W DOC AIRBUS | AMM A320F

Detailed Inspection of Pylon Spigot Receptacle Upper Surface, and Upper Spar Surrounding Structure


TASK 54-51-00-220-815-A
Detailed Inspection of Pylon Spigot Receptacle Upper Surface, and Upper Spar Surrounding Structure


WARNING: BE CAREFUL WHEN YOU DO WORK ON THE ENGINE AFTER SHUTDOWN. THE ENGINE CAN STAY HOT FOR A LONG TIME. IF YOU DO NOT OBEY THIS INSTRUCTION, INJURY CAN OCCUR.
WARNING: PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU START A TASK ON OR NEAR:
  • THE FLIGHT CONTROLS
  • THE FLIGHT CONTROL SURFACES
  • THE LANDING GEAR AND THE RELATED DOORS
  • COMPONENTS THAT MOVE.
MOVEMENT OF COMPONENTS CAN KILL OR CAUSE INJURY TO PERSONS AND/OR CAN CAUSE DAMAGE TO THE EQUIPMENT.
WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
CAUTION: DO NOT APPLY TEMPORARY PROTECTION SYSTEM (TPS) ON THE INSPECTION AREA. IF YOU APPLY TPS ON THE INSPECTION AREA, YOU CAN CAUSE DAMAGE TO THE AIRCRAFT.
ZONE: 415
ZONE: 425
ZONE: 470
ZONE: 480
FIN: 4020KM1
FIN: 4020KM2
1. Reason for the Job
Refer to the MPD TASK: 545317-01
DETAILED INSPECTION OF PYLON SPIGOT RECEPTACLE UPPER SURFACE, AND UPPER SPAR SURROUNDING STRUCTURE.
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
No specific
1
FLASHLIGHT
No specific
1
MIRROR - INSPECTION
No specific
AR
WARNING NOTICE(S)
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.08BAA9)
Non Aqueous Cleaner-General - -
(Material No.14SBA1)
Textile-Lint free Cotton -
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
415
LOWER PYLON
425
LOWER PYLON
470
ENGINE 1 AFT PYLON
480
ENGINE 2 AFT PYLON
471AL, 471BL, 472AR, 472BR, 481AL, 481BL, 482AR, 482BR
 D. Referenced Information
REFERENCE
DESIGNATION
TASK 51-78-00-916-001-A
Application of Temporary Protection System (TPS)
TASK 54-53-11-000-806-A
Removal of the Pylon-to-Wing Access Panels and Doors
TASK 54-53-11-400-806-A
Installation of the Pylon-to-Wing Access Panels and Doors
TASK 78-30-00-040-807-A
Deactivation of the Thrust Reverser System for Nacelle Maintenance (ICU)
TASK 78-30-00-440-807-A
Reactivation of the Thrust Reverser System after Nacelle Maintenance (ICU)
SRM 511100
(for corrective action)
SRM 512200
(for corrective action)
3. Job Set-up
Subtask 54-51-00-941-105-A
A. Safety Precautions
   (1) On the center pedestal, on ENG panel 115VU:
     (a) Make sure that the ENG/MODE selector switch is in the NORM position.
     (b) Make sure that the ENG/MASTER 1(2) control switch was in the OFF position not less than five minutes before you do this procedure.
     (c) Put a WARNING NOTICE(S) in position to tell persons not to operate the ENG/MODE selector switch and the ENG/MASTER 1(2) control switch.
   (2) On the ENG section of maintenance panel 50VU:
     (a) Make sure that the ON legend of the FADEC GND PWR/1(2) pushbutton switch is off.
     (b) Put a WARNING NOTICE(S) in position to tell persons not to energize FADEC 1(2).
Subtask 54-51-00-040-101-A
B. Deactivation of the Thrust Reverser
WARNING: MAKE SURE THAT THE THRUST REVERSER IS LOCKED. IF NOT, THE THRUST REVERSER CAN OPERATE ACCIDENTALLY AND CAUSE INJURY TO PERSONNEL AND/OR DAMAGE TO THE REVERSER.
   (1) Make the thrust reverser unserviceable for maintenance (Ref. AMM TASK 78-30-00-040-807).
Subtask 54-51-00-010-109-A
C. Removal of the Panels
   (1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position.
     (a) For the left pylon, in zone 470
     (b) For the right pylon, in zone 480.
   (2) Remove the pylon-to-wing access panels and doors (Ref. AMM TASK 54-53-11-000-806):
     (a) For the left pylon: 471AL 471BL 472AR 472BR
     (b) For the right pylon: 481AL 481BL 482AR 482BR
Subtask 54-51-00-110-103-A
D. Preparation of the Inspection Area
   (1) Make sure that the inspection area is sufficiently clean to do a satisfactory inspection of the area.
   (2) If it is not sufficiently clean, clean the inspection area with Non Aqueous Cleaner-General - - (Material No.08BAA9) and Textile-Lint free Cotton - (Material No.14SBA1) .
   (3) Make sure that there is no Temporary Protection System (TPS) layer and if there is a TPS layer, remove it (Ref. AMM TASK 51-78-00-916-001).
   (4) Use a FLASHLIGHT and a MIRROR - INSPECTION, if necessary.
4. Procedure
Subtask 54-51-00-220-096-A
A. Inspection
   (1) Do a detailed inspection of the pylon spigot receptacle upper surface and upper spar surrounding structure.
   (2) Make sure that there is no:
     (a) Corrosion damage:
  • If you find corrosion damage, refer to Structural Repair Manual SRM 512200 for types of corrosion, inspection, removal and corrosion protection.
     (b) Other damage (scratches, cracks, gouges, dents, creases):
  • If you find this type of damage, refer to Structural Repair Manual SRM 511100 for damage classification and corrective action.
5. Close-up
Subtask 54-51-00-410-116-A
A. Installation of the Panels
   (1) Install the pylon-to-wing access panels and doors (Ref. AMM TASK 54-53-11-400-806):
     (a) For the left pylon: 471AL 471BL 472AR 472BR
     (b) For the right pylon: 481AL 481BL 482AR 482BR.
Subtask 54-51-00-440-100-A
B. Reactivation of the Thrust Reverser
   (1) Make the thrust reverser serviceable after maintenance (Ref. AMM TASK 78-30-00-440-807).
Subtask 54-51-00-942-084-A
C. Aircraft Maintenance Configuration
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Remove the access platform(s).
   (3) Remove the WARNING NOTICE(S).
[Rev.10 from 2021] 2026.04.01 02:00:10 UTC