W DOC AIRBUS | TSM A320F

Spurious APU leak indication on the Engine 1


TASK 36-11-00-810-951-A
Spurious APU leak indication on the Engine 1


1. Possible Causes
  • BMC-1 [1HA1]
  • P/BSW-AIR COND/APU BLEED [5HV]
  • wiring
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 36-11-00-740-001
BITE Test of the BMC 1(2)
AMM 36-11-34-000-001
Removal of the BMC
AMM 36-11-34-400-001
Installation of the BMC
ASM 361201
3. Fault Confirmation
Subtask 36-11-00-740-056-A ** ON A/C NOT FOR ALL
A. Test
   (1) Do the BITE test of the BMC1 AMM 36-11-00-740-001.
4. Fault Isolation
Subtask 36-11-00-810-245-A ** ON A/C NOT FOR ALL
A. If the BITE test gives the maintenance message:
BMC1 OR APU FAULT IND 7HV
   (1) If the fault continues:
     (a) If the fault continues:
  • do a check and repair the wiring ASM 361201 between:
    . pin A/B1 of the APU bleed pushbutton switch (5HV) and pin AA/14C of the BMC1 (1HA1)
    . pin A/B3 and the ground.
Subtask 36-11-00-810-245-D ** ON A/C NOT FOR ALL
A. If the BITE test gives the maintenance message:
BMC1 OR APU FAULT IND 7HV
NOTE: If the maintenance message BMC1 OR APU FAULT IND 7HV comes into view with no associated ECAM warning, no trouble shooting procedure is necessary.
   (1) If the fault continues:
     (a) If the fault continues:
  • Do a check and repair the wiring ASM 361201 between:
    . Pin A/B1 of the APU bleed pushbutton switch (5HV) and pin AA/14C of the BMC1 (1HA1)
    . Pin A/B3 and the ground.
Subtask 36-11-00-740-057-A ** ON A/C NOT FOR ALL
B. Do the test given in Para. 3.
[Rev.8 from Aug 2018] 2026.04.04 04:33:50 UTC