W DOC AIRBUS | TSM A320F

BMC1 output failure for HP Bleed Override Solenoid of Engine 1


TASK 36-11-00-810-930-A
BMC1 output failure for HP Bleed Override Solenoid of Engine 1


1. Possible Causes
  • BMC-1 [1HA1]
  • SOL-HP BLEED OVERRIDE, ENG1 [11HA1]
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
AMM 36-11-58-000-001
Removal of the HP Bleed Override Solenoid
AMM 36-11-58-400-001
Installation of the HP Bleed Override Solenoid
3. Fault Confirmation
Subtask 36-11-00-740-052-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 36-11-00-810-218-A ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message:
BMC1 OR SOLENOID 11HA1
   (1) If the fault continues:
Subtask 36-11-00-810-218-C ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message:
BMC1 OR SOLENOID 11HA1
NOTE: If the maintenance message BMC1 OR SOLENOID 11HA1 comes into view with no associated ECAM warning, no trouble shooting procedure is necessary.
   (1) If the fault continues:
Subtask 36-11-00-740-053-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