W DOC AIRBUS | AMM A320F

Removal of the 63.5 Degree Bevel-Gearbox


TASK 27-84-43-000-001-A
Removal of the 63.5 Degree Bevel-Gearbox


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.
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.
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.
ZONE: 190
FIN: 6009CM
FIN: 6011CM
FIN: 6059CM
FIN: 6061CM
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
AR
WARNING NOTICE(S)
98D27504030001
1
LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT
98D27803000000
1
LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION
FOR [6011CM] (SLAT BEVEL GEARBOX)
FOR [6061CM] (SLAT BEVEL GEARBOX)
No specific
1
SCRAPER - NON METALLIC
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
190
BELLY FAIR, AIR CONDITIONING & HYD COMPT
FOR [6009CM] (SLAT BEVEL GEARBOX)
FOR [6011CM] (SLAT BEVEL GEARBOX)
191BB, 191BT, 191CT
FOR [6059CM] (SLAT BEVEL GEARBOX)
FOR [6061CM] (SLAT BEVEL GEARBOX)
192BT, 192CT, 192FB
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 27-00-00-480-002-A
Installation of the Flap/Slat Control-Lever Locking Tool (98D27803000000)
TASK 27-80-00-866-005-A
Retracting the Slats on the Ground
TASK 27-84-45-000-004-A
Removal of the Torque Shafts 6010CM and 6060CM
TASK 29-00-00-864-001-A
Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action
FOR [6009CM] (SLAT BEVEL GEARBOX)
FOR [6059CM] (SLAT BEVEL GEARBOX)
TASK 27-84-45-000-003-A
Removal of the Torque Shaft
FOR [6009CM] (SLAT BEVEL GEARBOX)
FOR [6011CM] (SLAT BEVEL GEARBOX)
TASK 27-50-00-400-003-A
Installation of the Lock-Torque Shaft - Flaps and Slats (98D27504030001)
TASK 53-35-11-000-001-A
Removal of the Wing-to-Fuselage Fairings
TASK 53-35-13-000-002-A
Removal of the Quick-Release Access Panels from the Belly Fairing Structure
FOR [6011CM] (SLAT BEVEL GEARBOX)
FOR [6061CM] (SLAT BEVEL GEARBOX)
TASK 27-84-45-000-005-A
Removal of the Torque Shaft
FOR [6059CM] (SLAT BEVEL GEARBOX)
FOR [6061CM] (SLAT BEVEL GEARBOX)
TASK 27-50-00-400-003-A
Installation of the Lock-Torque Shaft - Flaps and Slats (98D27504030001)
TASK 53-35-11-000-001-A
Removal of the Wing-to-Fuselage Fairings
TASK 53-35-13-000-002-A
Removal of the Quick-Release Access Panels from the Belly Fairing Structure
3. Job Set-up
Subtask 27-84-43-860-053-A
A. Aircraft Maintenance Configuration
   (1) Retract the slats to the 0 degree position (Ref. AMM TASK 27-80-00-866-005).
   (2) Install the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION on the slat/flap control lever (Ref. AMM TASK 27-00-00-480-002).
   (3) Make sure that the Green and Blue hydraulic systems are depressurized and put them in the maintenance configuration (Ref. AMM TASK 29-00-00-864-001).
   (4) Put the WARNING NOTICE(S) in position to tell persons not to pressurize the hydraulic systems.
Subtask 27-84-43-865-050-A
B. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB06
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB01
** ON A/C ALL
121VUFLIGHT CONTROLS/SLT/CTL/SYS27CVR21
Subtask 27-84-43-010-051-A
C. Get Access
   (1) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position below the applicable access panels.
   (2) Remove the applicable access panels:
     (a) FOR [6009CM] (SLAT BEVEL GEARBOX), [6011CM] (SLAT BEVEL GEARBOX)
Remove access panels 191BT and 191CT (Ref. AMM TASK 53-35-11-000-001) and 191BB (Ref. AMM TASK 53-35-13-000-002).
     (b) FOR [6059CM] (SLAT BEVEL GEARBOX), [6061CM] (SLAT BEVEL GEARBOX)
Remove access panels 192BT and 192CT (Ref. AMM TASK 53-35-11-000-001) and 192FB (Ref. AMM TASK 53-35-13-000-002).
Subtask 27-84-43-481-050-A
D. Installation of the Torque Shaft Locks
   (1) Install the 98D27504030001 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT to lock the slat transmission system:
     (a) FOR [6009CM] (SLAT BEVEL GEARBOX), [6011CM] (SLAT BEVEL GEARBOX)
Lock the left slat transmission-system (Ref. AMM TASK 27-50-00-400-003).
     (b) FOR [6059CM] (SLAT BEVEL GEARBOX), [6061CM] (SLAT BEVEL GEARBOX)
Lock the right slat transmission-system (Ref. AMM TASK 27-50-00-400-003).
4. Procedure
Subtask 27-84-43-020-051-A
A. Removal of the 63.5 Degree Bevel-Gearbox
   (1) Remove torque shaft 6010CM (6060CM) (2) (Ref. AMM TASK 27-84-45-000-004).
   (2) FOR [6009CM] (SLAT BEVEL GEARBOX), [6059CM] (SLAT BEVEL GEARBOX)
     (a) Remove torque shaft 6008CM (6058CM) (3) (Ref. AMM TASK 27-84-45-000-003).
     (b) Remove the unwanted corrosion preventive compound from the bolts (7) with the SCRAPER - NON METALLIC.
     (c) Hold the bevel gearbox (4) to make sure that it does not fall.
     (d) Remove the bolts (7) and the washers (6) that attach the bevel gearbox (4) to the support bracket (5).
     (e) Remove the bevel gearbox (4).
   (3) FOR [6011CM] (SLAT BEVEL GEARBOX), [6061CM] (SLAT BEVEL GEARBOX)
     (a) Remove torque shaft 6012CM (6062CM) (1) (Ref. AMM TASK 27-84-45-000-005).
     (b) Remove the unwanted corrosion preventive compound from the bolts (10) with the SCRAPER - NON METALLIC.
     (c) Hold the bevel gearbox (8) to make sure that it does not fall.
     (d) Remove the bolts (10) and the washers (11) that attach the bevel gearbox (8) to the support bracket (9).
     (e) Remove the bevel gearbox (8).
[Rev.10 from 2021] 2026.03.31 23:56:45 UTC