W DOC AIRBUS | TSM A320F

Loss of the G/S Indication on the PFD(s) and ND(s)


TASK 34-36-00-810-822-A
Loss of the G/S Indication on the PFD(s) and ND(s)


1. Possible Causes
  • MMR-1 [40RT1]
  • wiring from the glide/slope 1/2 antenna (4RT) to the MMR-1 (40RT1)
  • ANTENNA-GLIDE/SLOPE 1/2 [4RT]
  • MMR-2 [40RT2]
  • wiring from the glide/slope 1/2 antenna (4RT) to the MMR-2 (40RT2)
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
ESPM 2044160
AMM 34-36-00-720-002
Functional Test of the ILS
AMM 34-36-00-720-006
Functional Test of the ILS
ASM 343601
AMM 34-36-18-000-001
Removal of the Glide/Slope Antenna
AMM 34-36-18-400-001
Installation of the Glide/Slope Antenna
AMM 34-36-31-000-001
Removal of the ILS Receiver
AMM 34-36-31-400-001
Installation of the ILS Receiver
3. Fault Confirmation
Subtask 34-36-00-720-050-B ** ON A/C NOT FOR ALL
A. Test
Do the functional test of the MMR AMM 34-36-00-720-002.
Subtask 34-36-00-720-050-C ** ON A/C NOT FOR ALL
A. Test
Do the functional test of the MMR AMM 34-36-00-720-006.
4. Fault Isolation
Subtask 34-36-00-810-073-B
A. If the G/S indication does not come into view on the CAPT PFD and F/O ND during the test:
   (1) If the fault continues:
  • Do a check of the wiring from the glide/slope 1/2 antenna (4RT) to the MMR-1 (40RT1), ASM 343601 and ESPM 2044160.
     (a) If there is no continuity:
  • Repair the above wiring.
     (b) If there is continuity:
Subtask 34-36-00-810-074-B
B. If the G/S indication does not come into view on the F/O PFD and CAPT ND during the test:
   (1) If the fault continues:
  • Do a check of the wiring from the glide/slope 1/2 antenna (4RT) to the MMR-2 (40RT2), ASM 343601 and ESPM 2044160.
     (a) If there is no continuity:
  • Repair the above wiring.
     (b) If there is continuity:
Subtask 34-36-00-810-085-A
C. If the G/S indication does not come into view on the two PFDs and the two NDs during the test:
Subtask 34-36-00-720-051-A
D. Do the test given in Para. 3.
[Rev.8 from Aug 2018] 2026.04.04 04:32:58 UTC