W DOC AIRBUS | AMM A320F

Removal of the Bevel Gearbox


TASK 27-54-48-000-001-A
Removal of the Bevel Gearbox


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.
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.
ZONE: 573
ZONE: 575
ZONE: 673
ZONE: 675
FIN: 6217CM
FIN: 6267CM
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)
No specific
AR
SAFETY BARRIER(S)
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
AR
WARNING NOTICE(S)
98D27604000000
1
COLLAR-SAFETY, SPOILER
98D27604004000
1
COLLAR SAFETY SPOILER
98D27803000000
1
LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
573
FIXED STRUCT FROM STA 1800 TO STA 4666
575
AFT OUTBD SE OF WING AND TE FIXED STRUCT
673
FIXED STRUCT FROM STA 1800 TO STA 4666
675
AFT OUTBD SE OF WING AND TE FIXED STRUCT
FOR [6217CM] (FLAP BEVEL GEARBOX)
573CB, 573FB, 575AB
FOR [6267CM] (FLAP BEVEL GEARBOX)
673CB, 673FB, 675AB
 C. Referenced Information
REFERENCE
DESIGNATION
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 27-54-45-000-009-A
Removal of Torque Shaft
TASK 27-60-00-866-002-A
Extension-Retraction of the Spoilers for Maintenance
FOR [6217CM] (FLAP BEVEL GEARBOX)
TASK 57-51-37-000-002-A
Removal of the Access Panels 571AB(671AB), 573AB(673AB), 573BB(673BB), 573CB(673CB), 573EB(673EB)
TASK 57-51-37-000-003-A
Removal of the Access Panel
TASK 57-51-37-000-004-A
Removal of the Access Panels 575AB(675AB), 575BB(675BB), 575CB(675CB), 575DB(675DB), 575EB(675EB), 575FB(675FB), 575GB(675GB), 575HB(675HB)
FOR [6267CM] (FLAP BEVEL GEARBOX)
TASK 57-51-37-000-002-A
Removal of the Access Panels 571AB(671AB), 573AB(673AB), 573BB(673BB), 573CB(673CB), 573EB(673EB)
TASK 57-51-37-000-003-A
Removal of the Access Panel
TASK 57-51-37-000-004-A
Removal of the Access Panels 575AB(675AB), 575BB(675BB), 575CB(675CB), 575DB(675DB), 575EB(675EB), 575FB(675FB), 575GB(675GB), 575HB(675HB)
3. Job Set-up
Subtask 27-54-48-860-050-A
A. 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) Fully extend the flaps (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.
   (3) Put the WARNING NOTICE(S) in position on panel 114VU to tell persons not to operate the flap/slat controls.
   (4) Put spoiler No. 1 in the extended maintenance position (Ref. AMM TASK 27-60-00-866-002).
   (5) Put the 98D27604000000 COLLAR-SAFETY, SPOILER or 98D27604004000 COLLAR SAFETY SPOILER on the piston rod of the servo-control.
Subtask 27-54-48-865-050-A
B. 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/WTB/FLP/SYS212CVP20
121VUFLIGHT CONTROLS/FLP/CTL AND/MONG/SYS28CVQ21
122VUFLIGHT CONTROLS/WTB/FLP/SYS110CVS07
Subtask 27-54-48-941-050-A
C. Safety Precautions
   (1) Put the SAFETY BARRIER(S) in position.
Subtask 27-54-48-010-050-A
D. Get Access
   (1) Put the ACCESS PLATFORM 3M (10 FT) in position in zones 573(673) and 575(675).
   (2) Remove the access panels:
     (a) FOR [6217CM] (FLAP BEVEL GEARBOX)
       1 573CB (Ref. AMM TASK 57-51-37-000-002)
       2 573FB (Ref. AMM TASK 57-51-37-000-003)
       3 575AB (Ref. AMM TASK 57-51-37-000-004).
     (b) FOR [6267CM] (FLAP BEVEL GEARBOX)
       1 673CB (Ref. AMM TASK 57-51-37-000-002)
       2 673FB (Ref. AMM TASK 57-51-37-000-003)
       3 675AB (Ref. AMM TASK 57-51-37-000-004).
4. Procedure
Subtask 27-54-48-020-050-A
A. Removal of the Bevel Gearbox
   (1) Remove the torque shaft (1) (Ref. AMM TASK 27-54-45-000-009).
   (2) Remove the bolts (5) and the washers (4) from the bevel gearbox (3).
   (3) Remove the bevel gearbox (3) from the trailing edge rib and the torque shaft (2).
[Rev.10 from 2021] 2026.03.31 23:54:00 UTC