W DOC AIRBUS | TSM A320F

Rudder Trim Indicator Inoperative


TASK 22-62-00-810-818-A
Rudder Trim Indicator Inoperative


1. Possible Causes
  • IND-RUDDER TRIM [17CC]
  • wiring of the FAC 1 bus from the rudder-trim indicator (17CC) to the first terminal block
  • wiring of the FAC 2 bus from the rudder-trim indicator (17CC) to the first terminal block
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 22-62-00-710-001
Operational Test of the Rudder Trim Function
ASM 226901
3. Fault Confirmation
Subtask 22-62-00-710-086-A
A. Test
   (1) Do the operational test of the rudder trim function AMM 22-62-00-710-001.
4. Fault Isolation
Subtask 22-62-00-810-082-A
A. If the values shown on the rudder-trim indicator do not agree with the rudder movement indication on the lower ECAM DU (with the FAC 1 engaged):
  • replace the IND-RUDDER TRIM [17CC] .
   (1) If the fault continues:
  • do a check and repair the wiring of the FAC 1 bus from the rudder-trim indicator (17CC) to the first terminal block, ASM 226901.
Subtask 22-62-00-810-083-A
B. If the values shown on the rudder-trim indicator do not agree with the rudder movement indication on the lower ECAM DU (with the FAC 2 engaged):
  • replace the IND-RUDDER TRIM [17CC] .
   (1) If the fault continues:
  • do a check and repair the wiring of the FAC 2 bus from the rudder-trim indicator (17CC) to the first terminal block, ASM 226901.
Subtask 22-62-00-710-087-A
C. Do the test given in Para. 3.
[Rev.8 from Aug 2018] 2026.04.04 04:25:12 UTC