DOC AIRBUS | AMM A320FInstallation of the Flap-Tracks Attachment-Bracket Bearing
TASK 57-26-15-400-001-A
Installation of the Flap-Tracks Attachment-Bracket Bearing
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
C. Work Zones and Access Panels
D. Expendable Parts
E. Referenced Information
3. Job Set-up
Subtask 57-26-15-941-051-A
Subtask 57-26-15-942-050-A
[Rev.10 from 2021]
2026.04.01 02:11:43 UTC
Installation of the Flap-Tracks Attachment-Bracket Bearing
CAUTION:
BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:
1. Reason for the Job- 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.
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 | WARNING NOTICE(S) |
| No specific | Torque wrench: range to between 5.0 and 4.5 m.daN (36.87 and 33.19 lbf.ft )  | |
| No specific | Torque wrench: range to between 6.5 and 5.5 m.daN (47.94 and 40.56 lbf.ft ) | |
| No specific | Torque wrench: range to between 10.5 and 9.5 m.daN (77.43 and 70.06 lbf.ft ) | |
| 98D27803500001 | 1 | LOCKING TOOL ZERO POS |
| 98D57004033000 | 1 | REM.-INST. TOOL - FLAP BEARING |
| 98D57004034000 | 1 | REM-INST. TOOL - FLAP BEARING |
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.06ABB1) | Polysulfide Sealant-Fuel Tank Fillet - |
| (Material No.06AEA1) | Polysulfide Sealant-Low Adhesion Brushable - |
| (Material No.06AEB2) | Polysulfide Sealant-Low Adhesion Fillet Structure |
| (Material No.08BAA9) | Non Aqueous Cleaner-General - - |
| (Material No.14QFB1) | Wire-Locking Dia: 0.8 mm CRES Nickel Alloy - |
| (Material No.14SBA1) | Textile-Lint free Cotton - |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 531AB, 531BB, 532AB, 532BB, 533AB, 533BB, 631AB, 631BB, 632AB, 632BB, 633AB, 633BB |
| FIG.ITEM | DESIGNATION | IPC-CSN |
|---|---|---|
| 3 | WASHER | AIPC 57-26-15-01-030 |
| 3 | WASHER | AIPC 57-26-15-05-030 |
| 3 | WASHER | AIPC 57-26-15-10-030 |
| REFERENCE | DESIGNATION |
|---|---|
| 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 27-54-61-400-001-A | Installation of the Inboard Flap |
| TASK 27-54-61-400-003-A | Installation of the Inboard Double-Slotted Flap |
| TASK 27-54-62-000-001-A | Removal of the Outboard Flap |
| TASK 27-54-62-000-002-A | Removal of the Outboard Double-Slotted Flap |
| TASK 27-54-62-400-001-A | Installation of the Outboard Flap |
| TASK 27-54-62-400-002-A | Installation of the Outboard Double-Slotted Flap |
| TASK 57-51-33-000-002-A | Removal of the No.2 Flap Track Beam |
| TASK 57-51-33-000-003-A | Removal of the No.3 Flap Track Beam |
| TASK 57-51-33-000-004-A | Removal of the No.4 Flap Track Beam |
| TASK 57-51-33-400-002-A | Installation of the No.2 Flap Track Beam |
| TASK 57-51-33-400-003-A | Installation of the No.3 Flap Track Beam |
| TASK 57-51-33-400-004-A | Installation of the No.4 Flap Track Beam |
| TASK 57-55-11-000-001-A | Removal of the Flap Track Fairings Nos. 2, 3 and 4 |
| TASK 57-55-11-000-004-A | Removal of the Flap Track Fairings Nos. 2, 3 and 4 |
| TASK 57-55-11-400-001-A | Installation of the Flap Track Fairings Nos. 2, 3 and 4 |
| TASK 57-55-11-400-004-A | Installation of the Flap Track Fairings Nos. 2, 3 and 4 |
Subtask 57-26-15-941-051-A
A. Safety Precautions
(1) Make sure that the safety barriers are in position.
(2) Make sure that the 98D27803500001 LOCKING TOOL ZERO POS is installed on the slat/flap control lever.
(3) Make sure that the WARNING NOTICE(S) are in position to tell persons not to operate the slat/flap system.
Subtask 57-26-15-865-051-A (1) Make sure that the safety barriers are in position.
(2) Make sure that the 98D27803500001 LOCKING TOOL ZERO POS is installed on the slat/flap control lever.
(3) Make sure that the WARNING NOTICE(S) are in position to tell persons not to operate the slat/flap system.
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
Subtask 57-26-15-860-050-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 | 6CV | B07 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 | 6CV | B02 |
| ** ON A/C ALL | |||
| 121VU | FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 | 8CV | Q21 |
C. Aircraft Maintenance Configuration
(1) For the flap track beam 2:
(a) Make sure that the ACCESS PLATFORM 3M (10 FT) is below the applicable inboard flap at zone 531(631).
(b) Make sure that the applicable inboard flap is removed (Ref. AMM TASK 27-54-61-000-001).
(2) For the flap track beams 3 and 4:
(a) Make sure that the ACCESS PLATFORM 3M (10 FT) is below the applicable outboard flap at zone 533(633).
(b) Make sure that the applicable outboard flap is removed (Ref. AMM TASK 27-54-62-000-001).
(3) Make sure that the ACCESS PLATFORM 3M (10 FT) is below the applicable wing trailing edge at flap tracks 2, 3 and 4, zones 531(631), 532(632) and 533(633).
(4) Make sure that the applicable fixed fairing access panels are removed (Ref. AMM TASK 57-55-11-000-001):
Subtask 57-26-15-860-050-B ** ON A/C NOT FOR ALL (1) For the flap track beam 2:
(a) Make sure that the ACCESS PLATFORM 3M (10 FT) is below the applicable inboard flap at zone 531(631).
(b) Make sure that the applicable inboard flap is removed (Ref. AMM TASK 27-54-61-000-001).
(2) For the flap track beams 3 and 4:
(a) Make sure that the ACCESS PLATFORM 3M (10 FT) is below the applicable outboard flap at zone 533(633).
(b) Make sure that the applicable outboard flap is removed (Ref. AMM TASK 27-54-62-000-001).
(3) Make sure that the ACCESS PLATFORM 3M (10 FT) is below the applicable wing trailing edge at flap tracks 2, 3 and 4, zones 531(631), 532(632) and 533(633).
(4) Make sure that the applicable fixed fairing access panels are removed (Ref. AMM TASK 57-55-11-000-001):
- for flap track 2, 531AB 531BB 631AB 631BB
- for flap track 3, 532AB 532BB 632AB 632BB
- for flap track 4, 533AB 533BB 633AB 633BB.
- for the flap track beam 2 (Ref. AMM TASK 57-51-33-000-002)
- for the flap track beam 3 (Ref. AMM TASK 57-51-33-000-003)
- for the flap track beam 4 (Ref. AMM TASK 57-51-33-000-004).
C. Aircraft Maintenance Configuration
(1) For the flap track beam 2:
(a) Make sure that the ACCESS PLATFORM 3M (10 FT) is below the applicable inboard flap at zone 531(631).
(b) Make sure that the applicable inboard flap is removed (Ref. AMM TASK 27-54-61-000-003).
(2) For the flap track beams 3 and 4:
(a) Make sure that the ACCESS PLATFORM 3M (10 FT) is below the applicable outboard flap at zone 533(633).
(b) Make sure that the applicable outboard flap is removed (Ref. AMM TASK 27-54-62-000-002).
(3) Make sure that the ACCESS PLATFORM 3M (10 FT) is below the applicable wing trailing edge at flap tracks 2, 3 and 4, zones 531(631), 532(632) and 533(633).
(4) Make sure that the applicable fixed fairing access panels are removed (Ref. AMM TASK 57-55-11-000-004):
4. Procedure(1) For the flap track beam 2:
(a) Make sure that the ACCESS PLATFORM 3M (10 FT) is below the applicable inboard flap at zone 531(631).
(b) Make sure that the applicable inboard flap is removed (Ref. AMM TASK 27-54-61-000-003).
(2) For the flap track beams 3 and 4:
(a) Make sure that the ACCESS PLATFORM 3M (10 FT) is below the applicable outboard flap at zone 533(633).
(b) Make sure that the applicable outboard flap is removed (Ref. AMM TASK 27-54-62-000-002).
(3) Make sure that the ACCESS PLATFORM 3M (10 FT) is below the applicable wing trailing edge at flap tracks 2, 3 and 4, zones 531(631), 532(632) and 533(633).
(4) Make sure that the applicable fixed fairing access panels are removed (Ref. AMM TASK 57-55-11-000-004):
- for flap track 2, 531AB 531BB 631AB 631BB
- for flap track 3, 532AB 532BB 632AB 632BB
- for flap track 4, 533AB 533BB 633AB 633BB.
- for the flap track beam 2 (Ref. AMM TASK 57-51-33-000-002)
- for the flap track beam 3 (Ref. AMM TASK 57-51-33-000-003)
- for the flap track beam 4 (Ref. AMM TASK 57-51-33-000-004).
CAUTION:
BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:
Subtask 57-26-15-420-051-A - 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.
A. Preparation for Installation
(1) Clean the component interfaces and the adjacent areas with a Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
(2) Do an inspection of the component interfaces and the adjacent area.
(3) Make sure that the parts retained from the removed component are clean and in the correct condition.
Subtask 57-26-15-420-050-A ** ON A/C NOT FOR ALL (1) Clean the component interfaces and the adjacent areas with a Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
(2) Do an inspection of the component interfaces and the adjacent area.
(3) Make sure that the parts retained from the removed component are clean and in the correct condition.
B. Installation of the Flap Attachment-Bracket Bearing
(1) Apply Polysulfide Sealant-Low Adhesion Brushable - (Material No.06AEA1) or Polysulfide Sealant-Low Adhesion Fillet Structure (Material No.06AEB2) to the mating surfaces of the sleeve bearing (3), the spherical bearing (4) and the flap structure (2).
(2) Make sure that the Polysulfide Sealant-Low Adhesion Brushable - (Material No.06AEA1) or Polysulfide Sealant-Low Adhesion Fillet Structure (Material No.06AEB2) does not touch the internal surfaces of the spherical bearing (4).
(3) Carefully install the sleeve bearing (3) in the flap stucture (2).
(4) Make sure that the sleeve bearing (3) is fully engaged in the flap structure (2).
(5) Make sure that the Polysulfide Sealant-Low Adhesion Brushable - (Material No.06AEA1) or Polysulfide Sealant-Low Adhesion Fillet Structure (Material No.06AEB2) does not touch the threads of the outer ring (1) and the sleeve bearing (3).
(6) Install the outer ring (1) on the sleeve bearing (3), using the applicable tool as follows:
.
(8) Install the spherical bearing (4) in the sleeve bearing (3).
(9) Make sure that the Polysulfide Sealant-Low Adhesion Brushable - (Material No.06AEA1) or Polysulfide Sealant-Low Adhesion Fillet Structure (Material No.06AEB2) does not touch the internal surfaces of the spherical bearing (4).
(10) Make sure that the Polysulfide Sealant-Low Adhesion Brushable - (Material No.06AEA1) or Polysulfide Sealant-Low Adhesion Fillet Structure (Material No.06AEB2) does not touch the threads of the inner ring (5) or the sleeve bearing (3).
(11) Install the inner ring (5) in the sleeve bearing (3), using the applicable tool as follows:
.
14QFB1 Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -
(14) Apply Polysulfide Sealant-Fuel Tank Fillet - (Material No.06ABB1) to the parts that follow:
Subtask 57-26-15-410-050-A ** ON A/C NOT FOR ALL (1) Apply Polysulfide Sealant-Low Adhesion Brushable - (Material No.06AEA1) or Polysulfide Sealant-Low Adhesion Fillet Structure (Material No.06AEB2) to the mating surfaces of the sleeve bearing (3), the spherical bearing (4) and the flap structure (2).
(2) Make sure that the Polysulfide Sealant-Low Adhesion Brushable - (Material No.06AEA1) or Polysulfide Sealant-Low Adhesion Fillet Structure (Material No.06AEB2) does not touch the internal surfaces of the spherical bearing (4).
(3) Carefully install the sleeve bearing (3) in the flap stucture (2).
(4) Make sure that the sleeve bearing (3) is fully engaged in the flap structure (2).
(5) Make sure that the Polysulfide Sealant-Low Adhesion Brushable - (Material No.06AEA1) or Polysulfide Sealant-Low Adhesion Fillet Structure (Material No.06AEB2) does not touch the threads of the outer ring (1) and the sleeve bearing (3).
(6) Install the outer ring (1) on the sleeve bearing (3), using the applicable tool as follows:
- for the flap track beams 2 and 3, use the 98D57004033000 REM.-INST. TOOL - FLAP BEARING.
- for the flap track 4, use the 98D57004034000 REM-INST. TOOL - FLAP BEARING.
. (8) Install the spherical bearing (4) in the sleeve bearing (3).
(9) Make sure that the Polysulfide Sealant-Low Adhesion Brushable - (Material No.06AEA1) or Polysulfide Sealant-Low Adhesion Fillet Structure (Material No.06AEB2) does not touch the internal surfaces of the spherical bearing (4).
(10) Make sure that the Polysulfide Sealant-Low Adhesion Brushable - (Material No.06AEA1) or Polysulfide Sealant-Low Adhesion Fillet Structure (Material No.06AEB2) does not touch the threads of the inner ring (5) or the sleeve bearing (3).
(11) Install the inner ring (5) in the sleeve bearing (3), using the applicable tool as follows:
- for the flap track beams 2 and 3, use the 98D57004033000 REM.-INST. TOOL - FLAP BEARING.
- for the flap track 4, use the 98D57004034000 REM-INST. TOOL - FLAP BEARING.
. WARNING:
USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH TIME YOU CUT LOCKWIRE, REMOVE AND DISCARD IT IMMEDIATELY. LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND, AND/OR CAN CAUSE DAMAGE.
(13) Safety the outer ring (1) and the inner ring (5) together with (14) Apply Polysulfide Sealant-Fuel Tank Fillet - (Material No.06ABB1) to the parts that follow:
- the interface of the outer ring (1) and the flap structure (2)
- the interface of the sleeve bearing (3) and the flap structure (2).
C. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the applicable flap track beam:
(a) Install the applicable inboard flap (Ref. AMM TASK 27-54-61-400-001).
(5) For the flap track beams 3 and 4:
(a) Install the applicable outboard flap (Ref. AMM TASK 27-54-62-400-001).
Subtask 57-26-15-420-050-B ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the applicable flap track beam:
- for the flap track beam 2 (Ref. AMM TASK 57-51-33-400-002)
- for the flap track beam 3 (Ref. AMM TASK 57-51-33-400-003)
- for the flap track beam 4 (Ref. AMM TASK 57-51-33-400-004).
- for flap track 2, install 531AB 531BB 631AB 631BB
- for flap track 3, install 532AB 532BB 632AB 632BB
- for flap track 4, install 533AB 533BB 633AB 633BB.
(a) Install the applicable inboard flap (Ref. AMM TASK 27-54-61-400-001).
(5) For the flap track beams 3 and 4:
(a) Install the applicable outboard flap (Ref. AMM TASK 27-54-62-400-001).
D. Installation of the Flap Attachment-Bracket Bearing
(1) For the flap track 2:
(a) Apply Polysulfide Sealant-Low Adhesion Brushable - (Material No.06AEA1) or Polysulfide Sealant-Low Adhesion Fillet Structure (Material No.06AEB2) to the mating surfaces of the bearing assembly (1), the nut (4) and the flap structure (2).
(2) For the flap track 3:
(a) Apply Polysulfide Sealant-Low Adhesion Brushable - (Material No.06AEA1) or Polysulfide Sealant-Low Adhesion Fillet Structure (Material No.06AEB2) to the mating surfaces of the bearing assembly (1), the nut (4) and the flap structure (2).
(3) For the flap track 4:
(a) Apply Polysulfide Sealant-Low Adhesion Brushable - (Material No.06AEA1) or Polysulfide Sealant-Low Adhesion Fillet Structure (Material No.06AEB2) to the mating surfaces of the bearing assembly (1), the nut (4) and the flap structure (2).
(4) Make sure that the Polysulfide Sealant-Low Adhesion Brushable - (Material No.06AEA1) or Polysulfide Sealant-Low Adhesion Fillet Structure (Material No.06AEB2) does not touch the internal surfaces of the bearing assembly (1).
(5) Carefully install the bearing assembly (1) in the flap structure (2).
(6) Make sure that the bearing assembly (1) is fully engaged in the flap structure (2).
(7) Make sure that the Polysulfide Sealant-Low Adhesion Brushable - (Material No.06AEA1) or Polysulfide Sealant-Low Adhesion Fillet Structure (Material No.06AEB2) does not touch the internal surfaces of the bearing assembly (1).
(8) Make sure that the Polysulfide Sealant-Low Adhesion Brushable - (Material No.06AEA1) or Polysulfide Sealant-Low Adhesion Fillet Structure (Material No.06AEB2) does not touch the threads of the nut (4) or the bearing assembly (1).
(9) For the flap track 2:
(a) Install the new AIPC 57-26-15-01-030 WASHER (3).
(10) For the flap track 3:
(a) Install the new AIPC 57-26-15-05-030 WASHER (3).
(11) For the flap track 4:
(a) Install the new AIPC 57-26-15-10-030 WASHER (3).
(12) Install the nut (4), using the applicable tool as follows:
(15) TORQUE the applicable nut (4) again, as specified in workstep (12).
(16) Safety the nut (4) with the washer (3).
(17) Apply Polysulfide Sealant-Fuel Tank Fillet - (Material No.06ABB1) to the parts that follow:
Subtask 57-26-15-410-050-B ** ON A/C NOT FOR ALL (1) For the flap track 2:
(a) Apply Polysulfide Sealant-Low Adhesion Brushable - (Material No.06AEA1) or Polysulfide Sealant-Low Adhesion Fillet Structure (Material No.06AEB2) to the mating surfaces of the bearing assembly (1), the nut (4) and the flap structure (2).
(2) For the flap track 3:
(a) Apply Polysulfide Sealant-Low Adhesion Brushable - (Material No.06AEA1) or Polysulfide Sealant-Low Adhesion Fillet Structure (Material No.06AEB2) to the mating surfaces of the bearing assembly (1), the nut (4) and the flap structure (2).
(3) For the flap track 4:
(a) Apply Polysulfide Sealant-Low Adhesion Brushable - (Material No.06AEA1) or Polysulfide Sealant-Low Adhesion Fillet Structure (Material No.06AEB2) to the mating surfaces of the bearing assembly (1), the nut (4) and the flap structure (2).
(4) Make sure that the Polysulfide Sealant-Low Adhesion Brushable - (Material No.06AEA1) or Polysulfide Sealant-Low Adhesion Fillet Structure (Material No.06AEB2) does not touch the internal surfaces of the bearing assembly (1).
(5) Carefully install the bearing assembly (1) in the flap structure (2).
(6) Make sure that the bearing assembly (1) is fully engaged in the flap structure (2).
(7) Make sure that the Polysulfide Sealant-Low Adhesion Brushable - (Material No.06AEA1) or Polysulfide Sealant-Low Adhesion Fillet Structure (Material No.06AEB2) does not touch the internal surfaces of the bearing assembly (1).
(8) Make sure that the Polysulfide Sealant-Low Adhesion Brushable - (Material No.06AEA1) or Polysulfide Sealant-Low Adhesion Fillet Structure (Material No.06AEB2) does not touch the threads of the nut (4) or the bearing assembly (1).
(9) For the flap track 2:
(a) Install the new AIPC 57-26-15-01-030 WASHER (3).
(10) For the flap track 3:
(a) Install the new AIPC 57-26-15-05-030 WASHER (3).
(11) For the flap track 4:
(a) Install the new AIPC 57-26-15-10-030 WASHER (3).
(12) Install the nut (4), using the applicable tool as follows:
- for the flap track beams 2 and 3, use the 98D57004033000 REM.-INST. TOOL - FLAP BEARING
- for the flap track beam 4, use the 98D57004034000 REM-INST. TOOL - FLAP BEARING.
- for the flap track 2, to between 10.5 and 9.5 m.daN (77.43 and 70.06 lbf.ft )
- for the flap track 3, to between 10.5 and 9.5 m.daN (77.43 and 70.06 lbf.ft )
- for the flap track 4, to between 6.5 and 5.5 m.daN (47.94 and 40.56 lbf.ft ) .
(15) TORQUE the applicable nut (4) again, as specified in workstep (12).
(16) Safety the nut (4) with the washer (3).
(17) Apply Polysulfide Sealant-Fuel Tank Fillet - (Material No.06ABB1) to the parts that follow:
- the interface of the nut (4) and the flap structure (2)
- the interface of the bearing assembly (1) and the flap structure (2).
E. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the applicable flap track beam:
(a) Install the applicable inboard flap (Ref. AMM TASK 27-54-61-400-003).
(5) For the flap track beams 3 and 4:
(a) Install the applicable outboard flap (Ref. AMM TASK 27-54-62-400-002).
Subtask 57-26-15-865-052-A (1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the applicable flap track beam:
- for the flap track beam 2 (Ref. AMM TASK 57-51-33-400-002)
- for the flap track beam 3 (Ref. AMM TASK 57-51-33-400-003)
- for the flap track beam 4 (Ref. AMM TASK 57-51-33-400-004).
- for flap track 2, install 531AB 531BB 631AB 631BB
- for flap track 3, install 532AB 532BB 632AB 632BB
- for flap track 4, install 533AB 533BB 633AB 633BB.
(a) Install the applicable inboard flap (Ref. AMM TASK 27-54-61-400-003).
(5) For the flap track beams 3 and 4:
(a) Install the applicable outboard flap (Ref. AMM TASK 27-54-62-400-002).
F. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
5. Close-up| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 | 6CV | B07 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 | 6CV | B02 |
| ** ON A/C ALL | |||
| 121VU | FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 | 8CV | Q21 |
Subtask 57-26-15-942-050-A
A. Removal of Equipment
(1) Remove the 98D27803500001 LOCKING TOOL ZERO POS from the slat/flap control lever.
(2) Remove the safety barriers.
(3) Remove the WARNING NOTICE(S).
(4) Remove the access platform(s).
(5) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(1) Remove the 98D27803500001 LOCKING TOOL ZERO POS from the slat/flap control lever.
(2) Remove the safety barriers.
(3) Remove the WARNING NOTICE(S).
(4) Remove the access platform(s).
(5) Remove the ground support and maintenance equipment, the special and standard tools and all other items.