Removal of the Wing and Engine Scan Light
TASK 33-49-11-000-001-A
Removal of the Wing and Engine Scan Light
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Work Zones and Access Panels
C. Referenced Information
3. Job Set-up
Subtask 33-49-11-865-050-A
Subtask 33-49-11-020-050-A
[Rev.10 from 2021]
2026.04.01 04:02:20 UTC
Removal of the Wing and Engine Scan Light
WARNING:
WEAR GLASSES AND PROTECTIVE CLOTHING WHEN YOU DO WORK ON THE LIGHT. THE LAMP IS PRESSURIZED AND AN EXPLOSION CAN OCCUR.
WARNING:
DO NOT DISCONNECT THE ELECTRICAL CONNECTIONS FOR AT LEAST 2 MINUTES AFTER YOU DE-ENERGIZE THE ELECTRICAL CIRCUITS.
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)-ADJUSTABLE |
| No specific | AR | CAP - BLANKING |
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 231 | FWD PASSENGER COMPARTMENT |
| 232 | FWD PASSENGER COMPARTMENT |
| FOR [3LX] (LT-WING & ENG SCAN, L) | |
| 231KW | |
| FOR [4LX] (LT-WING & ENG SCAN, R) | |
| 232KW | |
| REFERENCE | DESIGNATION |
|---|---|
Subtask 33-49-11-865-050-A
A. Open, safety and tag this(these) circuit breaker(s):
Subtask 33-49-11-010-051-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C ALL | |||
| FOR FIN: 4LX (LTWING & ENG SCAN, R) | |||
| 122VU | LIGHTING/EXT LT/WING/AND ENG SCAN/R | 1LX | W03 |
| FOR FIN: 3LX (LTWING & ENG SCAN, L) | |||
| 122VU | LIGHTING/EXT LT/WING/AND ENG SCAN/L | 5LX | W02 |
B. Get Access
(1) Put the ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE in position in zone 230.
(2) Remove the sidewall panel in the forward passenger compartment:
(a) FOR [3LX] (LT-WING & ENG SCAN, L)
231KW
(b) FOR [4LX] (LT-WING & ENG SCAN, R)
232KW
(3) Remove the thermal and acoustic insulation in zones 231 and 232.
4. Procedure(1) Put the ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE in position in zone 230.
(2) Remove the sidewall panel in the forward passenger compartment:
(a) FOR [3LX] (LT-WING & ENG SCAN, L)
231KW
(b) FOR [4LX] (LT-WING & ENG SCAN, R)
232KW
(3) Remove the thermal and acoustic insulation in zones 231 and 232.
Subtask 33-49-11-020-050-A
A. Removal of the Wing and Engine Scan Light
(1) Outside the aircraft:
(a) Loosen the 16 screws (2) which attach the wing and engine scan light (1) to the structure (3) of the aircraft.
(2) Inside the forward passenger compartment:
(a) Disconnect the movable connector (4) from the light (1) and put a CAP - BLANKING on the disconnected connector.
(3) Remove the wing and engine scan light (1).
(1) Outside the aircraft:
(a) Loosen the 16 screws (2) which attach the wing and engine scan light (1) to the structure (3) of the aircraft.
(2) Inside the forward passenger compartment:
(a) Disconnect the movable connector (4) from the light (1) and put a CAP - BLANKING on the disconnected connector.
(3) Remove the wing and engine scan light (1).
NOTE: It could be possible that the wing and engine scan lights are not easy to remove. Do not use tools which could damage the aircraft structure.
Wing and Engine Scan Light