W DOC AIRBUS | AMM A320F

Removal of the Torque Shaft

TASK 27-54-45-000-003-A
Removal of the Torque Shaft

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: MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING GEAR. THIS WILL PREVENT UNWANTED MOVEMENT OF THE LANDING GEAR, AND THUS POSSIBLE INJURY TO PERSONS AND DAMAGE TO THE AIRCRAFT AND/OR EQUIPMENT.
CAUTION: BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:
  • DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
  • DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
  • MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
FIN: 6206CM
FIN: 6256CM
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
AR
SAFETY BARRIER(S)
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
AR
WARNING NOTICE(S)
460005835
2
SLEEVE - GROUND LOCK
98D27504030001
1
LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT
98D27803000000
1
LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
FOR [6206CM] (FLAP XMSN TORQUE SHAFT)
571AB
FOR [6256CM] (FLAP XMSN TORQUE SHAFT)
671AB
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 27-50-00-400-003-A
Installation of the Lock-Torque Shaft - Flaps and Slats (98D27504030001)
TASK 27-50-00-866-008-A
Extension of the Flaps on the Ground
TASK 27-50-00-866-008-A-01
Extension of the Flaps/Slats on the Ground
TASK 32-12-00-010-001-A
Open the Main Gear Doors for Access
F Torque Shafts - Flap Power Transmission ** ON A/C NOT FOR ALL
F Torque Shafts - Flap Power Transmission ** ON A/C NOT FOR ALL
F Torque Shafts - Flap Power Transmission
3. Job Set-up
Subtask 27-54-45-941-052-A
A. Safety Precautions
   (1) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
   (2) Put a WARNING NOTICE(S) in position to tell persons not to operate the landing-gear doors.
   (3) Put a WARNING NOTICE(S) in position to tell persons not to operate the flap controls.
Subtask 27-54-45-860-052-A
B. Aircraft Maintenance Configuration
WARNING: MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS SURFACES ARE CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT.
   (1) Extend the flaps fully (Ref. AMM TASK 27-50-00-866-008).
   (2) Install the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION on the flap/slat control lever on panel 114VU.
Subtask 27-54-45-865-052-A
C. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/FLP/CTL AND MONG/SYS16CVB07
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/FLP/CTL AND MONG/SYS16CVB02
** ON A/C ALL
121VUFLIGHT CONTROLS/FLP/CTL AND/MONG/SYS28CVQ21
Subtask 27-54-45-010-052-A
D. Get Access
   (1) Open the main gear doors (Ref. AMM TASK 32-12-00-010-001).
   (2) Install the 460005835 SLEEVE - GROUND LOCK on the applicable main gear door actuator.
   (3) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in the applicable position.
   (4) Remove the applicable access panel:
     (a) FOR [6206CM] (FLAP XMSN TORQUE SHAFT)
remove 571AB
     (b) FOR [6256CM] (FLAP XMSN TORQUE SHAFT)
remove 671AB.
4. Procedure
CAUTION: BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:
  • DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
  • DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
  • MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
Subtask 27-54-45-020-052-A
A. Removal of the Torque Shaft
   (1) Install the 98D27504030001 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT on a flap torque shaft, outboard of the component that you remove (Ref. AMM TASK 27-50-00-400-003).
   (2) Remove the retaining ring (20) and the pin (13).
   (3) Remove and discard the cotter pin (22).
   (4) Remove and discard the nut (21).
   (5) Remove the washer (23), the bolt (10) and the washer (11).
   (6) Remove the bolts (24) from the seal base plate (25) and from the shroud box.
   (7) Remove the bolts (19).
   (8) Remove and discard the nuts (18).
   (9) Compress the plunging joint (15) to permit the removal of the torque shaft (14). Remove the torque shaft (14) through the seal base plate (25) at the inboard end of the shroud box.
   (10) During the removal, hold the torque shaft (14) through the opening in the forward face of the shroud box.
   (11) Remove the retaining ring (17), the pin (16) and the plunging joint (15).
[Rev.10 from 2021] 2026.03.31 23:53:24 UTC
"Aviabrain" 2025