W DOC AIRBUS | TSM A320F

Failure of the Nose Wheel Steering Servo-Control


TASK 32-51-00-810-834-A
Failure of the Nose Wheel Steering Servo-Control


1. Possible Causes
  • SERVO CTL-N/W STEERING [6GC]
  • BSCU [10GG]
  • upper support attachment bolts
2. Job Set-up Information
 A. Consumable Materials
REFERENCE
DESIGNATION
(Material No.03HBD9)
Synthetic Ester base Grease-General Purpose Low Temp -
 B. Referenced Information
REFERENCE
DESIGNATION
AMM 07-11-00-581-003
Lifting of the Aircraft at the Forward Jacking Point, MLG Wheels on the Ground
AMM 07-11-00-586-001
Lowering of the Aircraft at Forward Jacking Point, MLG Wheels on the Ground
AMM 09-10-00-584-002
Towing by the Nose Landing Gear from the Front with a Towbar
AMM 24-41-00-861-002
Energize the Aircraft Electrical Circuits from the External Power
AMM 24-41-00-862-002
De-energize the Aircraft Electrical Circuits Supplied from the External Power
AMM 29-10-00-863-001
Pressurize the Green Hydraulic System with a Hydraulic Ground Power-Cart
AMM 29-10-00-863-002
Pressurize the Yellow Hydraulic System with a Hydraulic Ground Power-Cart
AMM 29-10-00-864-001
Depressurize the Green Hydraulic System
AMM 29-10-00-864-002
Depressurize the Yellow Hydraulic System
AMM 32-42-34-000-001
Removal of the Braking/Steering Control Unit (BSCU)
AMM 32-42-34-400-001
Installation of the Braking/Steering Control Unit (BSCU)
AMM 32-51-51-000-001
Removal of the Nose-Wheel Steering Servo-Control
AMM 32-51-51-400-001
Installation of the Nose-Wheel Steering Servo-Control
3. Fault Confirmation
Subtask 32-51-00-710-056-A ** ON A/C NOT FOR ALL
A. Test
   (1) Energize the aircraft electrical circuits AMM 24-41-00-861-002.
   (2) Pressurize the Green hydraulic system AMM 29-10-00-863-001.
   (3) On the nose gear leg, on the nose-wheel steering deactivation electrical box:
  • make sure that the towing lever is in the TOWING (disengaged) position.
NOTE: Two square steel plates are necessary.
   (4) Put one of the steel plates in position in front of the nose wheels.
   (5) Apply a thick layer of Synthetic Ester base Grease-General Purpose Low Temp - (Material No.03HBD9) to the top of the greased steel plate.
   (6) Put the other steel plate on the top of the greased steel plate.
   (7) Move the aircraft and put the nose wheels on the steel plates AMM 09-10-00-584-002.
NOTE: Do not disconnect the tow bar from the aircraft.
   (8) With the tow bar, try to change the direction of the nose wheels.
Subtask 32-51-00-710-056-B ** ON A/C NOT FOR ALL
A. Test
   (1) Energize the aircraft electrical circuits AMM 24-41-00-861-002.
   (2) Pressurize the Yellow hydraulic system AMM 29-10-00-863-002.
   (3) On the nose gear leg, on the nose-wheel steering deactivation electrical box:
  • Make sure that the towing lever is in the TOWING (disengaged) position.
NOTE: Two square steel plates are necessary.
   (4) Put one of the steel plates in position in front of the nose wheels.
   (5) Apply a thick layer of Synthetic Ester base Grease-General Purpose Low Temp - (Material No.03HBD9) to the top of the greased steel plate.
   (6) Put the other steel plate on the top of the greased steel plate.
   (7) Move the aircraft and put the nose wheels on the steel plates AMM 09-10-00-584-002.
NOTE: Do not disconnect the tow bar from the aircraft.
   (8) With the tow bar, try to change the direction of the nose wheels.
4. Fault Isolation
Subtask 32-51-00-810-096-A
A. If you cannot change the direction of the nose wheels:
   (1) If the fault continues:
     (a) If the fault continues:
  • Lift the aircraft at the forward jacking point AMM 07-11-00-581-003.
  • Manually shake the nose gear shock-absorber and make sure that there is no free play.
       1 If there is free play:
  • Do a check of the upper support attachment bolts .
  • Tighten, repair or replace as necessary.
Subtask 32-51-00-710-057-A
B. Test
   (1) Do the test given in Para. 3.A.
5. Close-up
Subtask 32-51-00-860-054-A ** ON A/C NOT FOR ALL
A. Put the aircraft back to its initial configuration.
   (1) Depressurize the Green hydraulic system AMM 29-10-00-864-001.
   (2) De-energize the aircraft electrical circuits AMM 24-41-00-862-002.
   (3) Remove the greased plates AMM 09-10-00-584-002.
   (4) Lower the aircraft to the ground AMM 07-11-00-586-001.
   (5) Make sure that the work area is clean and clear of tool(s) and other items.
Subtask 32-51-00-860-054-B ** ON A/C NOT FOR ALL
A. Put the aircraft back to its initial configuration.
   (1) Depressurize the Yellow hydraulic system AMM 29-10-00-864-002.
   (2) De-energize the aircraft electrical circuits AMM 24-41-00-862-002.
   (3) Remove the greased plates AMM 09-10-00-584-002.
   (4) Lower the aircraft to the ground AMM 07-11-00-586-001.
   (5) Make sure that the work area is clean and clear of tool(s) and other items.
[Rev.8 from Aug 2018] 2026.04.04 04:31:50 UTC