Removal of the Wing-Tip Structure
TASK 57-31-21-000-001-A
Removal of the Wing-Tip Structure
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Referenced Information
3. Job Set-up
Subtask 57-31-21-941-052-A ** ON A/C NOT FOR ALL
Subtask 57-31-21-020-051-C ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 02:12:18 UTC
Removal of the Wing-Tip Structure
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.
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 JobSelf explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | ACCESS PLATFORM 4M (13 FT) |
| No specific | AR | CAP - BLANKING |
| No specific | AR | SAFETY BARRIER(S) |
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| No specific | AR | TRESTLE - PADDED |
| No specific | AR | WARNING NOTICE(S) |
| 98D27803500001 | 1 | LOCKING TOOL ZERO POS |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 33-41-11-000-001-A | Removal of the Wingtip Navigation Light |
| TASK 33-48-14-000-001-A | Removal of the Strobe Light |
| TASK 33-48-38-000-001-A | Removal of the Power Supply Unit |
| TASK 57-31-22-000-001-A | Removal of the Wing-Tip Fence |
Subtask 57-31-21-941-052-A ** ON A/C NOT FOR ALL
A. Safety Precautions
(1) Install the 98D27803500001 LOCKING TOOL ZERO POS on the flap/slat control lever.
(2) Put WARNING NOTICE(S) in the cockpit to tell persons not to operate the flaps or slats.
(3) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
(4) Put the ACCESS PLATFORM 4M (13 FT) in position below the applicable wing-tip, zone 534 (634).
(5) Remove the applicable access panel:
Subtask 57-31-21-865-050-A ** ON A/C NOT FOR ALL (1) Install the 98D27803500001 LOCKING TOOL ZERO POS on the flap/slat control lever.
(2) Put WARNING NOTICE(S) in the cockpit to tell persons not to operate the flaps or slats.
(3) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
(4) Put the ACCESS PLATFORM 4M (13 FT) in position below the applicable wing-tip, zone 534 (634).
(5) Remove the applicable access panel:
- for the left wing-tip remove 534AB
- for the right wing-tip remove 634AB.
B. Open, safety and tag this(these) circuit breaker(s):
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 122VU | LIGHTING/EXT LT/NAV1/AND LOGO/LT | 1LA | T03 |
| ** ON A/C NOT FOR ALL | |||
| 122VU | LIGHTING/EXT LT/NAV2/AND LOGO/LT | 2LA | T02 |
| 122VU | LIGHTING/WING/STROBE | 10LV | V05 |
| ** ON A/C NOT FOR ALL | |||
| 122VU | LIGHT/EXT LT NAV1/AND LOGO/LT | 1LA | T03 |
Subtask 57-31-21-020-051-C ** ON A/C NOT FOR ALL
A. Preparation of the Wing-Tip Structure if it is to be Replaced
(1) If the wing-tip structure is to be replaced, remove:
Subtask 57-31-21-020-050-B ** ON A/C NOT FOR ALL (1) If the wing-tip structure is to be replaced, remove:
- the navigation light assembly (Ref. AMM TASK 33-41-11-000-001)
- the strobe light assembly (Ref. AMM TASK 33-48-14-000-001)
- the power supply unit (Ref. AMM TASK 33-48-38-000-001)
- the wing-tip fence (Ref. AMM TASK 57-31-22-000-001).
B. Removal of the Wing-tip Structure
(1) Disconnect the supply cable from the connector (4).
(2) Put the CAP-BLANKING on each disconnected electrical connector and receptacle.
(3) Remove the grommet (3) from the adjacent structure.
(4) Push the supply cable through the hole where the grommet (3) was installed.
(5) Hold the wing tip (2) (weight approximately 20 kg (44 lb)) on supports and remove the bolts (5).
(6) Remove the wing tip (2) laterally from the two spigots (1) and put it on a suitable TRESTLE - PADDED.
(7) Prevent damage to the component interfaces and the adjacent area.
(1) Disconnect the supply cable from the connector (4).
(2) Put the CAP-BLANKING on each disconnected electrical connector and receptacle.
(3) Remove the grommet (3) from the adjacent structure.
(4) Push the supply cable through the hole where the grommet (3) was installed.
(5) Hold the wing tip (2) (weight approximately 20 kg (44 lb)) on supports and remove the bolts (5).
(6) Remove the wing tip (2) laterally from the two spigots (1) and put it on a suitable TRESTLE - PADDED.
(7) Prevent damage to the component interfaces and the adjacent area.
Wing Tip Structure