W DOC AIRBUS | TSM A320F

Loss of the RA1 and RA2 Input to the GPWC


TASK 34-48-00-810-854-A
Loss of the RA1 and RA2 Input to the GPWC


1. Possible Causes
  • GPWC [1WZ]
  • XCVR-RA, 1 [2SA1]
  • XCVR-RA, 2 [2SA2]
  • wiring from the GPWC (1WZ) to the radio altimeter transceiver 1 (2SA1)
  • wiring from the GPWC (1WZ) to the radio altimeter transceiver 2 (2SA2)
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 34-42-00-740-002
BITE Test of the Radio Altimeter
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
ASM 344801
ASM 344802
AMM 34-48-34-000-001
Removal of the GPWC
AMM 34-48-34-400-001
Installation of the GPWC
3. Fault Confirmation
Subtask 34-48-00-740-116-A ** ON A/C NOT FOR ALL
A. Test
   (1) Do the BITE test of the Enhanced GPWS AMM 34-48-00-740-002.
4. Fault Isolation
Subtask 34-48-00-810-119-A ** ON A/C NOT FOR ALL
A. If the test gives the maintenance messages RA1(2SA1)/GPWC(1WZ) and RA2(2SA2)/GPWC(1WZ):
   (1) If the test gives a maintenance message:
  • Do the trouble shooting procedure related to the maintenance message.
   (2) If the test does not give a maintenance message:
     (a) If the fault continues:
       1 If the fault continues:
  • do a check and repair the wiring from the GPWC (1WZ) to the radio altimeter transceiver 1 (2SA1): from pins AB/13A, 13B to pins AB/2G, 3G ASM 344801.
  • do a check and repair the wiring from the GPWC (1WZ) to the radio altimeter transceiver 2 (2SA2): from pins AA/8C, 8D to pins AB/2G, 3G ASM 344802.
Subtask 34-48-00-740-117-A ** ON A/C NOT FOR ALL
B. Do the test given in Para. 3.
[Rev.8 from Aug 2018] 2026.04.04 04:33:18 UTC