Removal of the Non-TPIS Kit

TASK 32-49-51-000-802-A
Removal of the Non-TPIS Kit

WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.

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.

WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.

FIN: 2878GM

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	AIR SOURCE FILTERED, DRY
No specific	1	CAP - BLANKING
No specific	1	SAFETY BARRIER(S)
No specific	1	SPATULA - NON METALLIC
No specific	AR	WARNING NOTICE(S)

B. Consumable Materials

REFERENCE	DESIGNATION
(Material No.06ABA1)	Polysulfide Sealant-Fuel Tank Brushable -
(Material No.06LDG2)	Non Hardening Jointing Putty-High Temp. Area - Structure
(Material No.08BBF1)	Non Aqueous Cleaner_- Methyl-Ethyl-Ketone -

C. Expendable Parts

FIG.ITEM	DESIGNATION	IPC-CSN
12	LOCKWASHER	AIPC 32-21-11-11-080
29	COTTER PIN	AIPC 32-21-11-12-080
16	NUT	AIPC 32-21-11-23-010
16	NUT	AIPC 32-21-11-43-010
12	LOCKWASHER	AIPC 32-21-11-51-470
29	COTTER PIN	AIPC 32-21-11-52-080
12	LOCKWASHER	AIPC 32-21-11-91-470

D. Referenced Information

REFERENCE	DESIGNATION
TASK 07-11-00-581-003-A	Lifting of the Aircraft at the Forward Jacking Point, MLG Wheels on the Ground
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 32-41-12-000-001-A	Removal of the NLG Wheel
Non-TPIS Kit
Non-TPIS Kit

3. Job Set-up
Subtask 32-49-51-941-051-A

A. Safety Precautions
(1) Put the WARNING NOTICE(S) in position:

In the cockpit, on the right center instrument panel 400VU, to tell persons not to operate the landing gear control lever.
On the steering handwheel (CAPT and F/O) and on the brake pedals, to tell persons not to operate them .

(2) Install the safety devices on the landing gears (Ref. AMM TASK 32-00-00-481-001).
(3) Put the SAFETY BARRIER(S) in position.

Subtask 32-49-51-860-053-A

B. Aircraft Maintenance Configuration
(1) De-energized the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
(2) On the parking brake panel 110VU, make sure that the PARK BRK control switch is in the OFF position.
(3) Make sure that the wheel chocks are in position.
(4) Lift the aircraft at the forward jacking point (Ref. AMM TASK 07-11-00-581-003).
(5) Remove the NLG wheels (Ref. AMM TASK 32-41-12-000-001).

4. Procedure
Subtask 32-49-51-020-051-A

A. Removal of the Non-TPIS Kit
(1) Remove the plug (3) of the 701VC connector of the 1M upper electrical harness:
(a) Remove the nut (1) and the bolt (2) that attach the tab of the plug (3).
(b) Remove the plug (3).
(c) Install the bolt (2) and the nut (1).
(d) Tighten the nut (1).
(e) Install a CAP - BLANKING on the electrical connector.
(2) Disconnect the rod (28).
(a) Remove and discard the cotter pin (29).
(b) Remove the nut (30), the washer (31) and the bolt (33).
(c) Disconnect the rod (28) from the support (32).
(3) Remove the bolt (10):
(a) For single-linkage version:
1 Remove and discard the nut (6).
2 Remove the washer (7) and the spacer (5).
3 Hold the casing (9) in position and remove the bolt (10) and the lockwasher (4).
4 Remove the second spacer (5).
(b) For dual-linkage version:
1 Remove and discard the nut (6).
2 Remove the washer (7), the spacer (5) and the spacer (8).
3 Hold the casing (9) in position and remove the bolt (10) and the lockwasher (4).
4 Remove the second spacer (5) and the second spacer (8).
(4) Remove the casing (9).
(a) Release and remove the screw (11).
(b) Remove and discard the lockwasher (12).
(c) Lift the casing (9) and disengage it from the pin (13).
(d) Remove the casing (9).
(5) Remove the blanking plug (15) from the torque link pin (14) of the leg structure:
(a) Remove and discard the nut (16).
(b) Remove the washer (17) from the pin (13).
(c) Remove the pin (13).
(d) Remove the blanking cap (15) from the torque link pin (14).

NOTE: The torque link pin (14) must stay in position during the removal of the blanking cap (15).

(e) Clean the pin (13) with Non Aqueous Cleaner_- Methyl-Ethyl-Ketone - (Material No.08BBF1) and dry it with AIR SOURCE FILTERED, DRY.
(f) Apply a thin layer of Non Hardening Jointing Putty-High Temp. Area - Structure (Material No.06LDG2) on the pin (13).
(g) Align the holes with the tool J47125 and engage the pin (13).
(h) Install the washer (17) and the new AIPC 32-21-11-43-010 NUT (16) or AIPC 32-21-11-23-010 NUT (16).
(i) Tighten the nut (16).
(j) Apply a bead of Polysulfide Sealant-Fuel Tank Brushable - (Material No.06ABA1) on the interface between the pin (13) and the gear leg.
(k) Put the casing (9) in position on the pin (13).
(l) Install the screw (11) and the new AIPC 32-21-11-51-470 LOCKWASHER (12) or AIPC 32-21-11-11-080 LOCKWASHER (12) or AIPC 32-21-11-91-470 LOCKWASHER (12) or AIPC 32-21-11-11-080 LOCKWASHER (12).
(m) Tighten the screw (11) and safety it with the lockwasher (12).
(n) Apply a bead of Polysulfide Sealant-Fuel Tank Brushable - (Material No.06ABA1) around the nut (16).
(6) Connect the rod (28).
(a) Connect the rod (28) to the support (32).
(b) Install the bolt (33), the washer (31) and the nut (30).
(c) Tighten the nut (30) and safety it with the new AIPC 32-21-11-52-080 COTTER PIN (29) or AIPC 32-21-11-12-080 COTTER PIN (29).
(7) Remove the bushes (27) from the wheel axle ends.
(a) Remove and discard the four cotter pins (23).
(b) Remove the four nuts (24) and the four washers (25).
(c) Remove and discard the four bolts (26).
(d) Remove the bushes (27).
(8) Remove the plug (22) from the TPIS harness installation-hole in the shock absorber:
(a) Remove the sealant between the sliding rod and the plug (22) with a SPATULA - NON METALLIC.
(b) Remove the cotter pin (19) and the nut (20).
(c) Discard the cotter pin (19).
(d) Remove the washer (21).
(e) Remove the bolt (18), the second washer (21) and the plug (22).

[Rev.10 from 2021] 2026.04.01 00:50:39 UTC