W DOC AIRBUS | AMM A320F

Removal of the No.1 Flap Track Beam


TASK 57-51-33-000-001-A
Removal of the No.1 Flap Track Beam


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.
CAUTION: THIS PART IS A REMOVABLE STRUCTURAL COMPONENT (RSC), WHICH CAN BE MOVED BETWEEN AIRCRAFT. THUS IT CAN HAVE DIFFERENT OPERATION CONDITIONS AND A DIFFERENT LIFE RECORD (FLIGHT HOURS/FLIGHT CYCLES/CALENDAR) FROM THE AIRCRAFT IT IS INSTALLED ON OR REMOVED FROM. THE OPERATOR IS RESPONSIBLE FOR THE SPECIFIC TRACKING AND CONTINUED AIRWORTHINESS OF REMOVABLE STRUCTURAL COMPONENTS. INCORRECT MAINTENANCE OF THESE COMPONENTS CAN CAUSE A RISK FOR THE FLIGHT SAFETY.
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)
No specific
AR
SAFETY BARRIER(S)
No specific
1
WARNING NOTICE(S)
98AMS172322005
1
WRENCH-ADAPTER
98AMS172332002
1
ADAPTER-WRENCH
 B. Referenced Information
REFERENCE
DESIGNATION
TASK 27-54-49-000-001-A
Removal of the Flap Track 1 Actuator
TASK 27-54-61-000-001-A
Removal of the Inboard Flap
TASK 27-54-61-000-003-A
Removal of the Inboard Double-Slotted Flap
TASK 57-51-15-000-001-A
Removal of the Shroud Box
SRM 514211
F No.1 Flap Track Beam ** ON A/C NOT FOR ALL
F No.1 Flap Track Beam ** ON A/C NOT FOR ALL
F No.1 Flap Track Beam ** ON A/C NOT FOR ALL
F No.1 Flap Track Beam ** ON A/C NOT FOR ALL
3. Job Set-up
Subtask 57-51-33-941-050-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 the cockpit to tell persons not to operate the flaps or slats.
Subtask 57-51-33-010-050-A ** ON A/C NOT FOR ALL
B. Get Access
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) Remove the applicable inboard flap (Ref. AMM TASK 27-54-61-000-001).
   (2) Remove the applicable No.1 flap track actuator (Ref. AMM TASK 27-54-49-000-001).
   (3) Put the ACCESS PLATFORM 3M (10 FT) in position below the applicable No.1 flap track beam (1), zone 581 (681).
Subtask 57-51-33-010-050-B ** ON A/C NOT FOR ALL
B. Get Access
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) Remove the applicable inboard flap (Ref. AMM TASK 27-54-61-000-003).
   (2) Remove the applicable No.1 flap track actuator (Ref. AMM TASK 27-54-49-000-001).
   (3) Remove the LH(RH) shroud box (Ref. AMM TASK 57-51-15-000-001).
   (4) Put the ACCESS PLATFORM 3M (10 FT) in position below the applicable No.1 flap track beam (1), zone 581 (681).
Subtask 57-51-33-010-050-C ** ON A/C NOT FOR ALL
B. Get Access
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) Remove the applicable inboard flap (Ref. AMM TASK 27-54-61-000-001).
   (2) Remove the applicable No.1 flap track actuator (Ref. AMM TASK 27-54-49-000-001).
   (3) Remove the LH(RH) shroud box (Ref. AMM TASK 57-51-15-000-001).
   (4) Put the ACCESS PLATFORM 3M (10 FT) in position below the applicable No.1 flap track beam (1), zone 581 (681).
Subtask 57-51-33-865-050-A
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
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
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 57-51-33-020-053-A ** ON A/C NOT FOR ALL
A. Removal of the No.1 Flap Track Beam
WARNING: SUPPORT THE UNIT/ASSEMBLY. THE UNIT/ASSEMBLY IS HEAVY. IF YOU DO NOT SUPPORT IT, IT WILL FALL. THIS CAN CAUSE INJURY TO PERSONS, AND/OR DAMAGE TO EQUIPMENT.
   (1) Hold the flap track beam (1).
NOTE: The weight of the flap track beam (1) is 35 kg (77.2 lb).
   (2) At the X-strut:
     (a) Remove the nut (2), the bolt (8), the washer (9) and the bush (10).
   (3) At the forward mounting:
     (a) Remove and discard the cotter pins (11).
     (b) Remove the nuts (12) and the washers (13).
     (c) Remove the bolts (17), the washers (16) and the bushes (15).
     (d) If there are shims (14) and (18), remove them. Keep the shims with the beam.
   (4) At the rear mounting:
     (a) Remove the nut (20) and the bolt (22).
     (b) Remove the six HiLok pins (23) and (24), and the six HiLok collars (21) SRM 514211.
   (5) Remove the flap track beam (1).
Subtask 57-51-33-020-053-B ** ON A/C NOT FOR ALL
A. Removal of the No.1 Flap Track Beam
   (1) If necessary, remove the beam (25) from the aircraft structure as follows:
     (a) Remove and discard the rivets (26) SRM 514211.
     (b) Remove the beam (25).
WARNING: SUPPORT THE UNIT/ASSEMBLY. THE UNIT/ASSEMBLY IS HEAVY. IF YOU DO NOT SUPPORT IT, IT WILL FALL. THIS CAN CAUSE INJURY TO PERSONS, AND/OR DAMAGE TO EQUIPMENT.
   (2) Hold the flap track beam (1).
NOTE: The weight of the flap track beam (1) is 28 kg (61.7 lb).
   (3) At the front mounting:
     (a) Release the lockwasher (15).
     (b) Use the 98AMS172322005 WRENCH-ADAPTER to remove the nut (16).
     (c) Remove and discard the lockwasher (15).
     (d) Remove the bolt (11).
     (e) Remove the nut (14).
     (f) Remove the washer (13) and the hollow bolt (12).
   (4) At the rear mounting:
     (a) Remove and discard the cotter pin (2).
     (b) Remove the nut (3), the washer (4) and the bolt (10).
     (c) Release the lockwasher (6).
     (d) Use the 98AMS172332002 ADAPTER-WRENCH to remove the nut (5).
     (e) Remove and discard the lockwasher (6).
     (f) Remove the washer (7).
     (g) Remove the hollow bolt (9) and the bush (8).
   (5) Remove the flap track beam (1).
Subtask 57-51-33-020-053-C ** ON A/C NOT FOR ALL
A. Removal of the No.1 Flap Track Beam
WARNING: SUPPORT THE UNIT/ASSEMBLY. THE UNIT/ASSEMBLY IS HEAVY. IF YOU DO NOT SUPPORT IT, IT WILL FALL. THIS CAN CAUSE INJURY TO PERSONS, AND/OR DAMAGE TO EQUIPMENT.
   (1) Hold the flap track beam (1).
NOTE: The weight of the flap track beam (1) is 35 kg (77.2 lb).
   (2) At the forward mounting:
     (a) Remove the nut (14) from the bolt (12).
     (b) Remove the bolt (12) and the bush (11) from the bracket (15).
   (3) At the rear mounting:
     (a) Remove the nuts (6), the bolts (5) and the bushes (4).
     (b) Remove the nut (8) and the bush (7) from the bolt (2).
     (c) Remove the bolt (2) and the bush (3) from the bracket (10).
     (d) Lower the flap track beam (1) and remove the ball pin (9).
   (4) Remove the flap track beam (1).
Subtask 57-51-33-020-053-D ** ON A/C NOT FOR ALL
A. Removal of the No.1 Flap Track Beam
WARNING: SUPPORT THE UNIT/ASSEMBLY. THE UNIT/ASSEMBLY IS HEAVY. IF YOU DO NOT SUPPORT IT, IT WILL FALL. THIS CAN CAUSE INJURY TO PERSONS, AND/OR DAMAGE TO EQUIPMENT.
   (1) Hold the flap track beam (1).
NOTE: The weight of the flap track beam (1) is 35 kg (77.2 lb).
   (2) At the forward mounting:
     (a) Remove the nut (15) and washer (14) from the bolt (12).
     (b) Remove the bolt (12) and the bush (11) from the bracket (16).
   (3) At the rear mounting:
     (a) Remove the nuts (6), the bolts (5) and the bushes (4).
     (b) Remove the nut (8) and the bush (7) from the bolt (2).
     (c) Remove the bolt (2) and the bush (3) from the bracket (10).
     (d) Lower the flap track beam (1) and remove the ball pin (9).
   (4) Remove the flap track beam (1).
[Rev.10 from 2021] 2026.04.02 06:59:50 UTC