check after replacement of any elevator control system cables (Autopilot, Stick Pusher and/or Elevator) (AMM 12-A-27-30-00-00A903A-A) Remove, clean, inspect and lubricate inner core (AMM 12-A-27-50-0000A-902A-A) Lubricate (AMM 12-A-27-50-00-00A902A-A) Lubricate (AMM 12-A-27-50-00-00A902A-A) Backlash check (AMM 12-A-27-5003-00A-313A-A)
Flap actuators (black anodized) (Part No. 978.73.20.307, 308 and 309)
Backlash check (AMM 12-A-27-5003-00A-313B-A)
Flap electrical system (MSN 101-400 Pre SB 27013)
Do the flap electrical system maintenance practices tests (AMM 12-A-27-50-00-00A-901A-A)
200 flying hours
Operational test MSN 101-105 (AMM 12-A-28-40-00-00A-903A-A) MSN 106-999 (12-A-28-40-00-00A-903B-A)
1000 flying hours or 4 years whichever comes first (installed)
Elevator control cables tensión
Flap flexible drive shafts (Post SB 27-003) (Part No’s 945.02.02.201 and 202)
Chapter 28 – Fuel Fuel low level warning system
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
At the next scheduled inspection, but not later than 150 flying hours
At the next scheduled inspection, but not later than 150 flying hours
2000 flying hours 400 flying hours or 12 months whichever comes first (installed) 150 flying hours or 12 months whichever comes first (installed) 600 flying hours or 800 flights or 12 months whichever comes first (installed) Annual inspection or every 1000 flying hours or 1300 landings whichever comes first (installed)
PAG: A2.63
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 ITEM Fuel cross vent and outward check valve Chapter 30 - Ice and Rain Protection Airfoil de-icers
Chapter 32 - Landing Gear Main and nose wheel bearings Main landing gear axles and bushes (PC-12/45 aircraft) NLG
INSPECTION REQUIREMENT Operational test (AMM 12-A-28-1001-00A-903A-A)
1000 flying hours
Apply a surface coating of Age Master No. 1 in accordance with the manufacturers instructions
6 months (installed)
Lubricate (AMM 12-A-12-20-06-00A902A-A) Inspection/Check (AMM 12-A-32-1000-00A-313A-A)
Overhaul (Ref. CMM 02100)
NLG Steering mechanism Examine AMM 12-A-32-50-00-00A-310A-A
Chapter 34 – Navigation Static system
Altimeter
Standby magnetic compass Attitude Heading Reference System (AHRS) Transponder system (single and dual systems)
Chapter 35 – Oxygen Passenger oxygen masks Chapter 52 – Doors Passenger/Crew Door Piano Hinge REVISIÓN: ORIGINAL
INTERVAL
Tire change or 12 months installed, whichever comes first 2000 flying hours or 12 months whichever comes first (installed) Threshold 25,000 flying hours or 30,000 landings, whichever comes first. Repeat 8,300 flying hours or 10,000 landings or 6 years whichever comes first. Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 8,300 flying hours or 10,000 landings or 6 years whichever comes first.
Leak check Single system (AMM 12A-34-11-10-00A-903A-A) Dual system (AMM 12-A-34-11-20-00A-903A-A) Check calibration at an approved center in accordance with the regulation in force (Ref. FAR Part 91 411) Check swing (AMM 12-A-34-21-0000A-903A-A) Check swing (AMM 12-A-34-25-0000A-903A-A) Functional test (AMM 12-A-34-5400-00A-903A-A) or (12-A-34-54-0000A-903B-A)
2 years
Inspection/check (AMM 12-A-35-2000-00A-313A-A)
3 years (installed)
Eddy Current Inspection
Threshold 32,500 flying hours or
FECHA: 16-JUNIO-2014
2 years (installed)
2 years (installed) 2 years (installed) 2 years (installed)
PAG: A2.64
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 ITEM
INSPECTION REQUIREMENT AMM 12-A-52-00-01-00A-353A-A
Passenger/Crew Door Skin Eddy Current Inspection AMM 12-A-52-10-01-00A-353A-A
Cargo Door Piano Hinge Eddy Current Inspection AMM 12-A-52-30-00-01A-353A-A
Cargo Door Skin Eddy Current Inspection AMM 12-A-52-30-01-00A-353A-A
Passenger/crew door
Examine with trim removed (AMM 12-A-25-21-03-00A-920A-A or 12-A25-22-03-00A-920A-A). Examine the top step area around the insulation mat for corrosion. If corrosion is found, write to Pilatus for a specific repair. Examine door hinge pin and hinges (AMM 12-A-52-10-00-00A313A-A)
Cargo door Examine with trim removed (AMM 12-A-25-21-03-00A-920A-A or 12-A25-22-03-00A-920A-A). Examine door hinge pin and hinges (AMM 12A-52-30-00-00A-313A-A) Chapter 53 – Fuselage Front pressure bulkhead
REVISIÓN: ORIGINAL
Examine with insulation on engine and cockpit sides removed. If insulation on cockpit side is wet, FECHA: 16-JUNIO-2014
INTERVAL 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first. Threshold 25,000 flying hours or 30,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first. Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first. Threshold 25,000 flying hours or 30,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first. Mild Corrosive Environment: 6000 flying hours or 6 years, whichever comes first. (See Note below) Moderate Corrosive Environment: 4000 flying hours or 4 years, whichever comes first. (See Note below) Severe Corrosive Environment: 2000 flying hours or 2 years, whichever comes first. (See Note below) NOTE: Local conditions may be more or less severe. Based on field experience the interval can be adjusted to more or less frequent, until an effective interval can be set. Mild Corrosive Environment: 6000 flying hours or 6 years, whichever comes first. (See Note below) PAG: A2.65
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 ITEM
Fuselage internal bottom surface
Structure around Windows Door frames and emergency exit frame
Rear pressure bulkhead Frame 40
INSPECTION REQUIREMENT
INTERVAL
remove, dry and reinstall insulation Examine frames 10, 21, 24, 36 and frames adjacent to doors and to emergency exit, with insulation removed. If corrosion is found, examine all fuselage bottom surface with insulation removed. If insulation is wet, remove, dry and reinstall insulation Examine Examine. If insulation is installed in the door frames and is wet, remove and discard it (no longer installed on production) Examine with trim removed
Moderate Corrosive Environment: 4000 flying hours or 4 years, whichever comes first. (See Note below) Severe Corrosive Environment: 2000 flying hours or 2 years, whichever comes first. (See Note below) NOTE: Local conditions may be more or less severe. Based on field experience the interval can be adjusted to more or less frequent, until an effective interval can be set. Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first
Eddy Current Inspection AMM 12-A-53-30-02-00A-353A-A Chapter 55 – Stabilizers Horizontal stabilizer internal surfaces and horizontal/vertical stabilizer interface
Examine as far as possible with panels removed
Vertical stabilizer internal surfaces Examine as far as posible with panels removed
Vertical Stabilizer Forward Attachment to Frame 40 Eddy Current Inspection AMM 12-A-55-30-03-00A-353A-A
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
Mild Corrosive Environment: 6000 flying hours or 6 years, whichever comes first. (See Note below) Moderate Corrosive Environment: 4000 flying hours or 4 years, whichever comes first. (See Note below) Severe Corrosive Environment: 2000 flying hours or 2 years, whichever comes first. (See Note below) NOTE: Local conditions may be more or less severe. Based on field experience the interval can be adjusted to more or less frequent, until an effective interval can be set. Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first PAG: A2.66
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 ITEM
INSPECTION REQUIREMENT
Rudder Trim Tab
Chapter 56 – Windows Cockpit side Windows Chapter 57 – Wing Wing internal surfaces and flap compartment Landing gear compartments
Wing to fuselage attachments
Examine AMM 12-A-55-40-04-00A-310A-A
Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first
Inspection/Check (refer to DM 12-A56-11-02-00A-313A-A)
11000 flying hours or 10 years installed, whichever comes first
Examine as far as possible with all wing panels removed Examine, especially main and rear spar parts
Mild Corrosive Environment: 6000 flying hours or 6 years, whichever comes first. (See Note below) Moderate Corrosive Environment: 4000 flying hours or 4 years, whichever comes first. (See Note below) Severe Corrosive Environment: 2000 flying hours or 2 years, whichever comes first. (See Note below) NOTE: Local conditions may be more or less severe. Based on field experience the interval can be adjusted to more or less frequent, until an effective interval can be set. 11000 flying hours or 10 years, whichever comes first
Examine attachment fittings with wings removed (AMM 12-A-57-0000-00A-313A-A)
Aileron Trim Tab Examine AMM 12-A-57-60-04-00A-310A-A
Wing Tips Examine AMM 12-A-57-33-00-00A-310A-A
Wing Skin around drain holes
REVISIÓN: ORIGINAL
INTERVAL
Eddy Current Inspection AMM 12-A-57-20-01-00A-353A-A FECHA: 16-JUNIO-2014
Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first Threshold 25,000 flying hours or 30,000 landings, whichever comes PAG: A2.67
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 ITEM
INSPECTION REQUIREMENT
INTERVAL first. Repeat 2,500 flying hours or 3,000 landings, whichever comes first.
Chapter 61 – Propeller Propeller Chapter 71 - Power Plant Power plant
Oil pressure transducer electrical connector (Pre SB 79-004) Engine torque and stick pusher torque transducers electrical connectors Chapter 76 - Engine Controls Propeller feathering microswitches
Lubricate (AMM 12-A-12-20-05-00A902A-A) Torque Limiter Test Performance Test (AMM 12-A-71-00-00-00A-903A-A, Table 501) Clean (AMM 12-A-71-00-03-00A250A-A) Clean (AMM 12-A-71-00-03-00A250A-A)
400 flying hours or 12 months whichever comes first (installed) 500 flying hours or 12 months whichever comes first (installed). (The tests are part of the power plant Annual Inspection Requirements) 500 flying hours or 12 months whichever comes first (installed) 500 flying hours or 12 months whichever comes first (installed)
Functional test (AMM 12-A-76-103000 flying hours or 12 months 02-00A-903A-A) whichever comes first TABLE 27 TIME LIMITED INSPECTION REQUIREMENTS - RVSM AIRCRAFT Static system Leak check 2 years AMM 12-B-34-11-00-00A-903A-A Transponder system (single and dual system) Functional test 2 years (installed) AMM 12-B-34-54-00-00A-903A-A or 12-B-34-54-00-00A-903B-A or 12-B34-54-10-00A-903A-A or 12-B-34-5410-00A-903B-A Static ports critical area Inspection/check 12 months AMM 12-B-53-30-01-00A-313A-A Static ports plate height Inspection/check 2 years AMM 12-B-34-11-12-00A-313A-A Altitude and vertical speed indication Functional test 2 years AMM 12-B-34-14-00-00A-903B-A
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.68
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45
INSPECTION ENGINES Y PROPELLER PILATUS PC-12/45 ENGINE PRATT & WHITNEY No. DE SERIE PROPELLER HARTZELL No. DE SERIE
PT6A-67B PCE-PR0456 HC-E4A-3D KX-167
Periodic Inspection
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.69
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.70
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.71
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.72
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.73
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.74
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Hot Section Inspection
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.75
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Fault Isolation
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.76
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.77
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.78
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.79
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.80
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.81
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
HOJA DE PRESENTACIÓN
PROGRAMA DE MANTENIMIENTO
AERONAVE: PILATUS PC-12/45
DESARROLLADO CONFORME A LA ISSUE No. 001 REVISIÓN No. 28 de 31/05/2014 DEL “AIRCRAFT MAINTENANCE MANUAL” DEL FABRICANTE, SECCIÓN 4 Y 5
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.1
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45
Índice HOJA DE PRESENTACIÓN .......................................................................................... A2-1 LISTA DE PÁGINAS EFECTIVAS ................................................................................. A2-3 HOJA PARA EL REGISTRO Y CONTROL DE REVISIONES. ..................................... A2-4 INTRODUCCION ............................................................................................................ A2-5 Chapter 04 - AIRWORTHINESS LIMITATIONS ............................................................ A2-6 STRUCTURAL AND COMPONENT LIMITATIONS - AIRWORTHINESS LIMITATIONS .................................................................................................................................... A2-6 Structural Limitations ........................................................................................... A2-6 Component Limitations ........................................................................................ A2-6 Miscellaneous Limitations .................................................................................... A2-7 Component Life ..................................................................................................... A2-8 Inspection Program ............................................................................................... A2-8 Chapter 05 - SCHEDULED/UNSCHEDULED MAINTENANCE SCHEDULED/UNSCHEDULED MAINTENANCE MASTER MAINTENANCE PLAN GENERAL .................................................................................................................... A2-13 100 HOUR INSPECTION - SCHEDULED INSPECTIONS ....................................... A2-42 ANNUAL INSPECTION - SCHEDULED INSPECTIONS ......................................... A2-49 OVERHAUL AND REPLACEMENT SCHEDULE - SCHEDULED INSPECTIONS ..... A2-59 TIME LIMITED INSPECTION REQUIREMENTS - SCHEDULED INSPECTIONS ...... A2-61 INSPECTION ENGINES Y PROPELLER .................................................................... A2-69
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.2
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45
LISTA DE PÁGINAS EFECTIVAS La siguiente es la lista de páginas efectivas del Programa de Mantenimiento aplicable a las aeronaves Marca Pilatus Modelo PC12/45 operada por Pilatus PC12 Center de Mexico, S.A. DE C.V. el poseedor del programa tendrá la obligación de mantenerlo actualizado, para ello revisaran físicamente que el número de páginas coincida con la lista. PAGINA
REVISION
FECHA
PAG. A2-1 PAG. A2-2 PAG. A2-3 PAG. A2-4 PAG. A2-5 PAG. A2-6 PAG. A2-7 PAG. A2-8 PAG. A2-9 PAG. A2-10 PAG. A2-11 PAG. A2-12 PAG. A2-13 PAG. A2-14 PAG. A2-15 PAG. A2-16 PAG. A2-17 PAG. A2-18 PAG. A2-19 PAG. A2-20 PAG. A2-21 PAG. A2-22 PAG. A2-23 PAG. A2-24 PAG. A2-25 PAG. A2-26 PAG. A2-27 PAG. A2-28 PAG. A2-29 PAG. A2-30 PAG. A2-31 PAG. A2-32 PAG. A2-33 PAG. A2-34 PAG. A2-35 PAG. A2-36 PAG. A2-37 PAG. A2-38 PAG. A2-39 PAG. A2-40
ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL ORIGINAL
16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAGINA PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG. PAG.
A2-41 A2-42 A2-43 A2-44 A2-45 A2-46 A2-47 A2-48 A2-49 A2-50 A2-51 A2-52 A2-53 A2-54 A2-55 A2-56 A2-57 A2-58 A2-59 A2-60 A2-61 A2-62 A2-63 A2-64 A2-65 A2-66 A2-67 A2-68 A2-69 A2-70 A2-71 A2-72 A2-73 A2-74 A2-75 A2-76 A2-77 A2-78 A2-79 A2-80
REVISION
FECHA
16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014
16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014 16-JUNIO-2014
PAG: A2.3
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45
HOJA PARA EL REGISTRO Y CONTROL DE REVISIONES. REGISTRO Y CONTROL DE REVISIONES
No. DE REVISIÓN
FECHA
FECHA DE INSERCIÓN
INICIALES
ORIGINAL 1 2 3 4 5 6 7 8 9 10
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.4
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45
INTRODUCCION El programa de mantenimiento para la aeronave Pilatus PC-12/45 indicado por el fabricante presenta dos opciones de aplicación, de acuerdo al número de horas de vuelo acumuladas durante un año, si se vuela un alto número de horas durante el año, se recomienda la utilización del programa de inspección progresiva, el cual se divide en 28 “Work Cards”, seis fases y las inspecciones “mini”. Para el caso especifico de las aeronaves de Pilatus PC-12 Center de México, el promedio de horas anuales voladas es bajo, por lo que se opto por el programa de mantenimiento estándar, que consta de una inspección a las 100 horas y una inspección anual. En ambos casos, el programa de mantenimiento es complementado con el control de componentes limitados por tiempo de vida y las inspecciones especiales. TOLERANCIAS PERMISIBLES. 1. Intervalos basados en horas de vuelo: a. Intervalos de 100 horas de vuelo o menos + 10 horas de vuelo. b. Intervalos de más de 100 horas de vuelo + 10 % pero no más de 50 horas de vuelo. 2. Intervalos basados en tiempo calendario a. Intervalos de 1año o menos + 10 % pero no más de un mes. b. Intervalos de más de 1 año + 10 % pero no más de 6 meses. 3. Intervalos basados en ciclos a. Menos de 500 ciclos: + 10 % pero no más de 25 ciclos. b. Más de 500 ciclos: + 10 % pero no más de 500 ciclos. La utilización de las extensiones aquí indicadas no implica que se recorran los tiempos de aplicación de las siguientes inspecciones, sino que se utilizarán los tiempos originales sin contar la extensión aplicada. Estas tolerancias podrán ser aplicadas conforme lo señalado solamente PREVIA AUTORIZACIÓN POR PARTE DE LA DGAC.
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.5
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45
Chapter 04 - AIRWORTHINESS LIMITATIONS
STRUCTURAL AND COMPONENT LIMITATIONS - AIRWORTHINESS LIMITATIONS
Structural Limitations STRUCTURE
LIFE
Fuselage and associated structure
Pre SB 04-009 20,000 flying hours or 27,000 landings, whichever comes first Post SB 04-009 25,000 flying hours or 30,000 landings, whichever comes first Wing structure Pre SB 04-009 20,000 flying hours or 27,000 landings, whichever comes first Post SB 04-009 25,000 flying hours or 30,000 landings, whichever comes first Tail structure Pre SB 04-009 20,000 flying hours or 27,000 landings, whichever comes first Post SB 04-009 25,000 flying hours or 30,000 landings, whichever comes first Beyond 25,000 flying hours or 30,000 landings (whichever comes first) refer to the Supplemental Structural Inspection Document (SSID) at Para 5 and 12-A-05-20-30-00A-280A-A for supplemental structural inspections.
Component Limitations COMPONENT
LIFE
Engine rotor components Engine mounting frame
P&WC SB 14002 (latest revision) Pre SB 04-009 20,000 flying hours or 27,000 landings, whichever comes first Post SB 04-009 25,000 flying hours or 30,000 landings, whichever comes first Beyond 25,000 flying hours or 30,000 landings (whichever comes first) refer to the Supplemental Structural Inspection Document (SSID) at Para 5 and 12-A-05-20-30-00A-280A-A for supplemental structural inspections. Engine mounting frame, replace all bolts, 11,000 flying hours washers and nuts Pitch trim actuator 20,000 flying hours or 27,000 landings, whichever comes first Flap actuator (Part No. 978.73.20.307, 308 20,000 flying hours or 27,000 landings, whichever comes first and 309) (black anodized) Fire extinguisher 10 years (elapsed). See Note 1 below. REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.6
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 COMPONENT
LIFE
Oxygen bottle 15 years (elapsed) NLG drag link right part (Part No. 4,000 landings 532.20.12.140) (Pre SB 32-014) Cargo door lower lug fittings (Qty 3) 13,000 flying hours or 17,000 landings, whichever comes first Pitch trim actuator attachment parts, fail safe plates and their attachment parts (IPC 12-20-00-07). Refer to AMM 12-A-27-40-02- 10,000 flying hours 00A-920A-A for fail safe plate removal/installation. Nose landing gear torque tube (P/N 532.50.- 11,000 flying hours or 15,000 landings or 10 years installed, 12.047) whichever comes first. Note 1: Fire extinguishers that are 10 years or older must be replaced by 30 June 2013.
Miscellaneous Limitations COMPONENT
LIMITATION
PROCEDURE
Cockpit outer side, DV Windows and cabin windows Cockpit inner and outer side, DV windows and cabin windows Windshield LH and RH
If cracked or stress crazing can be felt
Replace
If chipped, cracked (only for inner side windows), scratched, bubbles or delaminated If cracked in inner lamination If cracked in outer lamination
Refer to AMM 12-A-56-00-00-00A-313A-A for limitations
Horizontal stabilizer trim
Every 3,000 flying hours or at Annual Inspection, whichever comes first
NLG drag link right part (P/N 532.20.12.140)
Initially 2,000 flying hours or 2,500 landings (installed) whichever comes first, then every 300 flying hours or 400 landings, whichever comes first. Refer to AVOX Service Information Letter SIL-35-114 latest revision (www.avoxsys.com).
Oxygen bottle
Pitch trim actuator (Part No. 978.73.14.202 and 978.73.14.203) Wing Main Spar Fastener REVISIÓN: ORIGINAL
Replace Only unpressurized flight is permitted up to the next scheduled inspection providing it does not cause visual problems Functional test of Trim Runaway Aural Warning System (FAA CMR) in accordance with AMM 12A-27-40-00-00A-903A-A Inspection/check (refer to AMM 12-A-32-20-0600A-313A-A). Hydrostatic test. Refer to AVOX Service Information Letter SIL-35-114 latest revision (www. avoxsys.com).
5,000 flying hours or 5 years (installed) whichever comes First
Overhaul
Threshold 16000 wing flying hours or
Eddy current inspection, AMM 12-A-57-20-10-
FECHA: 16-JUNIO-2014
PAG: A2.7
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 COMPONENT Holes Strap Rib 6
LIMITATION
PROCEDURE
22500 wing landings, whichever comes first. All wings with no landing records must apply a calculated applicable landings equal to 2 x flying hours. See Notes 1 and 2 below.
00A-353D-A No cracks are permitted. If you find cracks contact Pilatus Aircraft for advice.
Note 1 The inspection is applicable to all aircraft except MSN 170, 222, 233, 234, 237, 240, 244, 250 and 324 which have performed the inspection as part of a fleet leader inspection survey and aircraft that have performed Service Bulletin 04-009 Revision 1 or later Note 2 Wings with more than 15500 flying hours or 22000 landings, whichever comes first, must perform the inspection within the next 500 flying hours or 500 landings, whichever comes first
Component Life TASK NO.
27-50/414 55-10/415 32-20/416 32-30/417 29-10/418
COMPONENT
LIFE (WHICHEVER COMES FIRST) FLYING LANDINGS HOURS
Flaps - Life Limit (discard) Horizontal Stabilizer - Life Limit (discard) NLG Drag Link - Life Limit (discard) MLG Actuator - Life Limit (discard) Nitrogen accumulator - Life Limit (discard)
25,000 25,000 25,000 25,000 25,000
30,000 30,000 30,000 30,000 30,000
Inspection Program TASK NO.
32-10/345 32-10/346 32-10/347
INSPECTION/REFERENCE
Main landing gear – Overhaul CMM 02099 Inspection kit P/N 500.60.12.027 MLG Yoke fitting lugs - Eddy Current Inspection CMM 02099 MLG Trailing Link - Eddy Current Inspection
REVISIÓN: ORIGINAL
Threshold (whichever comes first) flying landings hours
LIFE (WHICHEVER COMES FIRST) flying landings Years hours
25,000
30,000
8,300
10,000
25,000
30,000
8,300
10,000
25,000
30,000
8,300
10,000
FECHA: 16-JUNIO-2014
6
PAG: A2.8
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
52-10/348
52-20/349 52-30/350 53-00/351
53-00/352
53-00/353
53-00/354
53-00/355 53-00/356
53-00/357
53-00/358
53-00/359
53-00/360
53-00/361
55-20/362 27-30/363
27-30/364 27-30/365
INSPECTION/REFERENCE
CMM 02099 Passenger/crew door - Examine all structural elements AMM 12-A-52-10-00-00A-310A-A Emergency door - Examine all structural elements AMM 12-A-52-20-00-00A-310A-A Cargo door - Examine all structural elements AMM 12-A-52-30-00-00A-310A-A Upper Longerons Frame 10 - Eddy Current Inspection AMM 12-A-53-10-06-01A-353A-A Inspection kit P/N 500.60.12.032 Fuselage Frames 10 to 16 - Examine all structural elements AMM 12-A-53-10-00-00A-310A-A Inspection kit P/N 500.60.12.033 Fuselage Frames 16 to 36 - Examine all structural elements AMM 12-A-53-20-00-00A-310A-A Inspection kit P/N 500.60.12.041 Fuselage Frames 36 to 43 - Examine all structural elements AMM 12-A-53-30-00-00A-310A-A Antenna Structure - Examine AMM 12-A-53-00-00-00A-310A-A Antenna - Bottom fuselage skin - Eddy Current Inspection AMM 12-A-53-00-00-00A-353A-A Antenna - Upper fuselage skin - Eddy Current Inspection AMM 12-A-53-00-00-00A-353A-A Upper Flange Carry Through Frames 21 and 24 Examine AMM 12-A-53-20-02-00A-310A-A Inspection kit P/N 500.50.12.327 Frames 21 and 24 Wing Attachments - Eddy Current Inspection AMM 12-A-53-20-02-00A-353A-A Frames 21 and 24 Side Frame Attachments - Eddy Current Inspection AMM 12-A-53-20-02-00A-353A-A Frames 41 and 43 Stabilizer Attachment - Eddy Current Inspection AMM 12-A-53-30-02-00A-353A-A or AMM 12-A-55-30-03-00A-353A-A Elevator - Examine AMM 12-A-55-20-00-00A-310A-A Elevator - Control System - Examine AMM 12-A-27-30-00-00A-310A-A Inspection kit P/N 500.50.12.319 Elevator Control Rods - Eddy Current Inspection AMM 12-A-27-00-01-00A-353A-A Elevator Control Rods - Magnetic Particle Inspection
REVISIÓN: ORIGINAL
Threshold (whichever comes first) flying landings hours
LIFE (WHICHEVER COMES FIRST) flying landings Years hours
32,500
42,000
12,500
15,000
6
32,500
42,000
12,500
15,000
6
32,500
42,000
12,500
15,000
6
25,000
30,000
12,500
15,000
32,500
42,000
12,500
15,000
6
32,500
42,000
12,500
15,000
6
32,500
42,000
12,500
15,000
6
32,500
42,000
12,500
15,000
6
28,300
37,000
8,300
10,000
32,500
42,000
12,500
15,000
30,000
39,000
10,000
12,000
30,000
39,000
10,000
12,000
30,000
39,000
10,000
12,000
32,500
42,000
12,500
15,000
32,500
42,000
12,500
15,000
6
32,500
42,000
12,500
15,000
6
32,500
42,000
12,500
15,000
32,500
42,000
12,500
15,000
FECHA: 16-JUNIO-2014
6
PAG: A2.9
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
27-30/366 55-20/367 55-20/368 55-30/369
55-30/370
55-30/371
55-30/372
55-40/373 27-20/374
27-20/375 27-20/376 55-40-377 56-11/378
57-00/379
57-00/380
57-00/382
57-00/383
INSPECTION/REFERENCE
AMM 12-A-27-00-01-00A-352A-A Elevator Control Lever - Eddy Current Inspection AMM 12-A-27-30-05-00A-353A-A Elevator Drive Lever - Eddy Current Inspection AMM 12-A-55-20-01-00A-353A-A Elevator Hinges - Eddy Current Inspection AMM 12-A-55-20-01-00A-353A-A Vertical Stabilizer - Examine AMM 12-A-55-30-00-00A-310A-A Inspection kit P/N 500.50.12.325 Vertical Stabilizer Main and Rear Spar Attachment to Fuselage - Eddy Current Inspection AMM 12-A-53-30-02-00A-353A-A or AMM 12-A-55-30-03-00A-353A-A Vertical Stabilizer Main Attachment to Horizontal Stabilizer - Eddy Current Inspection AMM 12-A-55-00-00-00A-353A-A Vertical Stabilizer Pitch Trim Actuator Fitting and Attachment - Eddy Current Inspection AMM 12-A-55-30-02-00A-353A-A Rudder - Examine AMM 12-A-55-40-00-00A-310A-A Rudder Control System - Examine AMM 12-A-27-20-00-00A-310A-A Inspection kit P/N 500.50.12.318 Rudder Bellcranks - Eddy Current Inspection AMM 12-A-27-20-04-00A-353A-A Rudder Cable Quadrant Shear Spigot - Examine AMM 12-A-27-20-05-00A-310A-A Rudder Hinges - Eddy Current Inspection AMM 12-A-55-40-05-00A-353A-A Windshield LH and RH and Cockpit Side Windows Examine with windshield and side windows removed AMM 12-A-56-11-01-00A-310A-A and AMM 12-A-56-11-02-00A-310A-A and AMM 12-A-53-10-16-00A-310A-A Inspection kit P/N 500.50.12.326 Wing - Examine all structural elements Rib 1 to Rib 20 AMM 12-A-57-00-00-00A-310A-A Wing Main and Rear Spar to Fuselage Attachment Eddy Current Inspection AMM 12-A-57-00-03-00A-353A-A and AMM 12-A-57-00-03-01A-353A-A Inspection kit P/N 500.60.12.004 wing attachment Inspection kit P/N 500.60.12.007 double bush Wing Rear Spar at Rib 8 Flap Arm Attachment - Eddy Current Inspection AMM 12-A-57-20-10-00A-353C-A Wing Main Spar Fastener Holes Rib 1 thru Rib 6 -
REVISIÓN: ORIGINAL
Threshold (whichever comes first) flying landings hours
LIFE (WHICHEVER COMES FIRST) flying landings Years hours
32,500
42,000
12,500
15,000
32,500
42,000
12,500
15,000
32,500
42,000
12,500
15,000
32,500
42,000
12,500
15,000
32,500
42,000
12,500
15,000
32,500
42,000
12,500
15,000
32,500
42,000
12,500
15,000
32,500
42,000
12,500
15,000
6
32,500
42,000
12,500
15,000
6
32,500
42,000
12,500
15,000
32,500
42,000
12,500
15,000
32,500
42,000
12,500
15,000
32,500
42,000
12,500
15,000
6
30,000
39,000
10,000
12,000
6
30,000
39,000
10,000
12,000
25,000
30,000
12,500
15,000
25,000
30,000
3,300
4,000
FECHA: 16-JUNIO-2014
6
6
PAG: A2.10
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
57-00/384
57-00/385
27-50/386
27-50/387
27-50/388
27-50/389
27-50/390
27-50-391
27-50/392
57-60/393 27-10/394
27-10/395
INSPECTION/REFERENCE
Eddy Current Inspection AMM 12-A-57-20-10-00A-353A-A Inspection kit P/N 500.60.12.030 or Inspection kit P/N 500.60.12.020 Wing Main Spar Fastener Holes Strap Rib 6 - Eddy Current Inspection AMM 12-A-57-20-05-00A-353A-A Inspection kit P/N 500.60.12.031 or Inspection kit P/N 500.60.12.043 Wing Rear Spar Fastener Holes Rib 2 thru Rib 3 Eddy Current Inspection AMM 12-A-57-20-10-00A-353B-A Flap Mechanism - Examine AMM 12-A-27-51-00-00A-310A-A Inspection kit P/N 500.60.12.021 Inspection kit P/N 500.60.12.022 Inspection kit P/N 500.60.12.023 Inspection kit P/N 500.60.12.024 Inspection kit P/N 500.60.12.025 Flap Drive Arm (not removed) - Eddy Current Inspection AMM 12-A-27-51-00-00A-353A-A Flap Drive Arm (removed) - Eddy Current Inspection AMM 12-A-27-51-01-00A-353A-A AMM 12-A-27-51-02-00A-353A-A AMM 12-A-27-51-03-00A-353A-A Flap Support Arm - Eddy Current Inspection AMM 12-A-27-51-01-00A-353A-A AMM 12-A-27-51-02-00A-353A-A AMM 12-A-27-51-03-00A-353A-A Flap Cove Rib FIttings - Eddy Current Inspection AMM 12-A-27-51-01-00A-353A-A AMM 12-A-27-51-02-00A-353A-A AMM 12-A-27-51-03-00A-353A-A Flap Aft Links - Eddy Current Inspection AMM 12-A-27-51-01-00A-353A-A AMM 12-A-27-51-02-00A-353A-A AMM 12-A-27-51-03-00A-353A-A Flap Bellcranks - Eddy Current Inspection AMM 12-A-27-51-01-00A-353A-A AMM 12-A-27-51-02-00A-353A-A AMM 12-A-27-51-03-00A-353A-A Aileron - Examine AMM 12-A-57-60-00-00A-310A-A Aileron Control System - Examine AMM 12-A-27-10-00-00A-310A-A Inspection kit P/N 500.50.12.314 Inspection kit P/N 500.50.12.315 Inspection kit P/N 500.50.12.316 Inspection kit P/N 500.60.12.015 (MSN 684 - 999) Inspection kit P/N 500.60.12.016 (MSN 684 -999) Aileron Cable Segment - Eddy Current Inspection AMM 12-A-27-10-09-00A-353A-A
REVISIÓN: ORIGINAL
Threshold (whichever comes first) flying landings hours
LIFE (WHICHEVER COMES FIRST) flying landings Years hours
25,000
30,000
3,300
4,000
25,000
30,000
12,500
15,000
30,000
39,000
10,000
12,000
25,000
30,000
2,500
3,000
30,000
39,000
10,000
12,000
30,000
39,000
10,000
12,000
30,000
39,000
10,000
12,000
30,000
39,000
10,000
12,000
30,000
39,000
10,000
12,000
32,500
42,000
12,500
15,000
6
32,500
42,000
12,500
15,000
6
32,500
42,000
12,500
15,000
FECHA: 16-JUNIO-2014
6
PAG: A2.11
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
27-10/396 27-10/397 27-10/398
27-30/400 71-00/401
INSPECTION/REFERENCE
Aileron Control Rods - Eddy Current Inspection AMM 12-A-27-00-01-00A-353A-A Aileron Control Rods - Magnetic Particle Inspection AMM 12-A-27-00-01-00A-352A-A Aileron Bellcranks - Eddy Current and Magnetic Particle Inspections AMM 12-A-27-10-08-00A-353A-A AMM 12-A-27-10-08-00A-353B-A AMM 12-A-27-10-08-00A-352B-A Aileron Hinge Points - Eddy Current Inspection AMM 12-A-57-60-06-00A-353A-A Engine Mount - Magnetic Particle Inspection AMM 12-A-71-00-05-00A-352A-A Inspection kit P/N 500.60.12.006
Threshold (whichever comes first) flying landings hours
LIFE (WHICHEVER COMES FIRST) flying landings Years hours
32,500
42,000
12,500
15,000
32,500
42,000
12,500
15,000
32,500
42,000
12,500
15,000
32,500
42,000
12,500
15,000
26,600
35,000
6,600
8,000
SUPPLEMENTAL STRUCTURAL Do these supplemental structural inspections to increase the life of the airframe above more than 25000 flying hours or 30000 landings:
TASK NO.
INSPECTION/REFERENCE
Threshold (whichever comes first) flying landings hours
LIFE (WHICHEVER COMES FIRST) flying landings Years hours
27-00/402
Bonding leads to all Flight Control Surfaces – Examine
32,500
42,000
12,500
15,000
6
32-20/403
NLG - Overhaul CMM 02100 Overhaul Kit P/N 500.60.12.029 NLG Steering Mechanism - Examine AMM 12-A-32-50-00-00A-310A-A Passenger/Crew Door Piano Hinge - Eddy Current Inspection AMM 12-A-52-00-01-00A-353A-A Passenger/Crew Door Skin - Eddy Current Inspection AMM 12-A-52-10-01-00A-353A-A Cargo Door Piano Hinge - Eddy Current Inspection AMM 12-A-52-30-00-01A-353A-A Cargo Door Skin - Eddy Current Inspection AMM 12-A-52-30-01-00A-353A-A Frame 40 - Eddy Current Inspection AMM 12-A-53-30-02-00A-353A-A Vertical Stabilizer Forward Attachment to Frame 40 Eddy Current Inspection AMM 12-A-55-30-03-00A-353A-A Rudder Trim Tab - Examine
25,000
30,000
8,300
10,000
6
32,500
42,000
8,300
10,000
6
32,500
42,000
12,500
15,000
25,000
30,000
12,500
15,000
32,500
42,000
12,500
15,000
25,000
30,000
12,500
15,000
32,500
42,000
12,500
15,000
32,500
42,000
12,500
15,000
32,500
42,000
12,500
15,000
32-50/404 52-10/405
52-10/406 52-30/407 52-30/408 53-00/419 55-30/420
55-40/410
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
6
6
6
PAG: A2.12
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
57-60/411
57-00/412 57-00/413
INSPECTION/REFERENCE
AMM 12-A-55-40-00-00A-310A-A Aileron Trim Tab - Examine AMM 12-A-57-60-04-00A-310A-A Inspection kit P/N 500.50.12.317 or Inspection kit P/N 500.60.12.039 and Inspection kit P/N 500.60.12.040 Wing Tips - Examine AMM 12-A-57-33-00-00A-310A-A Wing Skin around drain holes - Eddy Current Inspection AMM 12-A-57-20-01-00A-353A-A
Threshold (whichever comes first) flying landings hours
LIFE (WHICHEVER COMES FIRST) flying landings Years hours
32,500
42,000
12,500
15,000
6
32,500
42,000
12,500
15,000
6
25,000
30,000
2,500
3,000
Chapter 05 - SCHEDULED/UNSCHEDULED MAINTENANCE SCHEDULED/UNSCHEDULED MAINTENANCE MASTER MAINTENANCE PLAN - GENERAL The Master Maintenance Plan lists all maintenance tasks from the Airworthiness Limitations (AL) DM, time limits DM, 100 Hour inspection DM, annual inspection DM and the Progressive Inspection (PI). The tasks are listed in ATA chapter (given in the task number) order. The purpose of this Master Maintenance Plan is to provide the operator/maintainer a complete overview of the maintenance which is applicable for the PC-12/45. This plan is intended as a tool to assist the operator/maintainer in planning. Each task has a unique task number. This number is only used in the Master Maintenance Plan and Progressive Inspection program for task identification.
TASK NO.
ITEMS / DESCRIPTION
00-00/45
Aircraft Do the corrosion and corrosion protection inspections AMM 12-A-20-40-00-00A-901A-A Airworthiness Directives and Service Bulletins reviewed and complied with as required Check Chapter 4 and Chapter 5 - Overhaul and Replacement Schedule and Time Limited Inspection Requirements reviewed and any additional requirements are complied with Check Access panels 42AB, 42AT and 32CT Install Access panels 42AB, 42AT and 32CT Remove Access panels 11AR, 11BL, 11BR, 12AZ, 12AB, 12BB, 12BL, 12BR, 12BZ, 12CL, 12CR, 12CZ, 12DZ,
00-00/121 00-00/122
06-00/119 06-00/123 06-00/218
REVISIÓN: ORIGINAL
INTERVAL/ LIMITATIONS
FECHA: 16-JUNIO-2014
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y Y
PAG: A2.13
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
06-00/219
07-10/160
07-10/161
10-10/428
11-00/220
12-20/124
12-20/125 12-20/126 21-20/127
21-20/221
21-30/46
21-30/47
21-30/48 21-30/49 21-40/50
INTERVAL/ LIMITATIONS
AL
TIME LIMITS
12EL, 12ER, 12EZ, 12FZ, 12HZ, 21GZ, 21JZ, 21PZ, 21QZ, 31AB, 31AL, 31BL, 32AB, 32AL, 32BL, 32BT, 32CL, 33ET, 41AT, 42AT, 42AB, 51KB, 51MB, 51NB, 52KB, 52MB, 52NB, 52OB, 52PB, 52RB, 52TB, 52SB, 61KB, 61MB, 61NB, 62KB, 62MB, 62NB, 62OB, 62PB, 62RB, 62SB, 62TB Open/remove and examine. Make sure the drain holes are clear. AMM 12-A-06-20-00-00A-040A-A Access panels 11AR, 11BL, 11BR, 12AZ, 12AB, 12BB, 12BL, 12BR, 12BZ, 12CL, 12 CR, 12CZ, 12DZ, 12EL, 12ER, 12EZ, 12FZ, 12HZ, 21GZ, 21JZ, 21PZ, 21QZ, 31AB, 31BL, 32AL, 32AB, 32AL, 32BL, 32BT, 32CL, 33ET, 41AT, 42AT, 42AB, 51KB, 51MB, 51NB, 52KB, 52MB, 52NB, 52OB, 52PB, 52RB, 52TB, 52SB, 61KB, 61MB, 61NB, 62KB, 62MB, 62NB, 62OB, 62PB, 62RB, 62SB, 62TB Close or install Aircraft Lower to the ground, remove jacks and disconnect from ground AMM 12-A-07-10-00-00A-901A-A Aircraft Lift on jacks and connect the aircraft to ground AMM 12-A-07-10-00-00A-901A-A External Protective Covers Examine. Replace if any part of the cover is missing, damaged, torn or does not install properly Placards and markings Examine and attach new placards if necessary AMM 12-A-11-20-00-00A-901A-A and 12-A-11-30-00-00A040A-A Aircraft Wash the exterior, including the landing gear and flap compartments AMM 12-A-12-20-01-00A-902A-A Windshields and windows Clean AMM 12-A-12-20-02-00A-902A-A Cockpit and cabin Clean AMM 12-A-12-20-03-00A-902A-A ECS emergency shut-off system ECS EMER shut-off valve - operational test; max pull force 22.5 lbf (100N) and make sure ram air scoop is completely open ECS and bleed air ducts, pipelines, equipment and associated clamps in the engine compartment Examine Pressurization system Adjustment/Test AMM 12-A-21-30-00-00A-903A-A Pressurization outflow valve and safety valve Remove and clean AMM 12-A-21-30-01-00A-250A-A
Cabin altitude switch Functional test AMM 12-A-21-30-07-00A-903A-A Cabin differential pressure switch Functional test AMM 12-A-21-30-08-00A-903A-A Water separator condenser
REVISIÓN: ORIGINAL
1500 flying hours or 2 Years whichever comes first 1500 flying hours or 2 Years whichever comes first (installed)
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
5 years (installed)
Y
5 years (installed)
Y
500 flying hours
Y
FECHA: 16-JUNIO-2014
100 HOUR
Y
PAG: A2.14
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
21-40/51 21-40/52 21-40/53
21-40/54
21-40/55 21-40/56 21-40/128
21-50/58 21-50/59
21-50/223 21-50/433
22-10/60
22-10/233
22-20/129 22-20/130 22-20/226 24-20/227 24-30/19
24-30/20
INTERVAL/ LIMITATIONS
Clean AMM 12-A-21-40-02-00A-250A-A Overtemperature switch Functional test AMM 12-A-21-40-06-00A-903A-A Duct overtemperature switch Functional test AMM 12-A-21-60-05-00A-903A-A Secondary heaters thermal protection switches (MSN 101-320 without a modified auxiliary heating system) Operational test AMM 12-A-21-40-09-00A-903A-A Secondary heaters thermal protection switches (MSN 321-999 and aircraft with a modified auxiliary heating system) Operational test AMM 12-A-21-40-00-00A-903A-A Cold air unit Re-oil AMM 12-A-21-40-01-00A-902A-A Heat exchanger matrix Inspection/check AMM 12-A-21-40-01-00A-313A-A Flight compartment foot heater (if installed) thermal protection switch Operational test AMM 12-A-21-40-11-00A-903A-A Vapor cycle compressor motor (if installed) Inspection/check AMM 12-A-21-50-03-00A-313A-A Vapor cycle compressor motor drive belt (if Installed) Check for tension AMM 12-A-21-50-00-00A-903A-A or 12-A-21-50-00-00A-903B-A Vapor cycle cooling system (if installed) Examine the cooling unit Vapor cycle compressor condenser module (including motor) (if installed) Clean per OSCMM
Servo mount (pitch, roll and yaw) Remove for clutch check AMM 12-A-22-10-00-00A313A-A Pitch, roll, and yaw actuators and capstan control cables Examine Angle of Attack (AOA) transmitters Examine Stick pusher system Check AMM 12-A-22-20-00-00A-903A-A Stick pusher system Functional test AMM 12-A-22-20-00-00A-903A-A AC electrical system Operational test AMM 12-A-24-20-00-00A-903A-A Starter/generator Overhaul P/N 978.91.23.421 P/N 978.91.23.422 P/N 978.91.23.431 P/N 978.91.23.433 P/N 978.91.23.441 Generator 2 drive assembly aft bearing (smaller inner
REVISIÓN: ORIGINAL
AL
TIME LIMITS
5 years (installed)
Y
5 years (installed)
Y
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
500 flying hours
Y
Y
500 flying hours
Y
Y
500 Ops Hr
Y
500 Ops Hr
Y
Initially at each scheduled inspection, then based on field experience the interval can be adjusted to a more effective interval 1000 flying hours or 12 months whichever comes first (installed)
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
1000 flying hours
Y
10000 flying hours
Y
FECHA: 16-JUNIO-2014
Y Y
Y
Y
Y
PAG: A2.15
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
24-30/21
24-30/61 24-30/62
24-30/63 24-30/64
24-30/65 24-30/66
24-30/67
24-30/68
24-30/69
24-30/131
24-30/132
24-30/228
24-40/229 24-50/70
INTERVAL/ LIMITATIONS
diameter) (Pre SB 24-010) Discard Generator 2 drive assembly aft bearing (smaller inner diameter) (Post SB 24-010 and MSN 231 - 999) Discard Starter/generator brushes Brush check AMM 12-A-24-30-01-00A-313A-A Generator 1 and 2 ground points Battery 1 and 2 (if installed) ground points Examine the corrosion protective layer AMM 12-A-2430-00-00A-901A-A Generator 2 (Part No. 524.32.12.158 Mod. B) brushes Inspection/check AMM 12-A-24-30-02-00A-313A-A Generator 2 (Part No. 524.32.12.158 Mod. A, Mod. C and above) brushes Inspection/check AMM 12-A-24-30-02-00A-313A-A Generator 2 drive assembly housing (Pre SB 24-010) Inspection/check AMM 12-A-24-30-04-00A-313A-A Generator 2 drive assembly housing (Post SB 24-010 and MSN 231 - 999) Inspection/check AMM 12-A-24-30-04-00A-313A-A NiCad battery or batteries (if 2nd battery installed) (Part No. 976.17.31.301) Remove and service AMM 12-A-24-30-07-00A-920AA and CMM NiCad battery or batteries (if 2nd battery installed) (Part No. 976.17.31.302) Remove and service AMM 12-A-24-30-07-00A-920AA and CMM Lead acid battery or batteries (if 2nd battery installed) Remove and do a capacity test AMM 12-A-24-30-0700A-920A-A and CMM
Generator 2 drive belt Examine and adjustment/test AMM12-A-24-30-0300A-903A-A or 12-A-24-30-03-00A-903B-A Battery (Batteries - if 2nd battery installed) Examine and operational test AMM12-A-24-30-0000A-903A-A or 12-A-24-30-00-00A-903B-A External power Operational test AMM12-A-24-30-00-00A-903A-A or 12-A-24-30-00-00A-903B-A External Power Unit (EPU) receptacle Examine Emergency power supply (if installed) Remove and Cap test AMM 12-A-24-52-51-00A-920A-
REVISIÓN: ORIGINAL
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
3000 flying hours
Y
200 flying hours
Y
2 years
Y
100 flying hours
Y
400 flying hours
Y
500 flying hours
Y
Y
1000 flying hours
Y
Y
Y
Y
Y
Y
Y
Y
100 flying hours or 3 month whichever comes first (installed) 400 flying hours or 12 month whichever comes first (installed) Initially at 1000 flying hours or 12 months (installed) whichever comes first. If capacity above 90% then every 600 flying hours or 6 months. If capacity is between 85% and 90% then every 300 flying hours or 3 months. If capacity is below 85% replace.
12 months (installed)
FECHA: 16-JUNIO-2014
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
PAG: A2.16
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
24-60/133 25-10/134 25-10/135 25-10/230
25-10/293
25-10/294 25-10/296
25-10/297
25-10/300
25-20/136 25-20/137 25-20/295 25-20/298 25-20/299
25-20/302
25-60/231
25-60/232 25-63/23
INTERVAL/ LIMITATIONS
A Cockpit circuit breaker panels and switch panels Examine Crew seat belts Examine Crew seats Examine as far as posible with seats installed Pilots relief tube system (if installed) Clean and leak check AMM 12-A-25-10-05-00A-920AA Crew seat cushion (Part No.0A318-0203 installed on IPECO Seat Part No's. 959.30.01.135 and 136) Discard Crew seat belts Overhaul Crew seats Remove MSN 101-660 AMM 12-A-25-10-01-00A-920A-A MSN 661-999 AMM 12-A-25-10-05-00A-920A-A Crew seats Install MSN 101-660 (AMM 12-A-25-10-01-00A-920A-A MSN 661-999 AMM 12-A-25-10-05-00A-920A-A Crew seats Remove cushions, covers and shells (Ref. CMM) and examine seat. Install cushions, covers and shells. Note: The CMM Document No’s. are given in AMM 12-A-25-10-01-00A-920A-A and 12-A-25-10-05-00A920A-A Passenger seat belts and extensions Examine Passenger seats Examine Passenger seat belts and extensions Overhaul Passenger seats Passenger seats Remove AMM 12-A-25-20-01-00A-920A-A, 12-A-2521-01-00A-920A-A, 12-A-25-22-01-00A-920A-A Install AMM 12-A-25-20-01-00A-920A-A, 12-A-25-2101-00A-920A-A, 12-A-25-22-01-00A-920A-A Passenger seats Examine as far as possible with seats installed. Move the recline mechanism and swivel function (executive seat only) through its full motion and check for correct operation. If necessary, refer to the applicable supplier CMM (CMM 25-20-07 for executive seats and CMM 25-20-99 for standard seats). ELT Operational test AMM12-A-25-63-00-00A-903A-A or 12-A-25-63-10-00A-903A-A or 12-A-25-63-20-00A903A-A or 12-A-25-63-30-00A-903A-A ELT installation Examine ELT battery Discard
REVISIÓN: ORIGINAL
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
3 years (elapsed for factory new or spare part new from EASA Form 1 date)
Y
12 years (elapsed)
Y
Y
12 years (elapsed)
Y Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
After 1 hour of use or as shown on the
FECHA: 16-JUNIO-2014
Y
Y
Y
Y
Y
Y
PAG: A2.17
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
INTERVAL/ LIMITATIONS
25-63/434
ELT Nav Interface Unit Serial Memory Module Discard Note 1Units which have already operated more than the allowed period must be replaced within 500 flying hours or 6 months, whichever comes first. Fire extinguisher Life limit Fire extinguisher Content check Flight control cables including auto pilot and stick pusher cables Inspection/check AMM 12-A-27-00-00-00A-313A-A
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
battery label
26-20/2 26-20/24 27-00/71
27-00/138 27-00/402
27-10/139 27-10/234
27-10/235 27-10/236
27-10/237
27-10/238
27-10/394
Aileron, elevator and rudder controls Operate, make sure full and free travel Bonding leads to all Flight Control Surfaces Examine
Y
10 years (elapsed)
Y
12 months (elapsed)
Y
2000 flying hours or 5 years whichever comes first (installed)
Y
Y
Y Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes firs
Aileron LH and RH Examine Aileron LH and RH rods and levers Examine Spray PTFE Teflon Spray OKS 571 (or equivalent) around the aileron pushrod guide roller sleeves at all three locations in each wing Aileron electrical bonding straps Examine Aileron controls Examine the control cables and pulleys as far as possible. Move the mechanism so that you can see all parts of the cables and make sure the safety clips are fully engaged in the turnbuckles Aileron cable tension Check MSN 101-683 AMM12-A-27-10-00-00A-903A-A MSN 684-999 AMM 12-A-27-10-00-00A-903B-A Ailerons Functional test MSN 101-683 AMM 12-A-27-10-00-00A-903A-A MSN 684-999 AMM 12-A-27-10-00-00A-903B-A Aileron Control System Examine AMM 12-A-27-10-00-00A-310A-A
REVISIÓN: ORIGINAL
16000 flying hours or 10 years whichever comes first (installed)
Y
Y
Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours
FECHA: 16-JUNIO-2014
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
PAG: A2.18
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
27-10/395
27-10/396
27-10/397
27-10/398
27-15/239
27-20/140
27-20/240 27-20/241
INTERVAL/ LIMITATIONS
Aileron Cable Segment Eddy Current Inspection AMM 12-A-27-10-09-00A-353A-A
Aileron Control Rods Eddy Current Inspection AMM 12-A-27-00-01-00A-353A-A
Aileron Control Rods Magnetic Particle Inspection AMM 12-A-27-00-01-00A-352A-A
Aileron Bellcranks Eddy Current and Magnetic Particle Inspections AMM 12-A-27-10-08-00A-353A-A AMM 12-A-27-10-08-00A-353B-A AMM 12-A-27-10-08-00A-352B-A
or 15,000 landings or 6 years, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first
Aileron trim Functional test MSN 101-683 AMM 12-A-27-15-00-00A-903A-A MSN 684-999 AMM 12-A-27-15-00-00A-903B-A Rudder Examine, in particular the cover plate (Part No. 555.40.12.215) on the bottom of the rudder to make sure it is not bent and there are no signs of interference with the rudder stop. Rudder static dischargers Examine Rudder controls Examine the control cables and pulleys as far as possible. Move the mechanism so that you can see all
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
y
Y
PAG: A2.19
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
27-20/242
27-20/243
27-20/244
27-20/245 27-20/246 27-20/374
27-20/375
27-20/376
27-20/431
INTERVAL/ LIMITATIONS
parts of the cables and make sure the safety clips are fully engaged in the turnbuckles Aileron/rudder interconnect system, MSN 101-683 Make sure the locking mechanism is fully engaged with the flaps at 40° and the moving parts (piston and housing) are lubricated. If necessary apply grease P04-002 with a brush. Retract the flaps to 0° and make sure the locking mechanism is fully disengaged. Rudder cable tension Check AMM12-A-27-20-00-00A-903A-A or 12-A-2720-00-00A-903B-A Rudder Functional test AMM12-A-27-20-00-00A-903A-A or 12-A-27-20-00-00A-903B-A Rudder trim Functional test AMM12-A-27-25-00-00A-903A-A Rudder electrical bonding straps Examine Rudder Control System Examine AMM 12-A-27-20-00-00A-310A-A
Rudder Bellcranks Eddy Current Inspection AMM 12-A-27-20-04-00A-353A-A
Rudder Cable Quadrant Shear Spigot Examine AMM 12-A-27-20-05-00A-310A-A
Rudder control cables tension Check after replacement of any rudder control system cables (Autopilot, and/or rudder) AMM 12-A-27-20-00-00A-903A-A
REVISIÓN: ORIGINAL
Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first At the next scheduled inspection, but not later than 150 flying hours
FECHA: 16-JUNIO-2014
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
y
Y
Y
Y
PAG: A2.20
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
27-30/141
Elevators Examine Elevator electrical bonding straps Examine Elevator static dischargers Examine Elevator controls Examine the control cables and pulleys as far as possible. Move the mechanism so that you can see all parts of the cables and make sure the safety clips are fully engaged in the turnbuckles Elevator cable tension Check AMM12-A-27-30-00-00A-903A-A Elevator Functional test AMM12-A-27-30-00-00A-903A-A Elevator control cables tension Check after replacement of any elevator control system cables (autopilot, stick pusher and/or elevator) AMM 12-A-27-30-00-00A-903A-A
27-30/247 27-30/248 27-30/249
27-30/250 27-30/251 27-30/334
27-30/363
27-30/364
27-30/365
27-30/366
Elevator - Control System Examine AMM 12-A-27-30-00-00A-310A-A
Elevator Control Rods Eddy Current Inspection AMM 12-A-27-00-01-00A-353A-A
Elevator Control Rods Magnetic Particle Inspection AMM 12-A-27-00-01-00A-352A-A
Elevator Control Lever Eddy Current Inspection AMM 12-A-27-30-05-00A-353A-A
REVISIÓN: ORIGINAL
INTERVAL/ LIMITATIONS
At the next Scheduled inspection, but not later than 150 flying hours Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat
FECHA: 16-JUNIO-2014
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
y
Y
PAG: A2.21
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
27-30/400
27-40/1
INTERVAL/ LIMITATIONS
Aileron Hinge Points Eddy Current Inspection AMM 12-A-57-60-06-00A-353A-A
Horizontal stabilizer trim Functional test of trim runaway aural warning system (FAA CMR) AMM12-A-27-40-00-00A-903A-A
27-40/3
Pitch trim actuator Life limit
27-40/25 27-40/26
27-40/142
27-40/252
27-40/291
27-40/292
27-40/307
27-50/4
27-50/27
27-50/28
27-50/29
Pitch trim actuator (Part No. 978.73.14.201) Overhaul Pitch trim actuator (Part No. 978.73.14.202 and 978.73.14.203) Overhaul Horizontal stabilizer trim Operational test of trim interrupt and alternate trim switches AMM 12-A-27-40-00-00A-903A-A Horizontal stabilizer trim actuator top and bottom attachments Examine Horizontal stabilizer trim Operational test of trim system AMM 12-A-27-40-0000A-903A-A Horizontal stabilizer trim Functional test of trim system AMM 12-A-27-40-0000A-903A-A Pitch trim actuator attachment parts, fail safe plates and their attachment parts (IPC 12-20-00-07) Life limit Flap actuators (black anodized) (Part No. 978.73.20.307, 308 and 309) Life limit Flap power drive unit (Part No. 978.73.20.001 and 002) Discard Flap power drive unit (Part No. 978.73.20.0-03) Overhaul
Flap actuators (white colored) (Part No’s 978.73.20.302, 303, 304, 305 and 306)
REVISIÓN: ORIGINAL
12,500 flying hours or 15,000 landings, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first 3000 flying hours or at Annual Inspection whichever comes first 20000 flying hours or 27000 landings whichever comes first
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
1500 flying hours
Y
5000 flying hours or 5 years whichever comes first (installed)
y
Y
Y
Y
10000 flying hours 20000 flying hours or 27 000 landings whichever comes first 4500 flying hours since new, or last overhaul 10000 flying hours or 13500 landings whichever comes first 4500 flying hours
FECHA: 16-JUNIO-2014
Y
Y
Y
Y
Y
Y
PAG: A2.22
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
27-50/30
27-50/31
27-50/72
27-50/73
27-50/74
27-50/75
27-50/76
27-50/77
27-50/143 27-50/144
27-50/253 27-50/254 27-50/255
27-50/386
INTERVAL/ LIMITATIONS
Discard Flap actuators (black anodized) (Part No. 978.73.20.307, 308 and 309) Overhaul Flap flexible drive shafts (Part No’s 945.02.02-.203, 204, 205 and 206) Discard Flap flexible drive shafts (Post SB 27-003) (Part No’s 945.02.02.201 and 202) Remove, clean, inspect and lubricate inner core AMM 12-A-27-50-00-00A-902A-A Flap actuators (white colored) (Part No’s 978.73.20.302, 303, 304, 305 and 306) Lubricate AMM 12-A-27-50-00-00A-902A-A Flap actuators (black anodized) (Part No. 978.73.20.307, 308 and 309) Lubricate AMM12-A-27-50-00-00A-902A-A Flap actuators (white colored) (Part No’s 978.73.20.302, 303, 304, 305 and 306) Backlash check AMM12-A-27-50-03-00A-313A-A Flap actuators (black anodized) (Part No. 978.73.20.307, 308 and 309) Backlash check AMM12-A-27-50-03-00A-313B-A
Flap electrical system (MSN 101-400 Pre SB 27-013) Do the flap electrical system maintenance practices tests AMM12-A-27-50-00-00A-901A-A Flaps Lower to 40° Flaps and flap support mechanism - examine. For Flap drive arms, refer to AMM 12-A-27-51-00-00A313A-A. Flaps electrical bonding straps Examine Flap motor, actuators and flexible drive shafts Examine Flaps Functional test and asymmetry monitor test. Pre SB 27-013 AMM 12-A-27-50-00-00A-903A-A Post SB 27-013 and MSN 401-999 AMM 12-A-27-5000-00A-903B-A Flap Mechanism Examine AMM 12-A-27-51-00-00A-310A-A
REVISIÓN: ORIGINAL
AL
5000 flying hours or 7000 landings Whichever comes first 10000 flying hours or 13500 landings Whichever comes first
ANNUAL
PI
Y
Y
400 flying hours or 12 month whichever comes first (installed) 150 flying hours or 12 month whichever comes first (installed) 600 flying hours or 12 month whichever comes first (installed) Annual inspection or 1000 flying hours or 1300 landings whichever comes first (installed)
Y
Y
Y
Y
Y
Y
Y
200 flying hours
FECHA: 16-JUNIO-2014
100 HOUR
Y
2000 flying hours
Threshold 30,000 flying hours or 39,000 landings, whichever comes first. Repeat 10,000 flying hours or 12,000 landings or 6 years, whichever comes
TIME LIMITS
Y Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
PAG: A2.23
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
27-50/387
Flap Drive Arm (not removed) Eddy Current Inspection AMM 12-A-27-51-00-00A-353A-A
27-50/388
27-50/389
27-50/390
27-50/391
27-50/392
Flap Drive Arm (removed) Eddy Current Inspection AMM 12-A-27-51-01-00A-353A-A AMM 12-A-27-51-02-00A-353A-A AMM 12-A-27-51-03-00A-353A-A
Flap Support Arm Eddy Current Inspection AMM 12-A-27-51-01-00A-353A-A AMM 12-A-27-51-02-00A-353A-A AMM 12-A-27-51-03-00A-353A-A
Flap Cove Rib FIttings Eddy Current Inspection AMM 12-A-27-51-01-00A-353A-A AMM 12-A-27-51-02-00A-353A-A AMM 12-A-27-51-03-00A-353A-A
Flap Aft Links Eddy Current Inspection AMM 12-A-27-51-01-00A-353A-A AMM 12-A-27-51-02-00A-353A-A AMM 12-A-27-51-03-00A-353A-A
Flap Bellcranks Eddy Current Inspection AMM 12-A-27-51-01-00A-353A-A AMM 12-A-27-51-02-00A-353A-A AMM 12-A-27-51-03-00A-353A-A
REVISIÓN: ORIGINAL
INTERVAL/ LIMITATIONS first Threshold 25,000 flying hours or 30,000 landings, whichever comes first. Repeat 2,500 flying hours or 3,000 landings, whichever comes first Threshold 30,000 flying hours or 39,000 landings, whichever comes first. Repeat 10,000 flying hours or 12,000 landings, whichever comes first Threshold 30,000 flying hours or 39,000 landings, whichever comes first. Repeat 10,000 flying hours or 12,000 landings, whichever comes first Threshold 30,000 flying hours or 39,000 landings, whichever comes first. Repeat 10,000 flying hours or 12,000 landings, whichever comes first Threshold 30,000 flying hours or 39,000 landings, whichever comes first. Repeat 10,000 flying hours or 12,000 landings, whichever comes first Threshold 30,000 flying hours or 39,000 landings, whichever comes first. Repeat 10,000 flying hours
FECHA: 16-JUNIO-2014
AL
TIME LIMITS
100 HOUR
ANNUAL
Y
Y
Y
Y
Y
Y
PAG: A2.24
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PI
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
INTERVAL/ LIMITATIONS
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
or 12,000 landings, whichever comes first 28-10/145 28-10/146
28-10/306 28-20/32 28-20/147 28-20/148
28-20/149
28-20/150 28-20/256
28-40/78
29-10/151
29-10/152
29-10/153
29-10/257
29-10/258
29-10/259
Fuel tank filler caps Examine Fuel Remove a sample from each drain valve and examine for water Fuel cross vent and outward check valve Operational test AMM12-A-28-10-01-00A-903A-A Engine driven pump Overhaul Fuel tank vent valve and flame arrestor Operational test AMM12-A-28-20-07-00A-903A-A Fuel filter element Remove and clean AMM12-A-28-20-01-00A-920A-A and 12-A-28-20-01-00A-250A-A Firewall shutoff valve Operate FUEL EMERG SHUTOFF lever and make sure firewall shutoff valve opens and closes fully to each dead stop. Make sure movement is free and check if initial pull out force at lever outer end is below 10 lbf (44.5 N) Engine driven pump Examine Fuel system components Examine as far as possible with panels in Task 0600/218 opened/removed Fuel low level warning system Operational test MSN 101-105 AMM12-A-28-40-00-00A-903A-A MSN 106-999 AMM12-A-28-40-00-00A-903B-A Low pressure filter blockage indicator Make sure that it has not come out. If indicator found out, do the inspection/check procedure AMM12-A-2910-04-00A-313A-A Hydraulic system MSN 101-230 - check fluid sensor and level using maintenance switch box. Fill as necessary AMM 12-A29-00-00-00A-902A-A. MSN 231-999 - make sure fluid level indicator on the reservoir tank shows full. Fill as necessary AMM 12-A29-00-00-00A-902B-A Reservoir tank Make sure nitrogen pressure is correct. Pressurize as necessary MSN 101-230 AMM12-A-29-00-00-00A-902A-A MSN 231-999 AMM12-A-29-00-00-00A-902B-A Power pack Examine, specially for leaks and cracks on the end plates and where motor is attached Nitrogen accumulator Check nitrogen pressure and fill as necessary AMM 12-A-29-10-02-00A-901A-A Power pack electric motor shaft seal drain fluid collector bottle (Post SB 29-002 and MSN 181-999) Remove, clean and re-install
REVISIÓN: ORIGINAL
1000 flying hours
Y
3500 flying hours
Y
1000 flying hours or 4 years whichever comes first (installed)
FECHA: 16-JUNIO-2014
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
PAG: A2.25
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
30-10/79
Airfoil de-icers Apply a surface coating of Age Master No. 1 in accordance with the manufacturers instructions Wing and horizontal stabilizer airfoil de-ice boots Inspection/check AMM 12-A-30-10-00-00A-313A-A Inertial separation system Operational test. MSN 101-320 and 322-400 AMM 12-A-30-20-00-00A903A-A MSN 321 and 401-999 AMM 12-A-30-20-00-00A903B-A Airfoil de-ice system Functional test AMM 12-A-30-10-00-00A-903A-A Engine air intake de-ice lip Examine, look for signs of gas leaks - none are permitted Air by-pass door and operating mechanism Examine and lubricate with minimum quantity of P10001 Probes de-ice system Operational test. Single P-S system AMM 12-A-30-30-10-00A-903A-A Dual system and P-S indicator AMM 12-A-30-30-2000A-903A-A MSN 321 and 401-999 AMM 12-A-30-30-20-00A903B-A Windshield de-ice system Operational test AMM 12-A-30-40-00-00A-903A-A or 12-A-30-40-00-00A-903B-A Propeller de-ice system Inspection/check AMM 12-A-30-60-00-00A-313A-A Propeller de-ice system Operational test AMM 12-A-30-60-00-00A-903A-A CAWS CACU clock battery (MSN 321 and 401 - 999) Discard Main and nose wheel bearings Lubricate AMM 12-A-12-20-06-00A-902A-A
30-10/154 30-10/155
30-10/260 30-20/156
30-20/261
30-30/157
30-40/262
30-60/158 30-60/159 31-50/34 32-10/80
32-10/81
32-10/162 32-10/163 32-10/164 32-10/165
32-10/263 32-10/264
INTERVAL/ LIMITATIONS
Main landing gear axles and bushes (PC-12/45 and PC-12/47 aircraft) Inspection/Check AMM 12-A-32-10-00-00A-313A-A
6 month
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
2 years (installed) Tire change or 12 month whichever comes first (installed) 2000 flying hours or 12 months whichever comes first (installed)
Main landing gear Lubricate AMM 12-A-12-20-04-00A-902A-A Main landing gear legs Examine Main landing gear compartments Examine Main landing gear shock struts Check nitrogen pressure AMM 12-A-32-10-00-00A902A-A Main landing gear electrical bonding straps Examine Main landing gear left and right axle bolt (Pre SB 32006) Remove and examine. Replace if damaged. Install a serviceable bolt
REVISIÓN: ORIGINAL
AL
FECHA: 16-JUNIO-2014
Y
Y
Y
Y
PAG: A2.26
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
INTERVAL/ LIMITATIONS
32-10/345
Main landing gear Overhaul CMM 02099
Threshold 25,000 flying hours or 30,000 landings, whichever comes first. Repeat 8,300 flying hours or 10,000 landings or 6 years, whichever comes first Threshold 25,000 flying hours or 30,000 landings, whichever comes first. Repeat 8,300 flying hours or 10,000 landings, whichever comes first Threshold 25,000 flying hours or 30,000 landings, whichever comes first. Repeat 8,300 flying hours or 10,000 landings, whichever comes first
32-10/346
32-10/347
32-20/5
32-20/166
32-20/167 32-20/168
32-20/169 32-20/265 32-20/266
32-20/305
32-20/335
32-20/336
MLG Yoke fitting lugs Eddy Current Inspection CMM 02099
MLG Trailing Link Eddy Current Inspection CMM 02099
NLG drag link right part (Part No. 532.20.12.140) (Pre SB 32-014) Life limit Nose landing gear leg shock strut Check nitrogen pressure AMM 12-A-32-20-00-00A902A-A Nose landing gear Lubricate AMM 12-A-12-20-04-00A-902A-A Nose landing gear leg and steering mechanism Examine, in particular the steering rod end (Part No. 532.20.12.134) for the complete retention of bearing into the steering rod end housing. Nose landing gear compartment Examine Nose landing gear electrical bonding straps Examine Nose landing gear spring strut Part No. 532.20.12.250 Remove, clean and lubricate AMM12-A-32-20-03-00A920A-A and 12-A-32-20-03-00A-250A-A Nose landing gear actuator fuselage attachment fitting (Part No. 553.10.12.326) Examine, if cracks are found replace attachment fitting SRM 12-A-53-00-01-00A-663A-A Nose landing gear torque tube (Part No. 532.50.12.047) Life limit NLG drag link right part (P/N 532.20.12.289 or 532.20.12.140)
REVISIÓN: ORIGINAL
4000 landings
11000 flying hours or 15000 landings or 10 years, whichever comes first Initially 2000 flying hours or 2500
FECHA: 16-JUNIO-2014
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
PAG: A2.27
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
32-20/403
32-30/170
32-40/171
32-40/172
32-40/173
32-40/174
32-40/175
32-40/176
32-50/404
33-40/177
33-41/178
ITEMS / DESCRIPTION
INTERVAL/ LIMITATIONS
Inspection/check AMM 12-A-32-20-06-00A-313A-A
landings (installed) whichever comes first, then every 300 flying hours or 400 landings, whichever comes first. Threshold 25,000 flying hours or 30,000 landings, whichever comes first. Repeat 8,300 flying hours or 10,000 landings or 6 years, whichever comes first
NLG Overhaul CMM 02100
Extension and retraction system Functional test of extension and retraction system and emergency extension system AMM 12-A-32-30-0000A-903A-A Mainwheels Examine. Rotate wheels, make sure bearing movement is smooth and free and no excessive play exists Mainwheel tires Examine and check tire pressure AMM 12-A-12-1004-00A-902A-A Nosewheel Examine. Rotate wheel, make sure bearing movement is smooth and free and no excessive play exists Nosewheel tire Examine and check tire pressure AMM12-A-12-10-0400A-902A-A Brake system Apply the parking brake. Examine the brake units. Make sure that pad wear indicators protrude from housing. Fluid reservoir Check and replenish if necessary AMM 12-A-12-1002-00A-902A-A NLG Steering Mechanism Examine AMM 12-A-32-50-00-00A-310A-A
Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 8,300 flying hours or 10,000 landings or 6 years, whichever comes first
Exterior lighting Operational test. MSN 101-320 and 322-400 AMM12-A-33-40-00-00A903A-A MSN 321 and 401-999 AMM 12-A-33-40-00-00A903B-A Landing lights
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
PAG: A2.28
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
33-42/179 33-43/180 33-44/181 33-46/182 34-00/183 34-00/184 34-11/82
34-11/185 34-11/186 34-11/268
34-14/83
34-21/84 34-25/85 34-54/86
35-10/6 35-10/7
35-10/187 35-10/188 35-10/269 35-10/270 35-20/87 52-10/88
INTERVAL/ LIMITATIONS
Examine Taxi lights Examine Navigation and strobe lights Examine Recognition lights (if installed) Examine Beacon lights (if installed) Examine Communications and navigation antennas Examine Cockpit instruments and avionic equipment Examine Static system Leak check. Single system AMM 12-A-34-11-10-00A-903A-A Dual system AMM 12-A-34-11-20-00A-903A-A Pitot tube Examine Static ports Examine Pitot and static system Drain. Single system AMM 12-A-34-11-00-00A-040A-A Dual system AMM 12-A-34-11-20-00A-901A-A Altimeter Check calibration at an approved center in accordance with the regulation in force (Ref. FAR Part 91 411) Standby magnetic compass Check swing AMM 12-A-34-21-00-00A-903A-A Attitude Heading Reference System (AHRS) Check swing AMM 12-A-34-25-00-00A-903A-A Transponder system (single and dual systems) Functional test AMM 12-A-34-54-00-00A-903A-A or 12-A-34-54-00-00A-903B-A Oxygen bottle Life limit Oxygen bottle Hydrostatic test. Refer to AVOX Service Information Letter SIL-35-114 latest revision (www.avoxsys.com).
High pressure relief indicator (green disk) Make sure that it is not damaged Oxygen system Check contents Oxygen pipelines and equipment Examine Oxygen system Operational test AMM 12-A-35-00-00-00A-903A-A Passenger oxygen masks Inspection/check AMM 12-A-35-20-00-00A-313A-A Passenger/crew door Examine with trim removed AMM 12-A-25-21-03-00A920A-A or 12-A-25-22-03-00A-920A-A Examine the top step area around the insulation mat
REVISIÓN: ORIGINAL
AL
2 years
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
2 years (installed)
Y
2 years (installed)
Y
2 years (installed)
Y
2 years (installed)
Y
15 years (elapsed)
Y
Refer to AVOX Service Information Letter SIL-35-114 latest revision (www.avoxsys.com).
Y
Y Y
3 years (installed)
Y
2000, 4000, 6000 flying hours or 2, 4, 6 years whichever comes first
Y
FECHA: 16-JUNIO-2014
Y Y
Y
Y
Y
PAG: A2.29
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
52-10/189
52-10/190
52-10/191
52-10/192
52-10/271
52-10/348
52-10/405
52-10/406
52-20/272 52-20/349
INTERVAL/ LIMITATIONS
for corrosion. If corrosion is found, write to Pilatus for a specific repair Examine door hinge pin and hinges AMM 12-A-52-1000-00A-313A-A Passenger/crew door seal Clean with a dry cloth, examine and apply P09-002 french chalk Passenger/crew door shoot bolts and door frame fittings Examine Passenger/crew door handle lock pin Make sure movement is free Passenger/crew door hinges Examine and lubricate as necessary with minimum quantity of P10-001 Lubricant Passenger/crew door, counterbalance and cable support brackets Examine Passenger/crew door Examine all structural elements AMM 12-A-52-10-00-00A-310A-A
Passenger/Crew Door Piano Hinge Eddy Current Inspection AMM 12-A-52-00-01-00A-353A-A
Passenger/Crew Door Skin Eddy Current Inspection AMM 12-A-52-10-01-00A-353A-A
Emergency door Examine (door removed) Emergency door Examine all structural elements AMM 12-A-52-20-00-00A-310A-A
REVISIÓN: ORIGINAL
Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first. Threshold 25,000 flying hours or 30,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first.
Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500
FECHA: 16-JUNIO-2014
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
PAG: A2.30
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
52-30/8
INTERVAL/ LIMITATIONS flying hours or 15,000 landings or 6 years, whichever comes first 13000 flying hours or 17000 landings whichever comes first
Cargo door lower lug fittings (qty 3) Life limit
52-30/89
52-30/193
52-30/194
52-30/195
52-30/273
52-30/274 52-30/350
52-30/407
52-30/408
Cargo door Examine with trim removed AMM 12-A-25-21-03-00A920A-A or 12-A-25-22-03-00A-920A-A. Examine door hinge pin and hinges AMM 12-A-52-3000-00A-313A-A Cargo door seal Clean with a dry cloth, examine and apply P09-002 french chalk Cargo door shoot bolts, door frame fittings and hooks Examine. Make sure the hook roller bushes are free to rotate. For roller bush wear limits refer to AMM 12-A52-30-00-00A-313A-A Cargo door hinges Examine and lubricate as necessary with minimum quantity of P10-001 Lubricant Emergency door seal Clean with a wet cloth, dry and examine and apply P09-002 french chalk Cargo door Examine Cargo door Examine all structural elements AMM 12-A-52-30-00-00A-310A-A
Cargo Door Piano Hinge Eddy Current Inspection AMM 12-A-52-30-00-01A-353A-A
Cargo Door Skin Eddy Current Inspection AMM 12-A-52-30-01-00A-353A-A
REVISIÓN: ORIGINAL
AL
FECHA: 16-JUNIO-2014
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
2000, 4000, 6000 flying hours or 2, 4, 6 years whichever comes first
Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first. Threshold 25,000 flying hours or 30,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever
TIME LIMITS
Y
Y
Y
Y
PAG: A2.31
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
INTERVAL/ LIMITATIONS
52-70/275
Door warning system Operational test AMM 12-A-52-70-00-00A-903A-A Fuselage and associated structure (Pre SB 04-009) Life Limit
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
comes first.
53-00/9
53-00/90
53-00/91
53-00/92
53-00/93
53-00/94
53-00/196
53-00/276 53-00/277
53-00/278
53-00/279 53-00/280
53-00/324
53-00/337 53-00/351
Front pressure bulkhead Examine with insulation on engine and cockpit sides removed. If insulation on cockpit side is wet, remove, dry and reinstall insulation Fuselage internal bottom surface Examine frames 10, 21, 24, 36 and frames adjacent to doors and to emergency exit, with insulation removed. If corrosion is found, examine all fuselage bottom surface with insulation removed. If insulation is wet, remove, dry and reinstall insulation Rear pressure bulkhead Examine with trim removed
Structure around windows Examine
Door frames and emergency exit frame Examine. If insulation is installed in the door frames and is wet, remove and discard it (no longer installed on production) Fuselage external surface Examine. For aircraft that experience stone damage to the belly skin, visually examine affected areas for cracks. Rear pressure Bulkhead Examine Floor top and bottom surface and seat rails Examine as far as possible with carpet and floor panels in Task 06-00/8 removed Baggage/freight net mounting plates attachment bolts and surrounding structure Examine for corrosion Baggage compartment Examine Rear fuselage internal structure Examine as far as possible, in particular examine battery mounting tray for corrosión Fuselage and associated structure (Post SB 04-009) Life limit
Carry through frames 21 and 24 Inspection/Check AMM 12-A-53-20-02-00A-313A-A Upper Longerons Frame 10 Eddy Current Inspection AMM 12-A-53-10-06-01A-353A-A
REVISIÓN: ORIGINAL
20000 flying hours or 27000 landings whichever comes first 2000, 4000, 6000 flying hours or 2, 4, 6 years whichever comes first
Y
Y
2000, 4000, 6000 flying hours or 2, 4, 6 years whichever comes first
Y
2000, 4000, 6000 flying hours or 2, 4, 6 years whichever comes first 2000, 4000, 6000 flying hours or 2, 4, 6 years whichever comes first 2000, 4000, 6000 flying hours or 2, 4, 6 years whichever comes first
Y
Y
Y
Y
25000 flying hours or 30000 landings whichever comes first
Threshold 25,000 flying hours or 30,000 landings, whichever comes first.
FECHA: 16-JUNIO-2014
Y
Y
PAG: A2.32
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
53-00/352
53-00/353
53-00/354
53-00/355
53-00/356
53-00/357
Fuselage Frames 10 to 16 Examine all structural elements AMM 12-A-53-10-00-00A-310A-A
Fuselage Frames 16 to 36 Examine all structural elements AMM 12-A-53-20-00-00A-310A-A
Fuselage Frames 36 to 43 Examine all structural elements AMM 12-A-53-30-00-00A-310A-A
Antenna Structure Examine AMM 12-A-53-00-00-00A-310A-A
Antenna - Bottom fuselage skin Eddy Current Inspection AMM 12-A-53-00-00-00A-353A-A
Antenna - Upper fuselage skin Eddy Current Inspection AMM 12-A-53-00-00-00A-353A-A
REVISIÓN: ORIGINAL
INTERVAL/ LIMITATIONS Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first Threshold 28,300 flying hours or 37,000 landings, whichever comes first. Repeat 8,300 flying hours or 10,000 landings, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes
FECHA: 16-JUNIO-2014
AL
TIME LIMITS
100 HOUR
ANNUAL
Y
Y
Y
Y
Y
Y
PAG: A2.33
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PI
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
53-00/358
53-00/359
53-00/360
53-00/361
53-00/419
55-00/10
INTERVAL/ LIMITATIONS
Upper Flange Carry Through Frames 21 and 24 Examine AMM 12-A-53-20-02-00A-310A-A
Frames 21 and 24 Wing Attachments Eddy Current Inspection AMM 12-A-53-20-02-00A-353A-A
Frames 21 and 24 Side Frame Attachments Eddy Current Inspection AMM 12-A-53-20-02-00A-353A-A
Frames 41 and 43 Stabilizer Attachment Eddy Current Inspection AMM 12-A-53-30-02-00A-353A-A or AMM 12-A-55-30-03-00A-353A-A
Frame 40 Eddy Current Inspection AMM 12-A-53-30-02-00A-353A-A
Tail structure (Pre SB 04-009) Life limit
REVISIÓN: ORIGINAL
first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 30,000 flying hours or 39,000 landings, whichever comes first. Repeat 10,000 flying hours or 12,000 landings or 6 years, whichever comes first Threshold 30,000 flying hours or 39,000 landings, whichever comes first. Repeat 10,000 flying hours or 12,000 landings, whichever comes first Threshold 30,000 flying hours or 39,000 landings, whichever comes first. Repeat 10,000 flying hours or 12,000 landings, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first 20000 flying hours or 27000 landings
FECHA: 16-JUNIO-2014
AL
TIME LIMITS
100 HOUR
ANNUAL
Y
Y
Y
Y
Y
Y
PAG: A2.34
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PI
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
55-00/325
55-10/95
55-10/96
55-10/197 55-10/319 55-20/362
55-20/367
55-20/368
55-30/198
55-30/199
55-30/281
INTERVAL/ LIMITATIONS
Tail structure (Post SB 04-00-9) Life limit
Horizontal stabilizer internal surfaces and horizontal/vertical stabilizer interface Examine as far as possible with panels removed Vertical stabilizer internal surfaces Examine as far as posible with panels removed
Horizontal stabilizer external surface Examine Horizontal/vertical stabilizer attachment Inspection/Check AMM 12-A-55-00-00-00A-361A-A Elevator Examine AMM 12-A-55-20-00-00A-310A-A
Elevator Drive Lever Eddy Current Inspection AMM 12-A-55-20-01-00A-353A-A
Elevator Hinges Eddy Current Inspection AMM 12-A-55-20-01-00A-353A-A
whichever comes first 25000 flying hours or 30000 landings whichever comes first 2000, 4000, 6000 flying hours or 2, 4, 6 years whichever comes first 2000, 4000, 6000 flying hours or 2, 4, 6 years whichever comes first
Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first
Vertical stabilizer external surface Examine, specially around rear spar top rivets. If cracks are found refer to SRM 12-A-55-00-01-00A664A-A for repair procedure Vertical stabilizer rear spar strap and lower aft fairing shear plate (Pre SB 55-002) Examine, if wear is found refer to SB 55-002 Vertical stabilizer electrical bonding straps Examine
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
PAG: A2.35
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
INTERVAL/ LIMITATIONS
55-30/369
Vertical Stabilizer Examine AMM 12-A-55-30-00-00A-310A-A
Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings,
55-30/370
55-30/371
55-30/372
55-30/420
55-40/373
Vertical Stabilizer Main and Rear Spar Attachment to Fuselage Eddy Current Inspection AMM 12-A-53-30-02-00A-353A-A or AMM 12-A-55-30-03-00A-353A-A
Vertical Stabilizer Main Attachment to Horizontal Stabilizer Eddy Current Inspection AMM 12-A-55-00-00-00A-353A-A
Vertical Stabilizer Pitch Trim Actuator Fitting and Attachment Eddy Current Inspection AMM 12-A-55-30-02-00A-353A-A
Vertical Stabilizer Forward Attachment to Frame 40 Eddy Current Inspection AMM 12-A-55-30-03-00A-353A-A
Rudder Examine AMM 12-A-55-40-00-00A-310A-A
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
AL
TIME LIMITS
100 HOUR
ANNUAL
Y
Y
Y
Y
y
Y
PAG: A2.36
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PI
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
55-40/377
55-40/410
56-10/200 56-11/12 56-11/13
56-11/14 56-11/15
56-11/332
56-11/378
56-20/201 57-00/11
INTERVAL/ LIMITATIONS whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first
Rudder Hinges Eddy Current Inspection AMM 12-A-55-40-05-00A-353A-A
Rudder Trim Tab Examine AMM 12-A-55-40-04-00A-310A-A
Windshield LH and RH Examine AMM 12-A-56-00-00-00A-313A-A Cockpit outer side, DV windows and cabin windows Replace Cockpit inner and outer side, DV windows and cabin windows Refer to AMM 12-A-56-00-00-00A-313A-A for limits
Windshield LH and RH Replace Windshield LH and RH Only unpressurized flight is permitted up to the next scheduled inspection providing it does not cause visual problems Cockpit side windows Inspection/check AMM 12-A-56-11-02-00A-313A-A
Windshield LH and RH and Cockpit Side Windows Examine with windshield and side windows removed AMM 12-A-56-11-01-00A-310A-A and AMM 12-A-56-11-02-00A-310A-A and AMM 12-A-53-10-16-00A-310A-A
Cockpit and cabin windows Examine AMM 12-A-56-00-00-00A-313A-A Wing structure (Pre SB 04-009) Life limit
REVISIÓN: ORIGINAL
If cracked or stress crazing Can be felt If chipped, cracked (only for inner side windows), scratched, bubbles or delaminated If cracked in inner lamination If cracked in outer lamination 11000 flying hours or 10 years whichever comes first (installed) Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first
20000 flying hours or 27000 landings whichever comes first
FECHA: 16-JUNIO-2014
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
PAG: A2.37
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
INTERVAL/ LIMITATIONS
57-00/97
Wing internal surfaces and flap compartment Examine as far as possible with all wing panels removed
2000, 4000, 6000 flying hours or 2, 4, 6 years whichever comes first 2000, 4000, 6000 flying hours or 2, 4, 6 years whichever comes first 11000 flying hours or 10 years whichever comes first
57-00/98
57-00/99
57-00/202 57-00/282 57-00/283
57-00/284 57-00/326
57-00/379
57-00/380
57-00/382
57-00/383
Landing gear compartments Examine, especially main and rear spar parts
Wing to fuselage attachments Examine attachment fittings with wings removed AMM 12-A-57-00-00-00A-313A-A Wing external surfaces Examine Wing tip static dischargers Examine Wing internal surfaces and flap compartment Examine as far as possible with panels in Task 0600/218 opened/removed Wing to fuselage Attachments Examine as far as posible Wing structure (Post SB 04-00-9) Life limit
Wing Examine all structural elements Rib 1 to Rib 20 AMM 12-A-57-00-00-00A-310A-A
Wing Main and Rear Spar to Fuselage Attachment Eddy Current Inspection AMM 12-A-57-00-03-00A-353A-A and AMM 12-A-57-00-03-01A-353A-A
Wing Rear Spar at Rib 8 Flap Arm Attachment Eddy Current Inspection AMM 12-A-57-20-10-00A-353C-A
Wing Main Spar Fastener Holes Rib 1 thru Rib 6 Eddy Current Inspection
REVISIÓN: ORIGINAL
25000 flying hours or 30000 landings whichever comes first Threshold 30,000 flying hours or 39,000 landings, whichever comes first. Repeat 10,000 flying hours or 12,000 landings or 6 years, whichever comes first Threshold 30,000 flying hours or 39,000 landings, whichever comes first. Repeat 10,000 flying hours or 12,000 landings or 6 years, whichever comes first Threshold 25,000 flying hours or 30,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 25,000 flying hours or
FECHA: 16-JUNIO-2014
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
PAG: A2.38
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
57-00/384
57-00/385
57-00/412
57-00/413
57-00/427
57-60/393
ITEMS / DESCRIPTION
INTERVAL/ LIMITATIONS
AMM 12-A-57-20-10-00A-353A-A
30,000 landings, whichever comes first. Repeat 3,300 flying hours or 4,000 landings, whichever comes first Threshold 25,000 flying hours or 30,000 landings, whichever comes first. Repeat 3,300 flying hours or 4,000 landings, whichever comes first Threshold 25,000 flying hours or 30,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 25,000 flying hours or 30,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first Threshold 25,000 flying hours or 30,000 landings, whichever comes first. Repeat 2,500 flying hours or 3,000 landings, whichever comes first. Threshold 16,000 wing flying hours or 22,500 wing landings, whichever comes first. Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6
Wing Main Spar Fastener Holes Strap Rib 6 Eddy Current Inspection AMM 12-A-57-20-05-00A-353A-A
Wing Rear Spar Fastener Holes Rib 2 thru Rib 3 Eddy Current Inspection AMM 12-A-57-20-10-00A-353B-A
Wing Tips Examine AMM 12-A-57-33-00-00A-310A-A
Wing Skin around drain holes Eddy Current Inspection AMM 12-A-57-20-01-00A-353A-A
Wing Main Spar Fastener Holes Strap Rib 6 Eddy Current Inspection AMM 12-A-57-20-10-00A-353D-A
Aileron Examine AMM 12-A-57-60-00-00A-310A-A
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
AL
TIME LIMITS
100 HOUR
ANNUAL
Y
Y
Y
Y
Y
Y
PAG: A2.39
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PI
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
57-60/411
61-00/100
61-10/37
61-10/203
61-10/285
61-20/286
71-00/16
71-00/17
71-00/38
71-00/101
71-00/102
71-00/106
71-00/107
INTERVAL/ LIMITATIONS years, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first 400 flying hours or 12 month whichever comes first (Ref Hartzell SL 61) (installed) 4000 flying hours or 6 years whichever comes first (Ref Hartzell SL 61) (installed)
Aileron Trim Tab Examine AMM 12-A-57-60-04-00A-310A-A
Propeller Lubricate AMM 12-A-12-20-05-00A-902A-A
Propeller Overhaul
Propeller blades Examine. Repair blades as necessary Ref. Hartzell MM Propeller hub Remove spinner dome and examine propeller hub. Install spinner dome AMM 12-A-61-10-01-00A-920A-A Propeller governor, Overspeed governor and beta controls Examine Engine mounting frame (Pre SB 04-009) Life limit
Engine mounting frame, replace all bolts, washers and nuts Life limit Engine shock mount assemblies Overhaul Power plant torque limiter Operational test AMM 12-A-71-00-00-00A-903H-A
Power plant performance Operational test AMM 12-A-71-00-00-00A-903I-A
Oil pressure transducer electrical connector (Pre SB 79-004) Clean AMM 12-A-71-00-03-00A-250A-A Engine torque and stick pusher torque transducer electrical connectors Clean AMM 12-A-71-00-03-00A-250A-A
REVISIÓN: ORIGINAL
AL
TIME LIMITS
100 HOUR
Y
Y
Y
20000 flying hours or 27000 landings whichever comes first
Y
11000 flying Hours
Y
FECHA: 16-JUNIO-2014
PI
Y
Y
At engine overhaul, but not later than 5000 flying hours 500 flying hours or 12 months whichever comes first (installed) 500 flying hours or 12 months whichever comes first (installed) 500 flying hours or 12 months whichever comes first (installed) 500 flying hours or 12 months whichever comes first (installed)
ANNUAL
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
PAG: A2.40
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
71-00/204
Power plant Post inspection ground run tests AMM 12-A-71-00-0000A-903A-A Engine tubular mounting frame and shockmounts Examine. Replace shockmount if cracks in elastomer are more than 1 in (25,4 mm) long and/or 0.06 in (1,5 mm) deep Power plant and accessories Examine. Refer to P&WC EMM 72-00-00 Periodic inspection and do the 100 hour and minor inspection ítems Engine drain mast and tank Examine for fuel leaks (no leaks permitted) and drain (no excessive leaks) Power plant Inspection ground run - note defects. NOTE: A pre inspection ground run is not a pre-requisite but may be useful to determine any repair work needed to maintain the airworthiness of the aircraft AMM 12-A71-00-00-00A-903A-A Engine tubular mounting frame firewall attachment fittings Examine with firewall insulation blanket removed as necessary. If cracked, blistered or flaking paint is found on the mounting frame refer to SRM 12-A-5420-02-00A-664A-A Engine mounting frame (Post SB 04-009) Life limit
71-00/205
71-00/206
71-00/209
71-00/287
71-00/301
71-00/327
71-00/401
71-00/432
71-10/207
71-10/208 72-00/18 72-00/39
72-00/308 74-00/288
INTERVAL/ LIMITATIONS
Engine Mount Magnetic Particle Inspection AMM 12-A-71-00-05-00A-352A-A
Powerplant and accessories Refer to P&WC EMM 72-00-00 Periodic Inspection and do the time limited inspection items Engine cowlings ENG 43AL and ENG 43AR Open and examine, particularly for condition of rubbing strips and fasteners. Lubricate the hinges with a minimum of material P10-001C Engine cowlings ENG 43AL and ENG 43AR Close Engine rotor components Life limit Engine Overhaul Engine accessories Overhaul Ignition system Operational test AMM 12-A-74-00-00-00A-903A-A
REVISIÓN: ORIGINAL
25000 flying hours or 30000 landings whichever comes first Threshold 26,600 flying hours or 35,000 landings, whichever comes first. Repeat 6,600 flying hours or 8,000 landings, whichever comes first
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
P&WC SB 14002 3500 flying hours P&-WC SB 14-603 latestrevision P&WC SB 14603 latest revision
FECHA: 16-JUNIO-2014
Y Y Y
PAG: A2.41
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 TASK NO.
ITEMS / DESCRIPTION
76-00/210
Engine controls in engine compartment Examine Beta slip ring carbon block Make sure gap is not more than 0.01in (0.2- 5mm) Cockpit control quadrant Caution Do not move PCL into the reverse range PCL - move between idle and max and make sure movement is full and free. Condition lever - Do the operational test AMM 12-A-76-10-00-00A-903A-A. Manual override lever - move between off and max and make sure movement is full and free. Cockpit control quadrant Power control - operational test AMM 12-A-76-10-0000A-903A-A Manual override - operational test AMM 12-A-76-2000-00A-903A-A Cockpit control quadrant Examine Propeller feathering microswitches Functional test AMM 12-A-76-10-02-00A-903A-A
76-00/211 76-00/212
76-00/303
76-00/304 76-10/117
77-00/213
78-00/214 79-00/215
79-20/43 79-20/289
79-20/290
INTERVAL/ LIMITATIONS
Engine instrument system Operational test. MSN 101-111 (AMM 12-A-77-40-00-00A-903A-A MSN 112-320 and 322-400 AMM 12-A-77-40-00-00A903B-A MSN 321 and 401-999 AMM 12-A-77-40-00-00A903C-A Exhaust stubs Examine Oil filler cap/dipstick Energize aircraft electrical system AMM 12-A-24-0000-00A-901A-A. Remove filler cap, examine and make sure the seal is in good condition. Set and hold AIR/GROUND switch to GROUND and make sure after 60 seconds the CAWS OIL QTY caption comes on. Install filler cap and make sure the locking mechanism operates correctly. Oil cooler Overhaul Engine oil cooler Examine. Make sure outlet door has full and free movement Oil system chip detector indication system Operational test AMM 12-A-79-30-01-00A-903A-A
AL
TIME LIMITS
100 HOUR
ANNUAL
PI
Y
Y
Y
Y
Y
Y
Y
Y 3000 flying hours or 12 months whichever comes first
At engine overhaul
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
Y
100 HOUR INSPECTION - SCHEDULED INSPECTIONS General 1. The terms used for the item inspection requirements are defined in 12-A-05-20-00-00A-018A-A
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.42
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Certain inspection items in the 100 hour inspection sheets are marked with an asterisk *. These items are applicable when the aircraft is inspected in conformity with the requirements of FAA Parts 43 and 91 only. 2. 100 Hour Inspection
Ac No. Chapt/Task 2.2 Job Set Up 27-50/143 12-20/124 12-20/125 12-20/126 06-00/123 71-10/207
AF Hrs. Item
Flaps - lower to 40° Aircraft - Wash the aircraft exterior, including the landing gear and flap compartments (12-A-12-20-01-00A-902A-A) Windshields and windows - clean (12-A-12-20-02-00A902A-A) Cockpit and cabin - clean (12-A-12-20-03-00A-902A-A) Access panels 42AB, 42AT and 32CT – remove (12-A-06-2000-00A-040A-A) Engine cowlings ENG 43AL and ENG 43AR - open and examine, particularly for condition of rubbing strips and fasteners. Lubricate the hinges with a minimum of P10001CWD40
INTERVAL
100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection
100 Hour Inspection
2.3 Procedure 10-10/428
22-20/129 22-20/130 24-30/131
*24-30/132 *24-60/133 *25-10/134 *25-10/135 *25-20/136 25-20/302
REVISIÓN: ORIGINAL
Parking, Mooring & Storing External protective covers - Examine. Replace if any part of the cover is missing, damaged, torn or does not install properly. Auto Flight Angle of Attack (AOA) transmitters – examine Stick pusher system - check (12-A-22-20-00-00A-903A-A) Electrical Power Generator 2 drive belt - examine and adjustment/test, AMM 12-A-24-30-03-00A-903A-A or 12-A-24-30-03-00A903B-A Battery (Batteries - if 2nd battery installed) - examine and operational test, AMM 12-A-24-30-00-00A-903A-A Cockpit circuit breaker panels and switch panels – Examine Equipment and Furnishings Crew seat belts – examine Crew seats - examine as far as possible with seats Installed Passenger seat belts and extensions - examine Passenger seats - examine as far as possible with seats installed. Move the recline mechanism and swivel function (executive seat only) through its full motion and check for correct operation. If necessary, refer to the applicable supplier CMM (CMM 25-20-07 for executive seats and CMM 25-20-99 for standard seats). FECHA: 16-JUNIO-2014
100 Hour Inspection
100 Hour Inspection 100 Hour Inspection
100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection
100 Hour Inspection
PAG: A2.43
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Ac No. Chapt/Task
*27-00/138 27-10/139 27-20/140
27-30/141 27-40/142 27-40/291 27-50/144
28-10/145 28-10/146 28-20/148 28-20/149
28-20/150 28-20/147
29-10/151
29-10/152
29-10/153
REVISIÓN: ORIGINAL
AF Hrs. Item Flight Controls Aileron, elevator and rudder controls - operate, make sure full and free travel Aileron LH and RH – examine Rudder - Examine, in particular the cover plate (Part No. 555.40.12.215) on the bottom of the rudder to make sure it is not bent and there are no signs of interference with the rudder stop. Elevators – examine Horizontal stabilizer trim - operational test of trim interrupt and alternate trim switches (12-A-27-40-00-00A-903A-A) Horizontal stabilizer trim - operational test of trim system (12-A-27-40-00-00A-903A-A) Flaps and flap support mechanism - examine. For Flap drive arms, refer to AMM 12-A-27-51-00-00A-313A-A. Fuel Fuel tank filler caps – examine Fuel - remove a sample from each drain valve and examine for wáter Fuel filter element - remove and clean, AMM 12-A-28-2001-00A-920A-A and 12-A-28-20-01-00A-250A-A Firewall shut-off valve - operate FUEL EMERG SHUTOFF lever and make sure firewall shutoff valve opens and closes fully to dead stop. Make sure movement is free and check if initial pull out force at lever outer end is below 10 lbf (44.5 N) Engine Driven fuel Pump (EDP) – examine Fuel tank vent valve and flame arrestor - operational test, AMM 12-A-28-20-07-00A-903A-A Hydraulic Power Low pressure filter blockage indicator - make sure that it has not come out. If indicator found out, do the inspection/check procedure, AMM 12-A-29-10-04-00A313A-A Hydraulic system, MSN 101-230 - check fluid sensor and level using maintenance switch box. Fill as necessary, AMM 12-A-29-00-00-00A-902A-A MSN 231-999 - make sure fluid level indicator on the reservoir tank shows full. Fill as necessary, AMM 12-A-29-00-00-00A-902B-A Reservoir tank - make sure nitrogen pressure is correct. Pressurize as necessary, MSN 101-230 AMM 12-A-29-0000-00A-902A-A, MSN 231-999 AMM 12-A-29-00-00-00AFECHA: 16-JUNIO-2014
INTERVAL
100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection
100 Hour Inspection
100 Hour Inspection 100 Hour Inspection
100 Hour Inspection
100 Hour Inspection
100 Hour Inspection
PAG: A2.44
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Ac No. Chapt/Task
30-10/154 30-20/155
30-20/156 30-30/157
30-60/158 30-60/159
*07-10/161 32-10/162 32-10/163 32-10/164 *32-10/165 32-10/264
32-20/167 32-20/168
32-20/169 *32-20/166 *32-30/170
*32-40/171 REVISIÓN: ORIGINAL
AF Hrs. Item 902B-A Ice and Rain Protection Wing and horizontal stabilizer airfoil de-ice boots inspection/check, AMM 12-A-30-10-00-00A-313A-A Inertial separation system - operational test. MSN 101-320 and 322-400, AMM 12-A-30-20-00-00A-903A-A. MSN 321 and 401-999, AMM 12-A-30-20-00-00A-903B-A Engine air intake de-ice lip - look for signs of gas leaks none are permitted Probes de-ice system - operational test. Single P-S system, AMM 12-A-30-30-10-00A-903A-A. Dual system and P-S indicator, AMM 12-A-30-30-20-00A-903A-A. MSN 321 and 401-999, AMM12-A-30-30-20-00A-903B-A Propeller de-ice system - inspection/check, AMM 12-A-3060-00-00A-313A-A Propeller de-ice system - operational test, AMM 12-A-3060-00-00A-903A-A Landing Gear Aircraft lift on jacks, AMM 12-A-07-10-00-00A-901A-A Main landing gear - for lubrication, AMM 12-A-12-20-0400A-902A-A
INTERVAL
100 Hour Inspection 100 Hour Inspection 100 Hour Inspection
100 Hour Inspection
100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection
Main landing gear legs – examine
100 Hour Inspection
Main landing gear compartments – examine Main landing gear shock struts - check nitrogen pressure (12-A-32-10-00-00A-902A-A) Main landing gear left and right axle bolt (Pre SB 32-006) remove and examine. Replace if damaged. Install a serviceable bolt. Nose landing gear - for lubrication, AMM 12-A-12-20-0400A-902A-A Nose landing gear leg and steering mechanism - examine, in particular the steering rod end (Part No. 532.20.12.134) for the complete retention of bearing into the steering rod end housing. Nose landing gear compartment – examine Nose landing gear shock strut - check nitrogen pressure, AMM 12-A-32-20-00-00A-902A-A Extension and retraction system - functional test of extension and retraction system and emergency extension system (12-A-32-30-00-00A-903A-A) Mainwheels - examine. Rotate wheels, make sure bearing
100 Hour Inspection
FECHA: 16-JUNIO-2014
100 Hour Inspection 100 Hour Inspection 100 Hour Inspection
100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection PAG: A2.45
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Ac No. Chapt/Task
32-40/172 *32-40/173 32-40/174 32-40/175
32-40/176 *07-10/160
33-40/177
33-41/178 33-42/179 33-43/180 33-44/181 33-46/182 34-00/183 *34-00/184 34-11/185 34-11/186 35-10/187 35-10/188 52-10/189 52-10/190 52-10/191 52-10/192
REVISIÓN: ORIGINAL
AF Hrs. Item movement is smooth and free and no excessive play exists Mainwheel tires - examine and check tire pressure (12-A12-10-04-00A-902A-A) Nosewheel - examine. Rotate wheel, make sure bearing movement is smooth and free and no excessive play exists Nosewheel tire - examine and check tire pressure (12-A-1210-04-00A-902A-A) Brake system - apply the parking brake. Examine the brake units. Make sure that pad wear indicators protrude from housing. Fluid reservoir - replenish if necessary (12-A-12-10-02-00A902A-A) Aircraft - lower to the ground, remove jacks and disconnect from ground (12-A-07-10-00-00A-901AA) Lighting Exterior lighting - operational test. MSN 101-320 and 322400 (AMM 12-A-33-40-00-00A-903A-A). MSN 321 and 401999 (AMM 12-A-33-40-00-00A-903B-A) Landing lights – examine Taxi lights – examine Navigation and strobe lights - examine Recognition lights (if installed) – examine Beacon lights (if installed) – examine Navigation Communications and navigation antennas – examine Cockpit instruments and avionic equipment – examine Pitot-tube – examine Static ports – examine Oxygen High pressure relief indicator (green disk) – make sure that it is not damaged Oxygen system - check contents Doors Passenger/crew door seal - clean with a dry cloth, examine and apply P09-002 french chalk Passenger/crew door shoot bolts and door frame fittings – examine Passenger/crew door handle lock pin - make sure movement is free Passenger/crew door hinges - examine and lubricate as necessary with minimum quantity of CPCtemporary (Pt. No. P10-001) FECHA: 16-JUNIO-2014
INTERVAL
100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection
100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection
PAG: A2.46
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Ac No. Chapt/Task 52-30/193 52-30/194
52-30/195
53-00/196
55-10/197 55-30/198
55-30/199
56-10/200 56-20/201
57-00/202 61-10/203
*71-00/205
71-00/206
71-00/209
74-00/288 REVISIÓN: ORIGINAL
AF Hrs. Item Cargo door seal - clean with a dry cloth, examine and apply French chalk (Pt. No. P09-002) Cargo door shoot bolts, door frame fittings and hooks examine. Make sure the hook roller bushes are free to rotate. For roller bush wear limits refer to AMM 12-A-5230-00-00A-313A-A Cargo door hinges - examine and lubricate as necessary with minimum quantity of P10-001 Lubricant Fuselage Fuselage external surface - examine. For aircraft that experience stone damage to the belly skin, visually examine affected areas for cracks. Stabilizers Horizontal stabilizer external surface – examine Vertical stabilizer external surface - examine, specially around rear spar top rivets. If cracks are found refer to SRM 12-A-55-00-01-00A-664A-A for repair procedure Vertical stabilizer rear spar strap and lower aft fairing shear plate (Pre SB 55-002) - examine, if wear is found refer to SB 55-002. Windows Windshield LH and RH - examine, AMM 12-A-56-00-00-00A313A-A Cockpit and cabin windows - examine, AMM 12-A-56-0000-00A-313A-A Wing Wing external surfaces – examine Propeller Propeller blades - examine. Repair blades as necessary Ref. Hartzell MM Power Plant Engine tubular mounting frame and shockmounts examine. Replace shockmount if cracks in elastomer are more than 1 in (25,4 mm) long and/or 0.06 in (1,5 mm) deep Power plant and accessories - examine. Refer to P&WC EMM 72-00-00 Periodic inspection and do the 100 hour and minor inspection ítems Engine drain mast and tank - for fuel leaks (no leaks permitted) and drain (no excessive leaks) Ignition Ignition system - operational test (12-A-74-00-00-00AFECHA: 16-JUNIO-2014
INTERVAL
100 Hour Inspection
100 Hour Inspection
100 Hour Inspection
100 Hour Inspection
100 Hour Inspection 100 Hour Inspection
100 Hour Inspection
100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection
100 Hour Inspection
100 Hour Inspection 100 Hour Inspection 100 Hour Inspection PAG: A2.47
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Ac No.
AF Hrs. Item
Chapt/Task
INTERVAL
903A-A) Engine Controls 76-00/2107600/210 76-00/211 76-00/304 76-00/212
77-00/213
78-00/214 79-00/215
79-30/290 2.3 Job Close Up 06-00/119 71-10/208 71-00/204 00-00/121 00-00/122
REVISIÓN: ORIGINAL
Engine controls in engine compartment – examine Beta slip ring carbon block - make sure gap is not more than 0.01in (0.25mm) Cockpit control quadrant – examine
100 Hour Inspection 100 Hour Inspection 100 Hour Inspection
CAUTION Do not move PCL into the reverse range PCL - move between idle and max and make sure movement is full and free. Condition lever - Do the operational test (12-A-76-10-00-00A-903A-A). Manual override lever - move between off and max and make sure movement is full and free. Engine Indication Engine instrument system - operational test MSN 101-111 (AMM 12-A-77-40-00-00A-903A-A) MSN 112-320 and 322400 (AMM 12-A-77-40-00-00A-903B-A) MSN 321 and 401999 (AMM 12-A-77-40-00-00A-903C-A) Exhaust Exhaust stubs – examine Oil Oil filler cap/dipstick - energize aircraft electrical system, AMM 12-A-24-00-00-00A-901A-A. Remove filler cap, examine and make sure the seal is in good condition. Set and hold AIR/GROUND switch to GROUND and make sure after 60 seconds the CAWS OIL QTY caption comes on. Install filler cap and make sure the locking mechanism operates correctly. Oil system chip detector indication system - operational test, AMM 12-A-79-30-01-00A-903A-A Access panels 42AB, 42AT and 32CT – Install Engine cowlings ENG43AL and ENG 43AR – close Power plant - post inspection ground run (12-A-71-00-0000A-903A-A) Airworthiness Directives and Service Bulletins reviewed and complied with as required Chapter 4 and Chapter 5 - Overhaul and Replacement Schedule, and Time Limited Inspection Requirements sections reviewed and any additional requirements are complied with FECHA: 16-JUNIO-2014
100 Hour Inspection
100 Hour Inspection
100 Hour Inspection
100 Hour Inspection
100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection 100 Hour Inspection
100 Hour Inspection
PAG: A2.48
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Ac No. Chapt/Task
INTERVAL
AF Hrs. Item
ANNUAL INSPECTION - SCHEDULED INSPECTIONS 1. General The terms used for the item inspection requirements are defined in DM 12-B-05-20-00-00A-018A-A.
Note
2.
The scope of the 100 flying hour inspection is included in the Annual Inspection. Note that some 100 flying hour inspection items are not called for in the Annual Inspection, but similar more detailed tasks replace them. Preparation
Ac No. Chapt/Task 71-00/287
27-50/143 12-20/124 12-20/125 12-20/126 25-10/296
25-20/298 07-10/161 06-00/218
REVISIÓN: ORIGINAL
AF Hrs. Item Power plant inspection ground run - note defects. A preinspection ground run is not a prerequisite but may be useful to determine any repair work necessary to maintain airworthiness of the aircraft. Flaps - lower to 40° Aircraft - Wash the aircraft exterior, including the landing gear and flap compartments (12-A-12-20-01-00A-902A-A) Windshields and windows - clean (12-A-12-20-02-00A902A-A) Cockpit and cabin - clean (12-A-12-20-03-00A-902-A-A) Crew seats - remove MSN 101-660, AMM 12-A-25-10-01-00A-920A-A, MSN 661-999, AMM 12-A-25-10-05-00A-920A-A Passenger seats - remove, AMM 12-A-25-20-01-00A-920AA, 12-A-25-21-01-00A-920A-A, 12-A-25-22-01-00A-920A-A Aircraft - Lift on jacks (12-A-07-10-00-00A-901A-A) Connect the aircraft to ground. Open/remove and examine the following panels:11AL, 11AR, 11BL, 11BR, 12AL, 12AR, 12AZ, 12AB, 12BB, 12BL, 12BR, 12BZ, 12CL, 12CR, 12CZ, 12DZ, 12EL, 12ER, 12EZ, 12FL, 12FR, 12FZ, 12HZ, 21GZ, 21JZ, 21PZ, 21QZ,31AB, 31AL, 31BL, 32AB, 32AL, 32BL, 32BT, 32CL, 32CT, 32DL, 33ET, 41AT, 42AT, 42AB, 51KB, 51MB, 51NB, 52KB, 52MB, 52NB, 52OB, 52PB, 52RB, 52TB, 52SB, 61KB, 61MB, 61NB, 62KB, 62MB, 62NB, 62OB, 62PB, 62RB, 62SB, 62TB. Make sure the drain holes are clear, AMM 12-A-06-20-00-00AFECHA: 16-JUNIO-2014
INTERVAL
Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection
Annual Inspection
PAG: A2.49
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Ac No. Chapt/Task
71-10/207
10-10/428
11-00/220
21-20/221 21-20/127
21-40/53
21-40/54
21-40/128
21-50/223
22-10/233 22-20/129 22-20/226
24-20/227 24-30/331 REVISIÓN: ORIGINAL
AF Hrs. Item 040A-A Engine cowlings ENG 43AL and ENG 43AR - open and examine, particularly for condition of rubbing strips and fasteners. Lubricate the hinges with a minimum of material P10-001CWD40. 3 Annual Inspection Parking, Mooring & Storing External protective covers - Examine. Replace if any part of the cover is missing, damaged, torn or does not install properly. Placards and Markings Placards and markings - examine. Attach new placards if necessary (12-A-11-20-00-00A-040A-A) and (1-2-A-11-3000-00A-040A-A) Air Conditioning ECS and bleed air ducts, pipelines, equipment and associated clamps in the engine compartment – examine ECS EMER shut-off valve - operational test; max pull force 22.5 lbf (100N) and make sure ram air scoop is completely open Secondary heaters thermal protection switches (MSN 101320 without a modified auxiliary heating system) operational test, AMM 12-A-21-40-09-00A-903A-A Secondary heaters thermal protection switches (MSN 321999 and aircraft with a modified auxiliary heating system) operational test, AMM 12-A-21-40-00-00A-903A-A Flight compartment foot heater (if installed) thermal protection switch - operational test, AMM 12-A-21-40-1100A-903A-A Vapor cycle cooling system (if installed) - examine the cooling unit Auto Flight Pitch, roll, and yaw actuators and capstan control cables – examine Angle of Attack (AOA) transmitters – examine Stick pusher system - functional test (12-A-22-20-00-00A903A-A) Electrical Power AC electrical system - operational test, AMM 12-A-24-2000-00A-903A-A Generator 2 drive belt - examine and adjustment/test, FECHA: 16-JUNIO-2014
INTERVAL
Annual Inspection
Annual Inspection
Annual Inspection
Annual Inspection Annual Inspection
Annual Inspection
Annual Inspection
Annual Inspection Annual Inspection
Annual Inspection Annual Inspection Annual Inspection
Annual Inspection Annual Inspection PAG: A2.50
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Ac No. Chapt/Task
24-30/132
24-40/229 24-60/133 25-10/134 25-10/230 25-10/300
25-20/136 25-20/137 25-60/232 27-10/139 27-10/234
27-10/235 27-10/236
27-10/237
27-10/238
27-15/239
27-20/140
REVISIÓN: ORIGINAL
AF Hrs. Item AMM 12-A-24-30-03-00A-903A-A or 12-A-24-30-03-00A903B-A Battery (Batteries - if 2nd battery installed) - examine and operational test, AMM 12-A-24-30-00-00A-903A-A or 12-A24-30-00-00A-903B-A External Power Unit (EPU) receptacle – examine Cockpit circuit breaker panels and switch panels – examine Equipment and Furnishings Crew seat belts – examine Pilots relief tube system (if installed) - clean and leak check, AMM 12-A-25-10-05-00A-920A-A Crew seats - remove cushions, covers and shells (Ref. CMM) and examine seat. Install cushions, covers and shells. Note 2 The CMM Document No’s. are given in Chap 25-10-01 and 25-10-05. Passenger seat belts and extensions – examine Passenger seats – examine ELT installation – examine Flight Controls Aileron LH and RH – examine Aileron LH and RH rods and levers - examine Spray PTFE Teflon Spray OKS 571 (or equivalent) around the aileron pushrod guide roller sleeves at all three locations in each wing Aileron electrical bonding straps – examine Aileron controls - examine the control cables and pulleys as far as possible. Move the mechanism so that you can see all parts of the cables and make sure the safety clips are fully engaged in the turnbuckles Aileron cable tension - check MSN 101-683, AMM 12-A-27-10-00-00A-903A-A MSN 684-999, AMM 12-A-27-10-00-00A-903B-A Ailerons - functional test MSN 101-683, AMM 12-A-27-10-00-00A-903A-A MSN 684-999, AMM 12-A-27-10-00-00A-903B-A Aileron trim - functional test MSN 101-683, AMM 12-A-27-15-00-00A-903A-A MSN 684-999, AMM 12-A-27-15-00-00A-903B-A Rudder - Examine, in particular the cover plate (Part No. 555.40.12.215) on the bottom of the rudder to make sure it is not bent and there are no signs of interference with the FECHA: 16-JUNIO-2014
INTERVAL
Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection
Annual Inspection
Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection
Annual Inspection
Annual Inspection
Annual Inspection
Annual Inspection
PAG: A2.51
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Ac No. Chapt/Task
27-20/246 27-20/240 27-20/241
27-20/242
27-20/243 27-20/244 27-20/245 27-30/141 27-30/247 27-30/248 27-30/249
27-30/250 27-30/251 27-40/142
27-40/292 27-40/252 27-50/144 27-50/253 27-50/254 27-50/255
REVISIÓN: ORIGINAL
AF Hrs. Item rudder stop. Rudder electrical bonding straps – examine Rudder static dischargers – examine Rudder controls - examine the control cables and pulleys as far as possible. Move the mechanism so that you can see all parts of the cables and make sure the safety clips are fully engaged in the turnbuckles Aileron/rudder interconnect system, MSN 101-683 - make sure the locking mechanism is fully engaged with the flaps at 40° and the moving parts (piston and housing) are lubricated. If necessary apply grease P04-002 with a brush. Retract the flaps to 0° and make sure the locking mechanism is fully disengaged Rudder cable tension - check, AMM 12-A-27-20-00-00A903A-A or 12-A-27-20-00-00A-903B-A Rudder - functional test, AMM 12-A-27-20-00-00A-903A-A or 12-A-27-20-00-00A-903B-A Rudder trim - functional test, AMM 12-A-27-25-00-00A903A-A Elevators – examine Elevators electrical bonding straps – examine Elevators static dischargers – examine Elevator controls - examine the control cables, pulleys, rods and connections as far as possible. Move the mechanism so that you can see all parts of the cables and rods. Make sure the safety clips are fully engaged in the turnbuckles. Elevator cable tension - check, AMM 12-A-27-30-00-00A903A-A Elevator - functional test, AMM 12-A-27-30-00-00A-903A-A Horizontal stabilizer trim - operational test of trim interrupt and alternate trim switches, AMM 12-A-27-40-00-00A903A-A Horizontal stabilizer trim - functional test of trim system, AMM 12-A-27-40-00-00A-903A-A Horizontal stabilizer trim actuator top and bottom attachments - examine Flaps and flap support mechanism - examine. For flap drive arms, refer to AMM 12-A-27-51-00-00A-313A-A. Flap electrical bonding straps – examine Flap motor, actuators and flexible drive shafts – examine Flaps - functional test and asymmetry monitor test. Pre SB 27-013, AMM 12-A-27-50-00-00A-903A-A FECHA: 16-JUNIO-2014
INTERVAL
Annual Inspection Annual Inspection Annual Inspection
Annual Inspection
Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection
Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection PAG: A2.52
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Ac No. Chapt/Task
28-10/145 28-10/146 28-20/148 28-20/149
28-20/256 28-20/150 28-20/147
29-10/257 29-10/151
29-10/152
29-10/258 29-10/153
29-10/259
30-10/154
REVISIÓN: ORIGINAL
AF Hrs. Item Post SB 27-013 and MSN 401-999, AMM 12-A-27-50-0000A-903B-A Fuel Fuel tank filler caps – examine Fuel - remove a sample from each drain valve and examine for wáter Fuel filter element - remove and clean, AMM 12-A-28-2001-00A-920A-A and 12-A-28-20-01-00A-250A-A Firewall shutoff valve - operate FUEL EMERG SHUTOFF lever and make sure firewall shutoff valve opens and closes fully to each dead stop. Make sure movement is free and check if initial pull out force at lever outer end is below 10 lbf (44.5 N) Fuel system components - examine Engine Driven fuel Pump (EDP) – examine Fuel tank vent valve and flame arrestor - operational test, AMM 12-A-28-20-07-00A-903A-A Hydraulic Power Power pack - examine, specially for leaks and cracks on the end plates and where motor is attached Low pressure filter blockage indicator - make sure that it has not come out. If indicator found out, do the inspection/checkprocedure, AMM 12-A-29-10-04-00A313A-A Hydraulic system, MSN 101-230 - check fluid sensor and level using maintenance switch box. Fill as necessary, AMM 12-A-29-00-00-00A-902A-A. MSN 231-999 - make sure fluid level indicator on the reservoir tank shows full. Fill as necessary, AMM 12-A-2900-00-00A-902B-A Nitrogen accumulator - check nitrogen pressure and fill as necessary, AMM 12-A-29-10-02-00A-901A-A Reservoir tank - make sure nitrogen pressure is correct. Pressurize as necessary MSN 101-230, AMM 12-A-29-00-00-00A-902A-A MSN 231-999, AMM 12-A-29-00-00-00A-902B-A Power pack electric motor shaft seal drain fluid collector bottle (Post SB 29-002 and MSN 181-999) - remove, clean and re-install Ice and Rain Protection Wing and horizontal stabilizer airfoil de-ice boots inspection/check, AMM 12-A-30-10-00-00A-313A-A FECHA: 16-JUNIO-2014
INTERVAL
Annual Inspection Annual Inspection Annual Inspection
Annual Inspection
Annual Inspection Annual Inspection Annual Inspection
Annual Inspection
Annual Inspection
Annual Inspection
Annual Inspection
Annual Inspection
Annual Inspection
Annual Inspection
PAG: A2.53
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Ac No. Chapt/Task 30-10/155
30-10/260 30-20/261 30-20/156 30-30/157
30-40/262 30-60/158 30-60/159
32-10/163 32-10/162 32-10/164 32-10/263 32-10/165 32-10/264
32-20/168
32-20/167 32-20/169 32-20/265 32-20/166
REVISIÓN: ORIGINAL
AF Hrs. Item Inertial separation system - operational test. MSN 101-320 and 322-400, AMM 12-A-30-20-00-00A903A-A MSN 321 and 401-999, AMM 12-A-30-20-00-00A-903B-A Airfoil de-ice system - functional test, AMM 12-A-30-10-0000A-903A-A Air by-pass door and operating mechanism - examine and lubricate with minimum quantity of P10-001 Engine air intake de-ice lip - look for signs of gas leaks none are permitted Probes de-ice system - operational test. Single P-S system, AMM 12-A-30-30-10-00A-903A-A Dual system and P-S indicator, AMM 12-A-30-30-20-00A903A-A MSN 321 and 401-999, AMM 12-A-30-30-20-00A-903B-A Windshield de-ice system - operational test, AMM 12-A-3040-00-00A-903A-A or 12-A-30-40-00-00A-903B-A Propeller de-ice system - inspection/check, AMM 12-A-3060-00-00A-313A-A Propeller de-ice system - operational test, AMM 12-A-3060-00-00A-903A-A Landing Gear Main landing gear legs – examine Main landing gear - for lubrication, AMM 12-A-12-20-0400A-902A-A Main landing gear compartments – examine Main landing gear electrical bonding straps – examine Main landing gear shock struts - check nitrogen pressure, AMM 12-A-32-10-00-00A-902A-A Main landing gear left and right axle bolt (Pre SB 32-006) remove and examine. Replace if damaged. Install a serviceable bolt Nose landing gear leg and steering mechanism - examine, in particular the steering rod end (Part No. 532.20.12.134) for the complete retention of bearing into the steering rod end housing. Nose landing gear - for lubrication, AMM 12-A-12-20-0400A-902A-A Nose landing gear compartment – examine Nose landing gear electrical bonding straps – examine Nose landing gear leg shock strut - check nitrogen pressure, AMM 12-A-32-20-00-00A-902A-A FECHA: 16-JUNIO-2014
INTERVAL
Annual Inspection
Annual Inspection Annual Inspection Annual Inspection
Annual Inspection
Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection
Annual Inspection
Annual Inspection Annual Inspection Annual Inspection Annual Inspection
PAG: A2.54
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Ac No. Chapt/Task 32-20/266
32-20/305
32-30/170
32-40/171 32-40/172 32-40/173 32-40/174 32-40/175
32-40/176
33-40/177
33-41/178 33-42/179 33-43/180 33-44/181 33-46/182 34-00/183 34-00/184 34-11/268
34-11/185 34-11/186
REVISIÓN: ORIGINAL
AF Hrs. Item Nose landing gear spring strut Part No. 532.20.12.250 remove, clean and lubricate, AMM 12-A-32-20-03-00A920A-A and 12-A-32-20-03-00A-250A-A Nose landing gear actuator fuselage attachment fitting (Part No. 553.10.12.326) - examine, if cracks are found replace attachment fitting, SRM 12-A-53-00-01-00A-663A-A Extension and retraction system - functional test of extension and retraction system and emergency extension system, AMM 12-A-32-30-00-00A-903A-A Mainwheels - examine. Rotate wheels, make sure bearing movement is smooth and free and no excessive play exists Mainwheel tires - examine and check tire pressure, AMM 12-A-12-10-04-00A-902A-A Nosewheel - examine. Rotate wheel, make sure bearing movement is smooth and free and no excessive play exists Nosewheel tire - examine and check tire pressure, AMM 12-A-12-10-04-00A-902A-A Brake system - apply the parking brake. Examine the brake units. Make sure that pad wear indicators protrude from housing. Fluid reservoir - replenish if necessary, AMM 12-A-12-1002-00A-902A-A Lighting Exterior lighting - operational test. MSN 101-320 and 322-400, AMM 12-A-33-40-00-00A903A-A MSN 321 and 401-999, AMM 12-A-33-40-00-00A-903B-A Landing lights – examine Taxi lights – examine Navigation and strobe lights – examine Recognition lights (if installed) – examine Beacon lights (if installed) – examine Navigation Communications and navigation antennas – examine Cockpit instruments and avionic equipment – examine Single pitot and static system - drain, AMM 12-A-34-11-0000A-040A-A Dual pitot static systems - drain, AMM 12-A-34-11-20-00A901A-A Pitot-tubes – examine Static ports – examine Oxygen FECHA: 16-JUNIO-2014
INTERVAL
Annual Inspection
Annual Inspection
Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection
Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection
PAG: A2.55
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Ac No. Chapt/Task 35-10/187 35-10/269 35-10/270
52-10/271 52-10/189 52-10/190 52-10/192
52-10/191 52-20/272 52-30/273 52-30/274 52-30/193 52-30/194
52-30/195 52-70/275
53-00/196
53-00/276 53-00/277
53-00/278 53-00/279 REVISIÓN: ORIGINAL
AF Hrs. Item High pressure relief indicator (green disk) – make sure that it is not damaged Oxygen pipelines and equipment – examine Oxygen system - operational tests, AMM 12-A-35-00-0000A-903A-A Doors Passenger/crew door, counterbalance and cable support brackets – examine Passenger/crew door seal - clean with a wet cloth, dry and examine and apply French chalk (Pt. No. P09-002) Passenger/crew door shoot bolts and door frame fittings examine Passenger/crew door hinges - examine and lubricate as necessary with minimum quantity of CPC temporary (Pt. No. P10-001) Passenger/crew door handle lock pin - make sure movement is free Emergency door - examine (door removed) Emergency door seal - clean with a wet cloth, dry, examine and apply material French chalk (Pt. No. P09-002) Cargo door – examine Cargo door seal - clean with a wet cloth, dry and examine and apply French chalk (Pt. No. P09-002) Cargo door shoot bolts, door frame fittings and hooks examine. Make sure the hook roller bushes are free to rotate. For roller bush wear limits refer to AMM 12-A-5230-00-00A-313A-A Cargo door hinges - examine and lubricate as necessary with minimum quantity of CPC-temporary (Pt. No. P10-001) Door warning system - operational test, AMM 12-A-52-7000-00A-903A-A Fuselage Fuselage external surface - examine. For aircraft that experience stone damage to the belly skin, visually examine affected areas for cracks. Rear pressure bulkhead – examine Floor top and bottom surface and seat rails – examine as far as possible with carpet and floor panels in item 0600/218 removed Baggage/freight net mounting plates attachment bolts and surrounding structure - examine for corrosión Baggage compartment – examine FECHA: 16-JUNIO-2014
INTERVAL
Annual Inspection Annual Inspection Annual Inspection
Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection
Annual Inspection
Annual Inspection Annual Inspection
Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection PAG: A2.56
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Ac No. Chapt/Task 53-00/280
53-00/337
55-10/197 55-10/319 55-30/198
55-30/199
55-30/281 56-10/200 56-20/201
57-00/202 57-00/282 57-00/283 57/00/284 61-10/203 61-10/285
61-20/286
71-00/205
71-00-301
REVISIÓN: ORIGINAL
AF Hrs. Item Rear fuselage internal structure - examine as far as possible, in particular examine battery mounting tray for corrosión Carry through frames 21 and 24 - Inspection/Check, AMM 12-A-53-20-02-00A-313A-A Stabilizers Horizontal stabilizer external surface – examine Horizontal/vertical stabilizer attachment Inspection/Check, AMM 12-A-55-00-00-00A-361A-A Vertical stabilizer external surface - examine, specially around rear spar top rivets. If cracks are found refer to SRM 12-A-55-00-01-00A-664A-A for repair procedure Vertical stabilizer rear spar strap and lower aft fairing shear plate (Pre SB 55-002) - examine, if wear is found refer to SB 55-002 Vertical stabilizer electrical bonding straps – examine Windows Windshield LH and RH - examine, AMM 12-A-56-00-00-00A313A-A Cockpit and cabin windows - examine, AMM 12-A-56-0000-00A-313A-A Wing Wing external surfaces – examine Wing tip static dischargers – examine Wing internal surfaces and flap compartment – examine as far as possible with panels in item 06-00/218 removed Wing to fuselage attachments - examine as far as Posible Propeller Propeller blades - examine. Repair blades as necessary Ref. Hartzell MM Propeller hub - remove spinner dome and examine propeller hub. Install spinner dome, AMM 12-A-61-10-0100A-920A-A Propeller governor, overspeed governor and beta controls examine Power Plant Engine tubular mounting frame and shockmounts examine. Replace shockmount if cracks in elastomer are more than 1 in (25,4 mm) long and/or 0.06 in (1,5 mm) deep Engine tubular mounting frame firewall attachment fittings - examine with firewall insulation blanket removed as FECHA: 16-JUNIO-2014
INTERVAL
Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection
Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection
Annual Inspection
Annual Inspection PAG: A2.57
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Ac No. Chapt/Task
71-00/206
71-00/209
74-00/288
76-00/210 76-00/211 76-00/304 76-00/303
78-00/214 79-00/215
79-20/289 79-30/290 Job Close Up 25-10/297
25-20/299 06-00/219
REVISIÓN: ORIGINAL
AF Hrs. Item necessary. If cracked, blistered or flaking paint is found on the mounting frame refer to SRM 12-A-54-20-00-00A-663AA Power plant and accessories - examine. Refer to P&WC EMM 72-00-00 Periodic inspection and do the 100 hour and minor inspection items Engine drain mast and tank - for fuel leaks (no leaks permitted) and drain (no excessive leaks) Ignition Ignition system - operational test, AMM 12-A-74-00-0000A-903A-A Engine Controls Engine controls in engine compartment – examine Beta slip ring carbon block - make sure gap is not more than 0.01in (0.25mm) Cockpit control quadrant - examine. Power controls - operational test, AMM 12-A-76-10-0000A-903A-A Manual override - operational test, AMM 12-A-76-20-0000A-903A-A Exhaust Exhaust stubs – examine Oil Oil filler cap/dipstick - energize aircraft electrical system, AMM 12-A-24-00-00-00A-901A-A. Remove filler cap, examine and make sure the seal is in good condition. Set and hold AIR/GROUND switch to GROUND and make sure after 60 seconds the CAWS OIL QTY caption comes on. Install filler cap and make sure the locking mechanism operates correctly. Engine oil cooler - examine. Make sure outlet door has full and free movement Oil system chip detector indication system - operational test, AMM 12-A-79-30-01-00A-903A-A Crew seats - install MSN 101-660, AMM 12-A-25-10-01-00A-920A-A MSN 661-999, AMM 12-A-25-10-05-00A-920A-A Passenger seats - install, AMM 12-A-25-20-01-00A-920A-A, 12-A-25-21-01-00A-920A-A, 12-A-25-22-01-00A-920A-A Close/install the following panels:11AL, 11AR, 11BL, 11BR, 12AB, 12BB, 12AL, 12AR, 12AZ, 12BB, 12BL, 12BR, 12BZ, FECHA: 16-JUNIO-2014
INTERVAL
Annual Inspection Annual Inspection
Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection
Annual Inspection Annual Inspection
Annual Inspection
Annual Inspection Annual Inspection
Annual Inspection Annual Inspection Annual Inspection
PAG: A2.58
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Ac No.
71-10/208 07-10/160 71-00/204 24-30/228 25-60/231 00-00/121 00-00/122
INTERVAL
AF Hrs. Item
Chapt/Task
12CL, 12CR, 12CZ, 12DZ, 12EL, 12ER, 12EZ, 12FL, 12FR, 12FZ, 12HZ, 21GZ, 21JZ, 21PZ, 21QZ,31AB, 31AL, 31BL, 32AB, 32AL, 32BL, 32BT, 32CL, 32CT, 32DL, 33ET, 41AT, 42AT, 42AB, 51KB, 51MB, 51NB, 52KB, 52MB, 52NB, 52OB, 52PB, 52RB, 52TB, 52SB, 61KB, 61MB, 61NB, 62KB, 62MB, 62NB, 62OB, 62PB, 62RB, 62SB, 62TB. Engine cowlings ENG43AL and ENG 43AR – close Aircraft - lower to the ground and remove the jacks, AMM 12-A-07-10-00-00A-901A-A Power plant - post inspection ground run, AMM 12-A-7100-00-00A-903A-A External power - operational test, AMM 12-A-24-30-0000A-903A-A or 12-A-24-30-00-00A-903B-A ELT - operational test, AMM 12-A-25-63-01-00A-920A-A Airworthiness Directives and Service Bulletins reviewed and complied with as required Chapter 4 and Chapter 5 - Overhaul and Replacement Schedule, and Time Limited Inspection Requirements sections reviewed and any additional requirements are complied with
Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection Annual Inspection
Annual Inspection
OVERHAUL AND REPLACEMENT SCHEDULE - SCHEDULED INSPECTIONS Procedure 1 Overhaul and Replacement Schedule COMPONENT
DISCARD INTERVAL
Chapter 24 - Electrical Power Starter-generator P/N 978.91.23.421 REVISIÓN: ORIGINAL
OVERHAUL INTERVAL
1000 flying hours
FECHA: 16-JUNIO-2014
PAG: A2.59
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 COMPONENT P/N 978.91.23.422 P/N 978.91.23.431 P/N 978.91.23.433 P/N 978.91.23.441 Generator 2 drive assembly aft bearing (smaller inner diameter) (Pre SB 24-010) Generator 2 drive assembly aft bearing (smaller inner diameter) (Post SB 24-010 and MSN 231-999) Chapter 25 - Equipment and Furnishings ELT battery Crew seat cushion (Part No.0A318-0203 installed on IPECO Seat Part No's. 959.30.01.135 and 136) Crew seat belts Passenger seat belts and extensions Chapter - 26 Fire Protection Fire extinguisher Chapter 27 - Flight controls Flap power drive unit (Part No’s 978.73.20.001 and 002) Flap power drive unit (Part No 978.73.20.003) Flap linear actuators (white colored) (Part No’s 978.73.20.302/303/304/305 and 306) Flap linear actuators (black anodized) (Part No’s 978.73.20.307/308 and 309) Flap flexible drive shafts (Part No’s 945.02.02.203/204/205 and 206) Chapter 28 – Fuel Engine driven pump Chapter 31 - Indicating/Recording MSN 321 and 401-999. CAWS CACU clock battery Chapter 61 – Propeller Propeller Chapter 71 - Power plant Engine shock mount assemblies
DISCARD INTERVAL
OVERHAUL INTERVAL
10000 flying hours 3000 flying hours
After one hour of use or as shown on the battery label 3 years (elapsed for factory new or spare part new from EASA Form 1 date) -
12 years (elapsed) 12 years (elapsed) 12 months contents check (elapsed)
4500 flying hours since new or last overhaul -
10000 flying hours or 13500 landings whichever comes first
4500 flying hours
5000 flying hours or 7000 landings whichever comes first 10000 flying hours or 13500 landings whichever comes first -
3500 flying hours
2 years (installed)
-
4000 flying hours or 6 years (Ref. Hartzell SL 61) (installed)
-
At engine overhaul, but not later than 5000 flying hours
Chapter 72 – Engine REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.60
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 COMPONENT Engine
DISCARD INTERVAL
3500 flying hours (Ref. P&WC SB 14603, latest revision) Ref. P&WC SB 14603, latest revision
-
Engine accessories
OVERHAUL INTERVAL
-
TIME LIMITED INSPECTION REQUIREMENTS - SCHEDULED INSPECTIONS Procedure 1 Time Limited Inspection Requirements ITEM Aircraft
Chapter 21 - Air Conditioning Cold air unit Heat exchanger matrix Overtemperature switch Duct overtemperature switch Water separator condenser Cabin altitude switch Cabin differential pressure switch Pressurization outflow valve and safety valve Pressurization system Vapor cycle compressor motor drive belt (if Installed)
REVISIÓN: ORIGINAL
INSPECTION REQUIREMENT
INTERVAL
Do the corrosion and corrosion protection inspections (AMM 12-A20-40-00-00A-901A-A)
AMM 12-A-20-40-00-00A-901A-A
Re-oil (AMM 12-A-21-40-01-00A902A-A) Inspection/check (AMM 12-A-21-4001-00A-313A-A) Remove and test (AMM 12-A-21-4006-00A-903A-A) Remove and test (AMM 12-A-21-6005-00A-903A-A) Clean (AMM 12-A-21-40-02-00A250A-A) Functional test (AMM 12-A-21-3007-00A-903A-A) Functional test (AMM 12-A-21-3008-00A-903A-A) Remove and clean (AMM 12-A-2130-01-00A-250A-A) Adjustment/test (AMM 12-A-21-3000-00A-903A-A) Check for tension (AMM 12-A-21-5000-00A-903A-A or 12-A-21-50-0000A-903B-A)
500 flying hours
FECHA: 16-JUNIO-2014
500 flying hours 5 years (installed) 5 years (installed) 500 flying hours 5 years (installed) 5 years (installed) 1500 flying hours or 2 years whichever comes first (installed) 1500 flying hours or 2 years whichever comes first 500 system operating Hours
PAG: A2.61
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 ITEM Vapor cycle compressor motor (if installed) Vapor cycle compressor condenser module (including motor) (if installed)
Chapter 22 - Auto Flight Servo mount (pitch, roll and yaw) Chapter 24 - Electrical Power NiCad battery or batteries (if 2nd battery installed) (Part No. 976.17.31.301) NiCad battery or batteries (if 2nd battery installed) (Part No. 976.17.31.302) Lead acid battery or batteries (if 2nd battery installed)
Starter/generator brushes Generator 2 (Part No. 524.32.12.158 Mod. B) brushes Generator 2 (Part No. 524.32.12.158 Mod. A, Mod. C and above) brushes Generator 2 drive assembly housing (Post SB 24-010 and MSN 231-999) Emergency Power Supply (if installed)
Generator 1 and 2 ground points Battery 1 and 2 (if installed) ground points Emergency Power Supply
ELT Nav Interface Unit Serial Memory Module
REVISIÓN: ORIGINAL
INSPECTION REQUIREMENT Inspection/check (AMM 12-A-21-5003-00A-313A-A) Clean per OSCMM
INTERVAL 500 system operating hours Initially at each scheduled inspection, then based on field experience the interval can be adjusted to a more effective level
Remove for clutch check (AMM 12-A22-10-00-00A-313A-A)
1000 flying hours or 12 months installed, whichever comes first
Remove and service (AMM 12-A-2430-07-00A-920A-A and CMM) Remove and service (AMM 12-A-2430-07-00A-920A-A and CMM) Remove and do a capacity test (AMM 12-A-24-30-07-00A-920A-A and CMM)
100 flying hours or 3 months whichever comes first (installed) 400 flying hours or 12 months whichever comes first (installed) Initially at 1000 flying hours or 12 months (installed) whichever comes first. If capacity above 90% then every 600 flying hours or 6 months. If capacity is between 85% and 90% then every 300 flying hours or 3 months. If capacity is below 85% replace.
Examine for wear (AMM 12-A-24-3001-00A-313A-A) Examine for wear (AMM 12-A-24-3002-00A-313A-A) Inspection/check (AMM 12-A-24-3004-00A-313A-A) Inspection/check (AMM 12-A-24-3004-00A-313A-A) Remove and do a capacity test (AMM 12-A-24-52-51-00A-920A-A and CMM) Examine the corrosion protective layer (AMM 12-A-24-30-00-00A901A-A). Remove and do a capacity test AMM 12-B-24-52-51-00-A-920A-A and CMM Discard
FECHA: 16-JUNIO-2014
200 flying hours 100 flying hours 500 flying hours 1000 flying hours 12 months (installed)
2 years
12 months (installed)
16000 flying hours or 10 years (installed), whichever comes first. Note 1
PAG: A2.62
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 ITEM
INSPECTION REQUIREMENT
INTERVAL Units which have already operated more than the allowed interval must be replaced within 500 flying hours or 6 months, whichever comes first.
Chapter 27 - Flight Controls Bonding leads to all Flight Control Surfaces
Flight control cables including auto pilot and stick pusher cables Rudder control cables tensión
Examine
Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first. 2000 flying hours or 5 years whichever comes first (installed)
Flap actuators (white colored) (Part No’s 978.73.20.302, 303, 304, 305 and 306) Flap actuators (black anodized) (Part No. 978.73.20.307, 308 and 309) Flap actuators (white colored) (Part No’s 978.73.20.302, 303, 304, 305 and 306)
Examine (AMM 12-A-27-00-00-00A313A-A) Check after replacement of any rudder control system cables (Autopilot and/or rudder) AMM 12-A-27-20-00-00A-903A-A Check after replacement of any elevator control system cables (Autopilot, Stick Pusher and/or Elevator) (AMM 12-A-27-30-00-00A903A-A) Remove, clean, inspect and lubricate inner core (AMM 12-A-27-50-0000A-902A-A) Lubricate (AMM 12-A-27-50-00-00A902A-A) Lubricate (AMM 12-A-27-50-00-00A902A-A) Backlash check (AMM 12-A-27-5003-00A-313A-A)
Flap actuators (black anodized) (Part No. 978.73.20.307, 308 and 309)
Backlash check (AMM 12-A-27-5003-00A-313B-A)
Flap electrical system (MSN 101-400 Pre SB 27013)
Do the flap electrical system maintenance practices tests (AMM 12-A-27-50-00-00A-901A-A)
200 flying hours
Operational test MSN 101-105 (AMM 12-A-28-40-00-00A-903A-A) MSN 106-999 (12-A-28-40-00-00A-903B-A)
1000 flying hours or 4 years whichever comes first (installed)
Elevator control cables tensión
Flap flexible drive shafts (Post SB 27-003) (Part No’s 945.02.02.201 and 202)
Chapter 28 – Fuel Fuel low level warning system
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
At the next scheduled inspection, but not later than 150 flying hours
At the next scheduled inspection, but not later than 150 flying hours
2000 flying hours 400 flying hours or 12 months whichever comes first (installed) 150 flying hours or 12 months whichever comes first (installed) 600 flying hours or 800 flights or 12 months whichever comes first (installed) Annual inspection or every 1000 flying hours or 1300 landings whichever comes first (installed)
PAG: A2.63
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 ITEM Fuel cross vent and outward check valve Chapter 30 - Ice and Rain Protection Airfoil de-icers
Chapter 32 - Landing Gear Main and nose wheel bearings Main landing gear axles and bushes (PC-12/45 aircraft) NLG
INSPECTION REQUIREMENT Operational test (AMM 12-A-28-1001-00A-903A-A)
1000 flying hours
Apply a surface coating of Age Master No. 1 in accordance with the manufacturers instructions
6 months (installed)
Lubricate (AMM 12-A-12-20-06-00A902A-A) Inspection/Check (AMM 12-A-32-1000-00A-313A-A)
Overhaul (Ref. CMM 02100)
NLG Steering mechanism Examine AMM 12-A-32-50-00-00A-310A-A
Chapter 34 – Navigation Static system
Altimeter
Standby magnetic compass Attitude Heading Reference System (AHRS) Transponder system (single and dual systems)
Chapter 35 – Oxygen Passenger oxygen masks Chapter 52 – Doors Passenger/Crew Door Piano Hinge REVISIÓN: ORIGINAL
INTERVAL
Tire change or 12 months installed, whichever comes first 2000 flying hours or 12 months whichever comes first (installed) Threshold 25,000 flying hours or 30,000 landings, whichever comes first. Repeat 8,300 flying hours or 10,000 landings or 6 years whichever comes first. Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 8,300 flying hours or 10,000 landings or 6 years whichever comes first.
Leak check Single system (AMM 12A-34-11-10-00A-903A-A) Dual system (AMM 12-A-34-11-20-00A-903A-A) Check calibration at an approved center in accordance with the regulation in force (Ref. FAR Part 91 411) Check swing (AMM 12-A-34-21-0000A-903A-A) Check swing (AMM 12-A-34-25-0000A-903A-A) Functional test (AMM 12-A-34-5400-00A-903A-A) or (12-A-34-54-0000A-903B-A)
2 years
Inspection/check (AMM 12-A-35-2000-00A-313A-A)
3 years (installed)
Eddy Current Inspection
Threshold 32,500 flying hours or
FECHA: 16-JUNIO-2014
2 years (installed)
2 years (installed) 2 years (installed) 2 years (installed)
PAG: A2.64
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 ITEM
INSPECTION REQUIREMENT AMM 12-A-52-00-01-00A-353A-A
Passenger/Crew Door Skin Eddy Current Inspection AMM 12-A-52-10-01-00A-353A-A
Cargo Door Piano Hinge Eddy Current Inspection AMM 12-A-52-30-00-01A-353A-A
Cargo Door Skin Eddy Current Inspection AMM 12-A-52-30-01-00A-353A-A
Passenger/crew door
Examine with trim removed (AMM 12-A-25-21-03-00A-920A-A or 12-A25-22-03-00A-920A-A). Examine the top step area around the insulation mat for corrosion. If corrosion is found, write to Pilatus for a specific repair. Examine door hinge pin and hinges (AMM 12-A-52-10-00-00A313A-A)
Cargo door Examine with trim removed (AMM 12-A-25-21-03-00A-920A-A or 12-A25-22-03-00A-920A-A). Examine door hinge pin and hinges (AMM 12A-52-30-00-00A-313A-A) Chapter 53 – Fuselage Front pressure bulkhead
REVISIÓN: ORIGINAL
Examine with insulation on engine and cockpit sides removed. If insulation on cockpit side is wet, FECHA: 16-JUNIO-2014
INTERVAL 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first. Threshold 25,000 flying hours or 30,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first. Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first. Threshold 25,000 flying hours or 30,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first. Mild Corrosive Environment: 6000 flying hours or 6 years, whichever comes first. (See Note below) Moderate Corrosive Environment: 4000 flying hours or 4 years, whichever comes first. (See Note below) Severe Corrosive Environment: 2000 flying hours or 2 years, whichever comes first. (See Note below) NOTE: Local conditions may be more or less severe. Based on field experience the interval can be adjusted to more or less frequent, until an effective interval can be set. Mild Corrosive Environment: 6000 flying hours or 6 years, whichever comes first. (See Note below) PAG: A2.65
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 ITEM
Fuselage internal bottom surface
Structure around Windows Door frames and emergency exit frame
Rear pressure bulkhead Frame 40
INSPECTION REQUIREMENT
INTERVAL
remove, dry and reinstall insulation Examine frames 10, 21, 24, 36 and frames adjacent to doors and to emergency exit, with insulation removed. If corrosion is found, examine all fuselage bottom surface with insulation removed. If insulation is wet, remove, dry and reinstall insulation Examine Examine. If insulation is installed in the door frames and is wet, remove and discard it (no longer installed on production) Examine with trim removed
Moderate Corrosive Environment: 4000 flying hours or 4 years, whichever comes first. (See Note below) Severe Corrosive Environment: 2000 flying hours or 2 years, whichever comes first. (See Note below) NOTE: Local conditions may be more or less severe. Based on field experience the interval can be adjusted to more or less frequent, until an effective interval can be set. Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first
Eddy Current Inspection AMM 12-A-53-30-02-00A-353A-A Chapter 55 – Stabilizers Horizontal stabilizer internal surfaces and horizontal/vertical stabilizer interface
Examine as far as possible with panels removed
Vertical stabilizer internal surfaces Examine as far as posible with panels removed
Vertical Stabilizer Forward Attachment to Frame 40 Eddy Current Inspection AMM 12-A-55-30-03-00A-353A-A
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
Mild Corrosive Environment: 6000 flying hours or 6 years, whichever comes first. (See Note below) Moderate Corrosive Environment: 4000 flying hours or 4 years, whichever comes first. (See Note below) Severe Corrosive Environment: 2000 flying hours or 2 years, whichever comes first. (See Note below) NOTE: Local conditions may be more or less severe. Based on field experience the interval can be adjusted to more or less frequent, until an effective interval can be set. Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings, whichever comes first PAG: A2.66
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 ITEM
INSPECTION REQUIREMENT
Rudder Trim Tab
Chapter 56 – Windows Cockpit side Windows Chapter 57 – Wing Wing internal surfaces and flap compartment Landing gear compartments
Wing to fuselage attachments
Examine AMM 12-A-55-40-04-00A-310A-A
Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first
Inspection/Check (refer to DM 12-A56-11-02-00A-313A-A)
11000 flying hours or 10 years installed, whichever comes first
Examine as far as possible with all wing panels removed Examine, especially main and rear spar parts
Mild Corrosive Environment: 6000 flying hours or 6 years, whichever comes first. (See Note below) Moderate Corrosive Environment: 4000 flying hours or 4 years, whichever comes first. (See Note below) Severe Corrosive Environment: 2000 flying hours or 2 years, whichever comes first. (See Note below) NOTE: Local conditions may be more or less severe. Based on field experience the interval can be adjusted to more or less frequent, until an effective interval can be set. 11000 flying hours or 10 years, whichever comes first
Examine attachment fittings with wings removed (AMM 12-A-57-0000-00A-313A-A)
Aileron Trim Tab Examine AMM 12-A-57-60-04-00A-310A-A
Wing Tips Examine AMM 12-A-57-33-00-00A-310A-A
Wing Skin around drain holes
REVISIÓN: ORIGINAL
INTERVAL
Eddy Current Inspection AMM 12-A-57-20-01-00A-353A-A FECHA: 16-JUNIO-2014
Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first Threshold 32,500 flying hours or 42,000 landings, whichever comes first. Repeat 12,500 flying hours or 15,000 landings or 6 years, whichever comes first Threshold 25,000 flying hours or 30,000 landings, whichever comes PAG: A2.67
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 ITEM
INSPECTION REQUIREMENT
INTERVAL first. Repeat 2,500 flying hours or 3,000 landings, whichever comes first.
Chapter 61 – Propeller Propeller Chapter 71 - Power Plant Power plant
Oil pressure transducer electrical connector (Pre SB 79-004) Engine torque and stick pusher torque transducers electrical connectors Chapter 76 - Engine Controls Propeller feathering microswitches
Lubricate (AMM 12-A-12-20-05-00A902A-A) Torque Limiter Test Performance Test (AMM 12-A-71-00-00-00A-903A-A, Table 501) Clean (AMM 12-A-71-00-03-00A250A-A) Clean (AMM 12-A-71-00-03-00A250A-A)
400 flying hours or 12 months whichever comes first (installed) 500 flying hours or 12 months whichever comes first (installed). (The tests are part of the power plant Annual Inspection Requirements) 500 flying hours or 12 months whichever comes first (installed) 500 flying hours or 12 months whichever comes first (installed)
Functional test (AMM 12-A-76-103000 flying hours or 12 months 02-00A-903A-A) whichever comes first TABLE 27 TIME LIMITED INSPECTION REQUIREMENTS - RVSM AIRCRAFT Static system Leak check 2 years AMM 12-B-34-11-00-00A-903A-A Transponder system (single and dual system) Functional test 2 years (installed) AMM 12-B-34-54-00-00A-903A-A or 12-B-34-54-00-00A-903B-A or 12-B34-54-10-00A-903A-A or 12-B-34-5410-00A-903B-A Static ports critical area Inspection/check 12 months AMM 12-B-53-30-01-00A-313A-A Static ports plate height Inspection/check 2 years AMM 12-B-34-11-12-00A-313A-A Altitude and vertical speed indication Functional test 2 years AMM 12-B-34-14-00-00A-903B-A
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.68
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45
INSPECTION ENGINES Y PROPELLER PILATUS PC-12/45 ENGINE PRATT & WHITNEY No. DE SERIE PROPELLER HARTZELL No. DE SERIE
PT6A-67B PCE-PR0456 HC-E4A-3D KX-167
Periodic Inspection
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.69
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.70
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.71
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.72
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.73
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.74
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Hot Section Inspection
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.75
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45 Fault Isolation
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.76
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.77
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.78
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.79
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.80
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
PROGRAMA DE MANTENIMIENTO PARA LA AERONAVE PILATUS PC-12/45
REVISIÓN: ORIGINAL
FECHA: 16-JUNIO-2014
PAG: A2.81
LOTE 1,2 Y 3, CARRETERA LIBRE A SALINAS KM 1.7 AEROPUERTO INTERNACIONAL DEL NORTE CIÉNEGA DE FLORES, NUEVO LEON, C.P. 65550.
Related documents
PROG MTTO PC12-45 - copia
81 Pages • 21,603 Words • PDF • 2 MB
C1_CURSO_A_PROF_BIOLOGIA - Copia - Copia
32 Pages • 14,838 Words • PDF • 3.5 MB
LAB01_Ponto-a-Ponto - Copia
8 Pages • 1,374 Words • PDF • 463 KB
Manual ISAK - Copia
139 Pages • 16,466 Words • PDF • 2 MB
pdf BOB ESPONJA copia
12 Pages • PDF • 22 MB
INSTRUCTIVO PREINSCRIPCIÓN SIU ESCUGEN - copia
20 Pages • 1,011 Words • PDF • 981 KB
Fangirl - Rainbow Rowell - Copia
251 Pages • 114,546 Words • PDF • 1.3 MB
Histo PPGE 45 anos - Copia
27 Pages • 11,679 Words • PDF • 205.7 KB
SOLICITUD ALMOTORES (2) (2) - copia
2 Pages • 1,164 Words • PDF • 384.1 KB
Bad Boy Nico - Copia
108 Pages • 31,579 Words • PDF • 449.3 KB
Paulo-Romeiro-SuperCrentes - Copia
67 Pages • 22,549 Words • PDF • 407.1 KB
2.Confiabilidad copia
2 Pages • 935 Words • PDF • 645.7 KB