Anti Skid Indication on ECAM WHEEL Page

TASK 32-60-00-040-001-A
Anti Skid Indication on ECAM WHEEL Page

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: 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.

1. Reason for the Job

NOTE: This deactivation task is not related to an AFM-CDL/MMEL item

2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment

REFERENCE	QTY	DESIGNATION
No specific	AR	SAFETY BARRIER(S)
No specific	AR	WARNING NOTICE(S)

B. Referenced Information

REFERENCE	DESIGNATION
TASK 24-41-00-861-002-A	Energize the Aircraft Electrical Circuits from the External Power
TASK 24-41-00-861-002-A-01	Energize the Aircraft Electrical Circuits from the APU
TASK 24-41-00-861-002-A-02	Energize the Aircraft Electrical Circuits from Engine 1(2)
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 29-10-00-863-001-A	Pressurize the Green Hydraulic System with a Hydraulic Ground Power-Cart
TASK 29-10-00-864-001-A	Depressurize the Green Hydraulic System
TASK 31-32-00-860-009-A	Procedure to Get Access to the SYSTEM REPORT/TEST/L/G Page
TASK 31-60-00-860-001-A	EIS Start Procedure
TASK 31-60-00-860-002-A	EIS Stop Procedure
TASK 32-00-00-481-001-A	Installation of the Safety Devices on the Landing Gears

3. Job Set-up
Subtask 32-60-00-941-051-A

A. Safety Precautions
(1) Put the SAFETY BARRIER(S) in position.
(2) Make sure that the ground safety locks are on the landing gear (Ref. AMM TASK 32-00-00-481-001).
(3) On the panel 400VU, make sure that the landing-gear control-lever 6GA is in the DOWN position.
(4) Put a WARNING NOTICE(S) in position to tell persons not to operate the landing gear.

Subtask 32-60-00-860-053-A

B. Aircraft Maintenance Configuration
(1) Pressurize the Green Hydraulic System (Ref. AMM TASK 29-10-00-863-001).
(2) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(3) On the panel 402VU, make sure that the A/SKID & NOSE WHEEL switch is set to ON.
(4) Do the EIS start procedure (ECAM only) (Ref. AMM TASK 31-60-00-860-001).
(5) On the center pedestal, on the MCDU, get the SYSTEM REPORT/TEST/L/G page (Ref. AMM TASK 31-32-00-860-009).

Subtask 32-60-00-865-052-A

C. Make sure that this(these) circuit breaker(s) is(are) closed:

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C ALL
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

4. Procedure
Subtask 32-60-00-720-051-B

A. Test of the Anti Skid Indication on the ECAM Wheel Page
(1) Do this test:

ACTION	RESULT
1.On the MCDU, push the line key adjacent to the BSCU A indication.	the BSCU SYS1 page is shown.
2.Push the line key adjacent to the TEST indication.	the BSCU SYS1/TEST page is shown and gives instructions.
3.Obey the instructions shown on the display. Wait 5 seconds, then push the line key adjacent to the TEST indication.	The test starts and continues for 45 seconds. If the test finds no faults, the NO FAILURE indication is shown. If the test results are incorrect, a list of fault messages are shown.
4.Push the line key adjacent to the RETURN indication to get the SYSTEM REPORT/TEST/L/G page.	the SYSTEM REPORT/TEST/L/G page is shown.
5.Push the line key adjacent to the BSCU B indication.	the BSCU SYS2 page is shown.
6.Do the same actions as in step 2. and 3.	get the same results as for the BSCU SYS1.

5. Close-up
Subtask 32-60-00-860-054-A

A. Aircraft Maintenance Configuration
(1) On the MCDU, push the line key adjacent to the RETURN indication until the CFDS menu page is shown.
(2) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
(3) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
(4) On the panel 402VU, make sure that the A/SKID & NOSE WHEEL switch is set to ON.
(5) Depressurize the Green Hydraulic System (Ref. AMM TASK 29-10-00-864-001).

Subtask 32-60-00-942-051-A

B. Removal of Equipment
(1) Remove the SAFETY BARRIER(S).
(2) Remove the WARNING NOTICE(S).
(3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.

[Rev.10 from 2021] 2026.04.01 00:52:02 UTC