W DOC AIRBUS | AMM A320F

Operational Test of the Overheat Detection System


TASK 36-22-00-710-001-A
Operational Test of the Overheat Detection System


FIN: 1000EM1 ** ON A/C NOT FOR ALL
FIN: 1000EM2 ** ON A/C NOT FOR ALL
1. Reason for the Job
Do a continuity test of the overheat detection.
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
WARNING NOTICE(S)
 B. Referenced Information
REFERENCE
DESIGNATION
TASK 24-41-00-861-002-A
Energize the Aircraft Electrical Circuits from the External Power
TASK 24-41-00-861-002-A-01
Energize the Aircraft Electrical Circuits from the APU
TASK 24-41-00-861-002-A-02
Energize the Aircraft Electrical Circuits from Engine 1(2)
TASK 24-41-00-862-002-A
De-energize the Aircraft Electrical Circuits Supplied from the External Power
TASK 24-41-00-862-002-A-01
De-energize the Aircraft Electrical Circuits Supplied from the APU
TASK 24-41-00-862-002-A-02
De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2)
TASK 36-11-00-740-001-A
BITE Test of the BMC 1(2)
3. Job Set-up
Subtask 36-22-00-861-050-A ** ON A/C NOT FOR ALL
A. Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
Subtask 36-22-00-941-050-A ** ON A/C NOT FOR ALL
B. Safety Precautions
   (1) Make sure that the engine 1(2) shut down occured not less than 5 minutes before you do this procedure.
   (2) On the ENG panel 115VU, put a WARNING NOTICE(S) to tell persons not to start the engine 1(2).
   (3) On the ENG section of the panel 50VU:
  • make sure that the ON legend of the ENG/FADEC GND PWR 1(2) pushbutton switch is off.
  • put a WARNING NOTICE(S) to tell persons not to energize the FADEC 1(2).
4. Procedure
Subtask 36-22-00-710-050-B ** ON A/C NOT FOR ALL
A. Operational Test of the Overheat Detection System
   (1) Do the BITE Test of the BMC1 and BMC2 with printing of each TEST RESULT page. (Ref. AMM TASK 36-11-00-740-001)
   (2) Make sure that the TEST RESULT pages do not show these maintenance indications:
ATA
MESSAGE
CLASS FAULT
361134
BMC1 (1HA1)
2
361134
BMC2 (1HA2)
2
362216
R WING LOOP A INOP
2
362216
R WING LOOP B INOP
2
362216
L WING LOOP A INOP
2
362216
L WING LOOP B INOP
2
362216
ENG 1 PYLON LOOP INOP
2
362216
ENG 2 PYLON LOOP INOP
2
362216
ENGINE 1 PYLON LOOP
1
362216
ENGINE 2 PYLON LOOP
1
362217
APU LOOP
1
362216
APU LOOP INOP OR BMC
IDENT CKT
2
362216
L WING LOOP A
2
362216
L WING LOOP B
2
362216
R WING LOOP A
2
362216
R WING LOOP B
2
5. Close-up
Subtask 36-22-00-942-050-A ** ON A/C NOT FOR ALL
A. Remove the WARNING NOTICE(S).
Subtask 36-22-00-862-050-A ** ON A/C NOT FOR ALL
B. De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
[Rev.10 from 2021] 2026.04.01 12:39:43 UTC