W DOC AIRBUS | AMM A320F

Reactivation of the BSCU Channel/System 1 or 2


TASK 32-42-00-440-006-A
Reactivation of the BSCU Channel/System 1 or 2


1. Reason for the Job
MMEL 32-42-03A
BRAKING/STEERING CONTROL UNIT (BSCU) CHANNEL 1
MMEL 32-42-04A
BRAKING/STEERING CONTROL UNIT (BSCU) CHANNEL 2
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
WARNING NOTICE(S)
 B. Referenced Information
REFERENCE
DESIGNATION
TASK 32-46-00-740-001-A
BITE Test of the BSCU
3. Job Set-up
Subtask 32-42-00-860-102-A
A. Aircraft Maintenance Configuration
   (1) On the panel 400VU, make sure that the landing gear control-lever is in the DOWN position.
   (2) Make sure that the CAPT and F/O brake pedals are released.
   (3) On the panel 402VU, make sure that the A/SKID & N/W STRG switch is at ON.
   (4) Make sure that the WARNING NOTICE(S) is(are) in position to tell persons not to operate:
  • the landing gear control-lever
  • the A/SKID & N/W STRG switch
  • the brake pedals.
Subtask 32-42-00-865-075-A
B. Table of the circuit breakers used in this procedure:
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
121VUHYDRAULIC/BRAKING AND STEERING/SYS2/SPLY4GGM36
121VUHYDRAULIC/BRAKING AND STEERING/SYS1/IND AND/SPLY2GGM33
4. Procedure
Subtask 32-42-00-440-057-B
A. Reactivation of the BSCU System 1 or 2
   (1) If the BSCU System 1 is deactivated:
  • Remove the safety clip and the tag and close the circuit breaker 2GG.
   (2) If the BSCU System 2 is deactivated:
  • Remove the safety clip and the tag and close the circuit breaker 4GG.
   (3) Do the BITE test of the BSCU (Ref. AMM TASK 32-46-00-740-001).
   (4) Do the trouble-shooting procedure related to the maintenance message.
   (5) Remove the applicable entry in the log book that refers to the deactivation of the BSCU system 1 or 2.
5. Close-up
Subtask 32-42-00-860-103-A
A. Put the aircraft back to the serviceable condition.
   (1) Remove the WARNING NOTICE(S).
[Rev.10 from 2021] 2026.04.01 00:47:29 UTC