W DOC AIRBUS | TSM A320F

Loss of the Altitude Bus 2 of the RA Transceiver 1 Identified by the GPWS


TASK 34-42-00-810-813-A
Loss of the Altitude Bus 2 of the RA Transceiver 1 Identified by the GPWS


1. Possible Causes
  • XCVR-RA, 1 [2SA1]
  • wiring of the ALTITUDE BUS 2 from the RA transceiver 1 (2SA1) to the first terminal block
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
ASM 344201
AMM 34-42-33-000-001
Removal of the Radio Altimeter Transceiver
AMM 34-42-33-400-001
Installation of the Radio Altimeter Transceiver
AMM 34-48-00-740-002
BITE Test of the GPWS
3. Fault Confirmation
Subtask 34-42-00-865-062-A
A. Make sure that this(these) circuit breaker(s) is(are) closed:
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
121VUCOM NAV/RAD ALTM/11SA1K11
Subtask 34-42-00-740-066-C
B. Test
   (1) Do the BITE test of the Enhanced GPWS AMM 34-48-00-740-002.
4. Fault Isolation
Subtask 34-42-00-810-064-A
A. If the test gives the maintenance message RA1 (1SA1)/GPWC (1WZ):
   (1) If the fault continues:
  • do a check and repair the wiring of the ALTITUDE BUS 2 from the RA transceiver 1 (2SA1) to the first terminal block ASM 344201.
Subtask 34-42-00-740-067-A
B. Do the test given in Para. 3.B.
[Rev.8 from Aug 2018] 2026.04.04 04:33:08 UTC