W DOC AIRBUS | TSM A320F

Loss of the Leak Detection Loop A on the Left Wing


TASK 36-22-00-810-807-A
Loss of the Leak Detection Loop A on the Left Wing


1. Possible Causes
  • BMC-1 [1HA1]
  • wiring
  • sensing element
  • wiring from the connector AA/3B to the sensing element (81HF)
  • wiring from the sensing element (23HF) to the sensing element (26HF)
  • wiring from the sensing element (36HF) to the connector AA/4B
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 36-22-00-100-801
Clean the Overheat Detection System (OHDS) Connectors and Apply the Electrical Insulating Compound
ASM 362201
AMM 36-22-16-000-001
Removal of the Overheat Sensing Elements
AMM 36-22-16-000-004
Removal of the Overheat Sensing Elements
AMM 36-22-16-000-005
Removal of the Overheat Sensing Elements
AMM 36-22-16-000-006
Removal of the Overheat Sensing Elements
AMM 36-22-16-400-001
Installation of the Overheat Sensing Elements
AMM 36-22-16-400-004
Installation of the Overheat Sensing Elements
AMM 36-22-16-400-005
Installation of the Overheat Sensing Elements
AMM 36-22-16-400-007
Installation of the Overheat Sensing Elements
3. Fault Confirmation
Subtask 36-22-00-710-052-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 36-22-00-810-056-B ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message:
L WING LOOP A INOP
NOTE: This procedure is related to the loss of the wing-loop detection signal or to incorrect continuity of the loop.
The resistance of the loop must be less than 15 ohms at ambient temperature.
The BMC gives the maintenance message when the resistance of the loop is more than 75 ohms (discontinuity).
There is continuity when the resistance of the loop is less than 75 ohms.
   (1) If there is continuity and the resistance of the loop is between 15 ohms and 75 ohms:
     (a) If the fault continues:
   (2) If there is no continuity:
  • do a check of the wiring from pin AA/3B of the BMC1 to the cable (21HF) and from pin AA/4B of the BMC1 to the cable (30HF) ASM 362201.
     (a) If there is no continuity:
     (b) If there is continuity:
  • do a visual inspection of the sensing elements on the L wing loop A.
       1 If a sensing element is damaged:
       2 If no sensing element is damaged:
  • do a continuity check of each sensing element, one after the other.
         a If there is no continuity on a sensing element:
         b If there is continuity on a sensing element:
  • do a check and repair the wiring from the connector AA/3B to the sensing element (81HF) ASM 362201.
  • do a check and repair the wiring from the sensing element (23HF) to the sensing element (26HF) ASM 362201.
  • do a check and repair the wiring from the sensing element (36HF) to the connector AA/4B ASM 362201.
  • install the BMC-1 [1HA1] AMM 36-11-34-400-001.
Subtask 36-22-00-710-053-A ** ON A/C NOT FOR ALL
B. Do the test given in Para. 3.
[Rev.8 from Aug 2018] 2026.04.04 04:40:30 UTC