Removal of the NLG Electrical Harness 2M

TASK 32-21-43-000-003-A
Removal of the NLG Electrical Harness 2M

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: 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.

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 2M (6 FT) - ADJUSTABLE
No specific	AR	CAP - BLANKING
No specific	AR	SAFETY CLIP - CIRCUIT BREAKER
No specific	AR	WARNING NOTICE(S)

B. Referenced Information

REFERENCE	DESIGNATION
TASK 24-41-00-862-002-A	De-energize the Aircraft Electrical Circuits Supplied from the External Power
TASK 24-41-00-862-002-A-01	De-energize the Aircraft Electrical Circuits Supplied from the APU
TASK 24-41-00-862-002-A-02	De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2)
TASK 32-00-00-481-001-A	Installation of the Safety Devices on the Landing Gears
TASK 32-00-00-481-002-A	Installation of the Safety Devices on the Landing Gear Doors
TASK 32-00-00-860-001-A	Flight Configuration Precautions with Electrical Power
TASK 32-00-00-860-001-A-01	Flight Configuration Precautions without Electrical Power
TASK 32-22-00-010-001-A	Nose Gear Doors - Ground Doors Opening
NLG - Electrical Harness 2M
Nose Wheel Steering - Servo-Control

3. Job Set-up
Subtask 32-21-43-941-056-A

A. Safety Precautions
(1) Make sure that the safety device are installed on the landing gears (Ref. AMM TASK 32-00-00-481-001).
(2) Put the WARNING NOTICE(S) in position:

on the panel 400VU, to tell persons not to operate the landing gear control lever,
on the NWS hand/wheels and the rudder pedals to tell persons not to operate them.

Subtask 32-21-43-010-056-A

B. Get Access
(1) Open the NLG doors (Ref. AMM TASK 32-22-00-010-001).
(2) Make sure that the safety devices are correctly installed on the landing gear doors (Ref. AMM TASK 32-00-00-481-002).
(3) Put the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position adjacent to the NLG.

Subtask 32-21-43-869-059-A

C. Flight Configuration Precautions
(1) If the electrical power is not necessary for other maintenance tasks, make sure that the aircraft electrical circuits are de-energized (Ref. AMM TASK 24-41-00-862-002). Then, it is not necessary to operate the circuit breakers below.

Subtask 32-21-43-865-059-A

D. Open, safety and tag this(these) circuit breaker(s):

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C ALL
49VU	L/G/LGCIU/SYS1/NORM	1GA	C09
121VU	HYDRAULIC/BRAKING AND STEERING/SYS2/SPLY	4GG	M36
121VU	HYDRAULIC/BRAKING AND STEERING/SYS2/CTL	3GG	M35
121VU	HYDRAULIC/BRAKING AND STEERING/SYS1/CTL	1GG	M34
121VU	HYDRAULIC/BRAKING AND STEERING/SYS1/IND AND/SPLY	2GG	M33
121VU	HYDRAULIC/LGCIU/SYS2	2GA	Q35
121VU	HYDRAULIC/LGCIU/SYS1/GRND SPLY	52GA	Q34
122VU	LIGHTING/EXT LT/TAXI AND TAKE OFF/TAXI	1LR	W08
122VU	LIGHTING/EXT LT/RWY TURN OFF/R	1LC2	W05

Subtask 32-21-43-869-064-A

E. Flight Configuration Precautions
(1) If the electrical power is necessary for other maintenance tasks, do the precautions for flight configuration (Ref. AMM TASK 32-00-00-860-001) after you have opened the circuit breakers.

4. Procedure
Subtask 32-21-43-020-053-D

A. Removal of the Upper Harness 2M

WARNING: FOR SAFETY STAND AFT OF THE GEAR LEG WHEN YOU OPERATE THE GROUND OPENING CONTROL OF THE DOOR. CAREFULLY READ THE PLACARD ON THE LEG DOOR BEFORE YOU OPEN THE NOSE GEAR DOORS.

(1) Put a CAP - BLANKING on the electrical connectors as you disconnect them.
(2) Disconnect the electrical connector 25GAA (18) from the NLG proximity sensor 25GA (19).
(3) Remove the screw (17), washer (16) and clamp (15) from the bracket (20).
(4) Cut, remove and discard the braid (14) from the grommet (13).
(5) Disconnect the electrical connector 5GCA (11) from the electrical box 5GC (12).
(6) Disconnect the electrical connector 3LC2A (8) from the right runway-turnoff-light 3LC2 (9).
(7) Remove the screw (1), washer (2) and clamp (3) from the bracket (5).
(8) Remove the screw (7), washer (6) and clamp (4) from the bracket (5).
(9) Cut, remove and discard the braid (25) from the grommet (26).
(10) Remove the screw (23), washer (22) and clamp (21) from the bracket (24).
(11) Disconnect the electrical connector 4GCA (28) from the nose-wheel steering feed-back sensor 4GC (27).
(12) Fold back the heat-shrink sleeve (58) until you can disconnect the electrical connector 6GCA (56).
(13) Disconnect the electrical connector 6GCA (56) from the nose-wheel steering servo-control 6GC (57).
(14) Remove the screw (41), washer (42) and clamp (43) from the bracket (45).
(15) Remove the screw (47), washer (46) and clamp (48) from the bracket (45).
(16) Disconnect the electrical connector 19GAA (39) from the proximity sensor 19GA installed on the bracket (40).
(17) Remove the screw (36), washer (35) and clamp (34) from the bracket (37).
(18) Remove the screw (32), washer (31), clamp (33) and spacer (38) from the bracket (37).
(19) Disconnect the electrical connector 8LRA (30) from the taxi light 8LR (29).
(20) Remove the nuts (50), washers (51), screws (54) and washers (53) to release the clamp (52) from the bracket (49).
(21) Disconnect the electrical connector 1302VCA (55) from the receptacle 1302VC of the housing installed on the aircraft structure.
(22) Remove the upper harness 2M (44).

[Rev.10 from 2021] 2026.04.01 00:42:44 UTC