Loss of the Leak Detection Loop A on the Right Wing

TASK 36-22-00-810-806-A
Loss of the Leak Detection Loop A on the Right Wing

1. Possible Causes

BMC-1 [1HA1]
wiring
sensing element
wiring from the connector AA/4D to the sensing element (80HF)
wiring from the sensing element (39HF) to the sensing element (42HF)
wiring from the sensing element (47HF) to the connector AA/5D

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
Component Location
Table of Component Location

3. Fault Confirmation
Subtask 36-22-00-710-050-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 36-22-00-810-055-B ** ON A/C NOT FOR ALL

A. If the test gives the maintenance message:
R WING LOOP A INOP

remove the BMC-1 [1HA1] AMM 36-11-34-000-001.
do a continuity check of the R wing loop A from pin AA/4D of the BMC1 to pin AA/5D of the BMC1 ASM 362201.

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:

do a check and clean all the connections ASM 362201 to remove contamination and decrease the resistance of the loop AMM 36-22-00-100-801.

(a) If the fault continues:

replace the BMC-1 [1HA1] AMM 36-11-34-400-001.

(2) If there is no continuity:

do a check of the wiring from pin AA/4D of the BMC1 to the cable (37HF) (found in the wing) and from pin AA/5D of the BMC1 to the cable (48HF) (found in the fuselage) ASM 362201.

(a) If there is no continuity:

repair the wiring .
install the BMC-1 [1HA1] AMM 36-11-34-400-001.

(b) If there is continuity:

do a visual inspection of the sensing elements on the R wing loop A.

1 If a sensing element is damaged:

replace the sensing element .
install the BMC-1 [1HA1] AMM 36-11-34-400-001.

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 the sensing element:

replace the sensing element: AMM 36-22-16-000-001 AMM 36-22-16-000-004 AMM 36-22-16-000-005 AMM 36-22-16-000-006 AMM 36-22-16-400-001 AMM 36-22-16-400-004 AMM 36-22-16-400-005 AMM 36-22-16-400-007.
install the BMC-1 [1HA1] AMM 36-11-34-400-001.

b If there is continuity on the sensing element:

do a check and repair the wiring from the connector AA/4D to the sensing element (80HF) ASM 362201.
do a check and repair the wiring from the sensing element (39HF) to the sensing element (42HF) ASM 362201.
do a check and repair the wiring from the sensing element (47HF) to the connector AA/5D ASM 362201.
install the BMC-1 [1HA1] AMM 36-11-34-400-001.

Subtask 36-22-00-710-051-A ** ON A/C NOT FOR ALL

B. Do the test given in Para. 3.

[Rev.8 from Aug 2018] 2026.04.04 04:34:02 UTC