W DOC AIRBUS | AMM A320F

Installation of the Aft Pylon Fairing (APF)


TASK 54-56-00-400-802-A
Installation of the Aft Pylon Fairing (APF)


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: BEFORE YOU START WORK, YOU MUST PUT ON A SAFETY HARNESS AND ATTACH IT TO THE ACCESS PLATFORM. WITHOUT A SAFETY HARNESS, YOU CAN FALL. THIS CAN KILL YOU OR CAUSE YOU INJURY.
CAUTION: BEFORE YOU INSTALL/REMOVE THE GSE-TOOL, READ THE INSTRUCTIONS IN THE APPLICABLE GSE INSTRUCTION MANUAL. WHILE YOU OPERATE THIS TOOL, CAREFULLY OBEY THEM. IF YOU DO NOT OBEY THE INSTRUCTIONS, DAMAGE TO EQUIPMENT CAN OCCUR.
ZONE: 470
ZONE: 480
FIN: 4020KM1 ** ON A/C NOT FOR ALL
FIN: 4020KM2 ** ON A/C NOT FOR ALL
1. Reason for the Job
Self explanatory
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
Torque wrench: range to between 1.06 and 0.82 m.daN (93.81 and 72.57 lbf.in ) T
No specific
Torque wrench: range to between 1.38 and 1.06 m.daN (122.12 and 93.81 lbf.in ) T
No specific
Torque wrench: range to between 1.61 and 1.31 m.daN (142.48 and 115.93 lbf.in ) T
98D54403004000
1
R/I PYLON APF
98D54403010000
1
RI APF INSTALL SUPPORT
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
470
ENGINE 1 AFT PYLON
480
ENGINE 2 AFT PYLON
473AL, 473AR, 483AL, 483AR
FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
437AL, 438AR, 451AL, 452AR
FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
447AL, 448AR, 461AL, 462AR
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 54-54-00-400-804-A
Installation of the Closing Sheet Metal
TASK 54-56-11-010-801-A
Opening of the Rear Mount Fairing (RMF) Door
TASK 54-56-11-410-801-A
Closing of the Rear Mount Fairing (RMF) Door
TASK 71-00-00-860-833-A
Procedure to Prevent Engine Motoring
TASK 71-13-00-010-802-A
Opening of the Fan Cowl Doors
TASK 71-13-00-410-802-A
Closing of the Fan Cowl Doors
TASK 78-30-00-040-805-A
Deactivation of the Thrust Reverser System for Ground Maintenance
TASK 78-30-00-440-805-A
Reactivation of the Thrust Reverser System after Ground Maintenance
TASK 78-36-00-010-802-A
Opening of the Thrust Reverser Cowl-Doors
TASK 78-36-00-410-802-A
Closing of the Thrust Reverser Cowl-Doors
3. Job Set-up
Subtask 54-56-00-941-067-A ** ON A/C NOT FOR ALL
A. Safety Precautions
   (1) Make sure that you did the procedure to prevent engine motoring
(Ref. AMM TASK 71-00-00-860-833).
Subtask 54-56-00-010-059-A ** ON A/C NOT FOR ALL
B. Get Access
   (1) Make sure that the fan cowl doors are open (Ref. AMM TASK 71-13-00-010-802):
     (a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
437AL 438AR
     (b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
447AL 448AR.
   (2) Make sure that the thrust-reverser cowl doors are open (Ref. AMM TASK 78-36-00-010-802):
     (a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
451AL 452AR
     (b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
461AL 462AR.
   (3) Make sure that the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE is in position:
     (a) For the left pylon, in zone 470
     (b) For the right pylon, in zone 480.
   (4) Make sure that the Rear Mount Fairing (RMF) door is open (Ref. AMM TASK 54-56-11-010-801):
     (a) For the left pylon: 473AL 473AR
     (b) For the right pylon: 483AL 483AR.
Subtask 54-56-00-040-063-A ** ON A/C NOT FOR ALL
C. 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 sure that the thrust reverser is unserviceable for maintenance (Ref. AMM TASK 78-30-00-040-805).
4. Procedure
Subtask 54-56-00-420-059-B ** ON A/C NOT FOR ALL
A. Installation of the Aft Pylon Fairing (APF)
F Aft Pylon Fairing ** ON A/C NOT FOR ALL
CAUTION: MAKE SURE THAT YOU INSTALL EACH OF THE SCREWS IN ITS CORRECT POSITION. THE SCREWS HAVE DIFFERENT LENGTHS. IF YOU DO NOT INSTALL EACH OF THE SCREWS IN ITS CORRECT POSITION, YOU CAN CAUSE DAMAGE.
   (1) Install the 98D54403010000 RI APF INSTALL SUPPORT on the APF (2). To do this:
     (a) Put the tension bar (14) in position on the bootstrap fittings (13) and install the quick locking pins (15).
     (b) Put the APF (2) in position with the 98D54403004000 R/I PYLON APF (12).
     (c) Put the strap (16) through the strainer (20), before you install the hooks (17).
     (d) Install the hooks (17) on the shackles (18).
     (e) Put the plier (19) on the APF leading edge and adjust the strap (16) in the correct direction.
     (f) Put the protection (21) around the strainer (20).
     (g) Pull the strap (16) to compress the exhaust nozzle seals.
   (2) When you install the APF (2) again, make sure that the pylon holes and the APF holes are correctly aligned. If it is not correctly aligned:
     (a) Loosen the screws (3) of the primary structure.
     (b) Adjust the primary structure strip (4) to align the holes.
     (c) Tighten the screws (3).
   (3) Install the screws (5).
   (4) TORQUE the screws (5) to between 1.06 and 0.82 m.daN (93.81 and 72.57 lbf.in ) T.
   (5) Install the washers (7) and the bolts (6).
   (6) Install the washers (9) and (10), the screws (11) and the nuts (8).
   (7) TORQUE the bolts (6) to between 1.61 and 1.31 m.daN (142.48 and 115.93 lbf.in )
T.
   (8) TORQUE the nuts (8) to between 1.38 and 1.06 m.daN (122.12 and 93.81 lbf.in )
T.
   (9) Install the screws (1) and tighten them.
   (10) Remove the
98D54403004000 R/I PYLON APF (12) from the APF (2).
   (11) Remove the 98D54403010000 RI APF INSTALL SUPPORT from the APF (2). To do this:
     (a) Adjust the strainer (20) to release the tension in the strap (16).
     (b) Remove the plier (19) from the APF leading edge and release the strap (16).
     (c) Remove the protection (21) from the strainer (20).
     (d) Remove the hooks (17) from the shackles (18).
     (e) Remove the strap (16) through the strainer (20).
     (f) Remove the quick locking pins (15) and tension bar (14) from the bootstrap fittings (13).
Subtask 54-56-00-410-053-A ** ON A/C NOT FOR ALL
B. Installation of the Components
   (1) Install the closing sheet metal (Ref. AMM TASK 54-54-00-400-804).
   (2) Close the Rear Mount Fairing (RMF) door (Ref. AMM TASK 54-56-11-410-801):
     (a) For the left pylon: 473AL 473AR
     (b) For the right pylon: 483AL 483AR.
Subtask 54-56-00-820-055-B ** ON A/C NOT FOR ALL
C. Check of the Clearances
F Clearance Check ** ON A/C NOT FOR ALL
   (1) Make sure that the clearance between the APF (1) and the RMF door (4), J1 is 4.2 +2 mm or -2 mm (0.1654 +0.0787 in. or -0.0787 in.).
   (2) Make sure that the clearance between the APF (1) and the pylon (3), J2 is 3 +2.1 mm or -2.1 mm (0.1181 +0.0827 in. or -0.0827 in.).
   (3) Make sure that the clearance between the APF (1) and the closing sheet metal (2), J3 is 2 +2 mm or -2 mm (0.0787 +0.0787 in. or -0.0787 in.).
   (4) Make sure that the out-of-flush dimension between the APF (1) and the RMF door (4), A1 is 0 +0.7 mm or -0.5 mm (0.0000 +0.0276 in. or -0.0197 in.).
   (5) Make sure that the out-of-flush dimension between the APF (1) and the pylon (3), A2 is 0 +0.7 mm or -0.5 mm (0.0000 +0.0276 in. or -0.0197 in.).
   (6) Make sure that the out-of-flush dimension between the APF (1) and the closing sheet metal (2), A3 is 0 +0.6 mm or -0.6 mm (0.0000 +0.0236 in. or -0.0236 in.).
   (7) If the values of the peripheral clearances and the out-of-flush dimensions do not agree with the permitted values given above, contact Airbus.
5. Close-up
Subtask 54-56-00-410-054-A ** ON A/C NOT FOR ALL
A. Close Access
   (1) Close the thrust reverser cowl-doors (Ref. AMM TASK 78-36-00-410-802):
     (a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
451AL 452AR
     (b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
461AL 462AR.
   (2) Close the fan cowl doors (Ref. AMM TASK 71-13-00-410-802):
     (a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
437AL 438AR
     (b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
447AL 448AR.
Subtask 54-56-00-440-061-A ** ON A/C NOT FOR ALL
B. Reactivation of the Thrust Reverser
   (1) Make the thrust reverser serviceable after maintenance (Ref. AMM TASK 78-30-00-440-805).
Subtask 54-56-00-942-059-A ** ON A/C NOT FOR ALL
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 02:03:27 UTC