W DOC AIRBUS | TSM A320F

BMC2 output failure for HP Bleed Override Solenoid of Engine 2


TASK 36-11-00-810-931-A
BMC2 output failure for HP Bleed Override Solenoid of Engine 2


1. Possible Causes
  • BMC-2 [1HA2]
  • SOL-HP BLEED OVERRIDE, ENG2 [11HA2]
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 36-11-00-740-054-A ** ON A/C NOT FOR ALL
A. Test
   (1) Do the BITE test of the BMC2 AMM 36-11-00-740-001.
4. Fault Isolation
Subtask 36-11-00-810-219-A ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message:
BMC2 OR SOLENOID 11HA2
   (1) If the fault continues:
Subtask 36-11-00-810-219-C ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message:
BMC2 OR SOLENOID 11HA2
NOTE: If the maintenance message BMC2 OR SOLENOID 11HA2 comes into view with no associated ECAM warning, no trouble shooting procedure is necessary.
   (1) If the fault continues:
Subtask 36-11-00-740-055-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