Functional Test of the Nose Wheel Steering with the CFDS
TASK 32-51-00-720-007-A
Functional Test of the Nose Wheel Steering with the CFDS
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Referenced Information
3. Job Set-up
Subtask 32-51-00-860-087-A ** ON A/C NOT FOR ALL
Subtask 32-51-00-720-061-B ** ON A/C NOT FOR ALL
Subtask 32-51-00-860-086-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 00:51:11 UTC
Functional Test of the Nose Wheel Steering with the CFDS
WARNING:
MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT. UNWANTED ELECTRICAL POWER CAN BE DANGEROUS.
WARNING:
MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS SURFACES ARE CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT.
WARNING:
MAKE SURE THAT THE CONTROLS AGREE WITH THE POSITION OF THE ITEMS THEY OPERATE BEFORE YOU PRESSURIZE A HYDRAULIC SYSTEM. UNWANTED MOVEMENT OF HYDRAULICALLY OPERATED ITEMS CAN CAUSE SERIOUS INJURY AND/OR DAMAGE.
CAUTION:
BEFORE YOU START THE NOSE WHEEL STEERING TEST, MAKE SURE THAT NO BOARDING BRIDGES ARE CONNECTED TO THE PASSENGER/CREW DOORS. IF A BOARDING BRIDGE IS CONNECTED, DAMAGE CAN OCCUR TO THE AIRCRAFT.
1. Reason for the JobSelf explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | WARNING NOTICE(S) |
| 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 29-10-00-863-003-A | Pressurize the Blue Hydraulic System with a Hydraulic Ground Power-Cart |
| TASK 29-10-00-863-003-A-01 | Pressurize the Blue Hydraulic System with the Blue Electric Pump |
| TASK 29-10-00-864-003-A | Depressurize the Blue Hydraulic System |
| TASK 31-32-00-860-009-A | Procedure to Get Access to the SYSTEM REPORT/TEST/L/G Page |
| TASK 32-51-11-000-001-A | Removal of the Transmitter Unit - Nose-Wheel Steering Handwheel |
| TASK 32-51-11-400-001-A | Installation of the Transmitter Unit - Nose-Wheel Steering Handwheel |
Subtask 32-51-00-860-087-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(2) Pressurize the Blue hydraulic system (Ref. AMM TASK 29-10-00-863-003).
(3) On the MCDU, get the SYSTEM REPORT/TEST L/G page (Ref. AMM TASK 31-32-00-860-009).
(4) On the panel 402VU, make sure that the A/SKID switch is at ON.
Subtask 32-51-00-941-064-A ** ON A/C NOT FOR ALL (1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(2) Pressurize the Blue hydraulic system (Ref. AMM TASK 29-10-00-863-003).
(3) On the MCDU, get the SYSTEM REPORT/TEST L/G page (Ref. AMM TASK 31-32-00-860-009).
(4) On the panel 402VU, make sure that the A/SKID switch is at ON.
B. Safety Precautions
(1) Put the WARNING NOTICE(S) in position to tell persons:
Subtask 32-51-00-860-087-B ** ON A/C NOT FOR ALL (1) Put the WARNING NOTICE(S) in position to tell persons:
- not to operate the A/SKID switch,
- not to pressurize the Green and the Yellow hydraulic systems.
C. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(2) On the MCDU, get the SYSTEM REPORT/TEST L/G page (Ref. AMM TASK 31-32-00-860-009).
(3) On the panel 402VU, make sure that the A/SKID switch is at ON.
Subtask 32-51-00-941-064-B ** ON A/C NOT FOR ALL (1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(2) On the MCDU, get the SYSTEM REPORT/TEST L/G page (Ref. AMM TASK 31-32-00-860-009).
(3) On the panel 402VU, make sure that the A/SKID switch is at ON.
D. Safety Precautions
(1) Put the WARNING NOTICE(S) in position to tell persons:
Subtask 32-51-00-865-117-A (1) Put the WARNING NOTICE(S) in position to tell persons:
- not to operate the A/SKID switch,
- not to pressurize the Green, the Blue and the Yellow hydraulic systems.
E. Table of the circuit breakers used in this procedure:
4. Procedure| 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 |
Subtask 32-51-00-720-061-B ** ON A/C NOT FOR ALL
A. Test
Subtask 32-51-00-720-061-C ** ON A/C NOT FOR ALL | ACTION | RESULT |
|---|---|
| 1.Open the circuit breakers 1GG, 2GG, 3GG and 4GG. Then close the circuit breakers 1GG and 2GG first, then 3GG and 4GG to make sure that you put the BSCU CHAN 1 in the active mode. | |
| 2.On the MCDU, push the line key adjacent to the BSCU 1 indication. |
|
| 3.Push the line key adjacent to the SPECIFIC DATA indication. |
|
| 4.Push the line key adjacent to the STEERING DATA indication. |
|
| 5.Turn the CAPT handwheel fully counterclockwise and hold it in position. On the MCDU, push the line key adjacent to the REFRESH indication. |
|
| 6.Release the CAPT handwheel to the neutral position. | |
| 7.Turn the CAPT handwheel fully clockwise and hold it in position. On the MCDU, push the line key adjacent to the REFRESH indication. |
|
| 8.Release the CAPT handwheel to the neutral position. | |
| 9.Set and hold a rudder angle with the rudder pedals. On the MCDU, push the line key adjacent to the REFRESH indication. |
|
| 10.Push the line key adjacent to the RETURN indication to get the SPECIFIC DATA indication |
|
| 11.Push the line key adjacent to the SYSTEM DATA indication and get the page 3/3. |
|
| 12.On the CAPT handwheel, push and hold the rudder-pedal disconnection pushbutton-switch. On the MCDU, push the line key adjacent to the REFRESH indication. |
|
| 13.Release the rudder-pedal disconnection pushbutton-switch. | |
| 14.Do again the steps 5 to 12 with the F/O handwheel. |
|
| 15.Push the line key adjacent to the RETURN indication to get the SYSTEM REPORT/TEST L/G page. |
|
| 16.Push the line key adjacent to the BSCU CHAN 2 indication. |
|
| 17.Do again the steps 3 to 14. |
|
| 18.Push the line key adjacent to the RETURN indication to get the SYSTEM REPORT/TEST L/G page. |
|
| 19.Push the line key adjacent to the BSCU CHAN 1 indication. |
|
| 20.Push the line key adjacent to the GND SCAN indication. |
|
21.If one or more of these messages is (are) shown:
| |
22.If one or more of these messages is (are) shown again:
| |
| 23.Open the circuit breakers 1GG and 2GG. Then close them to make sure that you put the BSCU CHAN 2 in the active mode. Do again the steps 18 to 21 for the BSCU CHAN 2: |
|
A. Test
5. Close-up| ACTION | RESULT |
|---|---|
| 1.Open the circuit breakers 1GG, 2GG, 3GG and 4GG. Then close the circuit breakers 1GG and 2GG first, then 3GG and 4GG to make sure that you put the BSCU CHAN 1 in the active mode. | |
| 2.On the MCDU, push the line key adjacent to the BSCU 1 indication. |
|
| 3.Push the line key adjacent to the SPECIFIC DATA indication. |
|
| 4.Push the line key adjacent to the STEERING DATA indication. |
|
| 5.Turn the CAPT handwheel fully counterclockwise and hold it in position. On the MCDU, push the line key adjacent to the REFRESH indication. |
|
| 6.Release the CAPT handwheel to the neutral position. | |
| 7.Turn the CAPT handwheel fully clockwise and hold it in position. On the MCDU, push the line key adjacent to the REFRESH indication. |
|
| 8.Release the CAPT handwheel to the neutral position. | |
| 9.Push the line key adjacent to the RETURN indication to get the SPECIFIC DATA indication |
|
| 10.Push the line key adjacent to the SYSTEM DATA indication and get the page 3/3. |
|
| 11.Set and hold a rudder angle with the rudder pedals. On the MCDU, push the line key adjacent to the REFRESH indication. |
|
| 12.On the CAPT handwheel, push and hold the rudder-pedal disconnection pushbutton-switch. On the MCDU, push the line key adjacent to the REFRESH indication. |
|
| 13.Release the rudder-pedal disconnection pushbutton-switch. | |
| 14.Do again the steps 5 to 13 with the F/O handwheel and F/O rudder pedals. |
|
| 15.Push the line key adjacent to the RETURN indication to get the SYSTEM REPORT/TEST L/G page. |
|
| 16.Push the line key adjacent to the BSCU 2 indication. |
|
| 17.Do again the steps 2 to 14. |
|
| 18.Push the line key adjacent to the RETURN indication to get the SYSTEM REPORT/TEST L/G page. |
|
| 19.Push the line key adjacent to the BSCU 1 indication. |
|
| 20.Push the line key adjacent to the GND SCAN indication. |
|
21.If one or more of these messages is (are) shown:
| |
22.If one or more of these messages is (are) shown again:
| |
| 23.Open the circuit breakers 1GG and 2GG. Then close them to make sure that you put the BSCU CHAN 2 in the active mode. Do again the steps 19 to 22 for the BSCU CHAN 2: |
|
Subtask 32-51-00-860-086-A ** ON A/C NOT FOR ALL
A. Put the aircraft back to its initial configuration.
(1) Depressurize the Blue hydraulic system (Ref. AMM TASK 29-10-00-864-003).
(2) On the MCDU, push the line key adjacent to the RETURN indication until the CFDS menu page comes into view.
(3) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
Subtask 32-51-00-860-086-B ** ON A/C NOT FOR ALL (1) Depressurize the Blue hydraulic system (Ref. AMM TASK 29-10-00-864-003).
(2) On the MCDU, push the line key adjacent to the RETURN indication until the CFDS menu page comes into view.
(3) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
A. Put the aircraft back to its initial configuration.
(1) On the MCDU, push the line key adjacent to the RETURN indication until the CFDS menu page comes into view.
(2) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
(1) On the MCDU, push the line key adjacent to the RETURN indication until the CFDS menu page comes into view.
(2) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).