W DOC AIRBUS | TSM A320F

Failure of the FAC 2


TASK 22-66-00-810-802-A
Failure of the FAC 2


1. Possible Causes
  • FAC-2 [1CC2]
  • wiring of the 28VDC signal from the circuit breaker (5CC2) to the FAC 2 (1CC2)
  • wiring of the ground signal at the FAC 2 (1CC2)
  • C/B-AUTO FLT/FAC2/28VDC [5CC2]
  • RELAY-RUD TRIM 2 [7CC2]
  • RELAY-RTL SYS2 [13CC2]
  • ACTUATOR-RUDDER TRIM [10CC]
  • LIMITATION UNIT-RUDDER TRAVEL [4CC]
  • short to ground between the circuit breaker 5CC2 and the three units
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
TSM TASK 22-63-00-810-802-A
Loss of the Yaw Damper Function on the FAC 2
AMM 22-66-34-000-002
Removal of the FAC
AMM 22-66-34-400-002
Installation of the FAC
ASM 226701
AMM 22-96-00-710-001
Operational Test of the AFS
AMM 27-22-51-000-001
Removal of the Rudder Trim Actuator
AMM 27-22-51-400-001
Installation of the Rudder Trim Actuator
AMM 27-23-51-000-001
Removal of the Rudder Travel Limitation Unit
AMM 27-23-51-400-001
Installation of the Rudder Travel-Limitation Unit
3. Fault Confirmation
Subtask 22-66-00-865-089-A
A. Make sure that this(these) circuit breaker(s) is(are) closed:
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
121VUAUTO FLT/FAC2/28VDC5CC2M19
Subtask 22-66-00-710-051-A
B. Test
   (1) Do the operational test of the AFS AMM 22-96-00-710-001 and read the result for the FAC 2.
     (a) If the circuit breaker 5CC2 is open refer to Para. 4.B.
4. Fault Isolation
Subtask 22-66-00-810-051-A
A. If the circuit breaker 5CC2 is closed, and if the test gives the maintenance message AFS: FAC2:
  • Do a check for 28VDC at the FAC 2 (1CC2).
   (1) If there is 28VDC:
   (2) If there is no 28VDC:
  • Do a check of the wiring of the 28VDC signal from the circuit breaker (5CC2) to the FAC 2 (1CC2).
  • Do a check of the wiring of the ground signal at the FAC 2 (1CC2) pin AC/3.
    ASM 226701.
     (a) If there is no continuity:
  • Repair the above wirings.
     (b) If there is continuity:
  • Replace the C/B-AUTO FLT/FAC2/28VDC [5CC2] .
Subtask 22-66-00-810-096-A
B. If the circuit breaker 5CC2 is open:
  • Close this circuit breaker.
   (1) If this circuit breaker opens again:
  • Disconnect these three units:
    FAC-2 [1CC2]
    RELAY-RUD TRIM 2 [7CC2]
    RELAY-RTL SYS2 [13CC2]
  • Close the circuit breaker 5CC2.
     (a) If the circuit breaker 5CC2 opens again:
  • Go to Para. 4. D.
     (b) If the circuit breaker 5CC2 stays closed:
  • Connect the FAC-2 [1CC2] .
       1 If the circuit breaker 5CC2 opens again:
         a If the circuit breaker 5CC2 opens again:
       2 If the circuit breaker 5CC2 stays closed:
  • Continues the troubleshooting.
Subtask 22-66-00-810-181-A
C. If the circuit breaker 5CC2 stays closed:
  • Connect the RELAY-RUD TRIM 2 [7CC2] .
   (1) If the circuit breaker 5CC2 opens again:
   (2) If the circuit breaker 5CC2 stays closed:
  • Connect the RELAY-RTL SYS2 [13CC2] .
     (a) If the circuit breaker 5CC2 opens again:
Subtask 22-66-00-810-182-A
D. If the circuit breaker 5CC2 opens again:
   (1) Do a check for a short to ground between the circuit breaker 5CC2 and the three units , ASM 226701.
     (a) If there is a short to ground:
  • Repair the related wiring.
     (b) If there is no short to ground:
  • Replace the C/B-AUTO FLT/FAC2/28VDC [5CC2] .
Subtask 22-66-00-710-130-A
E. Put the aircraft back to its initial configuration.
   (1) Connect all the units.
   (2) Do the test given in Para. 3.
[Rev.8 from Aug 2018] 2026.04.04 04:25:15 UTC