Leak Detection from the Loop B in the Right Wing
TASK 36-22-00-810-878-A
Leak Detection from the Loop B in the Right Wing
1. Possible Causes
A. Fixtures, Tools, Test and Support Equipment
B. Referenced Information
3. Fault Confirmation
Subtask 36-22-00-710-127-A ** ON A/C NOT FOR ALL
Subtask 36-22-00-810-148-A ** ON A/C NOT FOR ALL
[Rev.8 from Aug 2018]
2026.04.04 04:34:10 UTC
Leak Detection from the Loop B in the Right Wing
1. Possible Causes
- CABLE ASSY [76HF]
- wiring
- OVHT SENS ELEMENT [75HF]
- OVHT SENS ELEMENT [79HF]
- INTERCONNECTING CABLE [93HF]
- SNSG ELEM-OVHT, R WING LOOP B [72HF]
- SNSG ELEM-OVHT, R WING LOOP B [71HF]
- SNSG ELEM-OVHT, R WING LOOP B [70HF]
- SNSG ELEM-OVHT, R WING LOOP B [69HF]
- CABLE-CONNECTING, R WING LOOP B [68HF]
- CABLE-CONNECTING, R WING LOOP B [67HF]
- SNSG ELEM-OVHT, R WING LOOP B [66HF]
- SNSG ELEM-OVHT, R WING LOOP B [65HF]
- SNSG ELEM-OVHT, R WING LOOP B [82HF]
- CABLE-CONNECTING, R WING LOOP B [64HF]
- duct
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| 9240SI | 1 | CONTROLLER-LOOP |
| REFERENCE | DESIGNATION |
|---|---|
| AMM 36-11-00-740-802 | BITE Test of the Engine Bleed Air System (EBAS) (System Test) |
| AMM 36-11-34-000-001 | Removal of the BMC |
| AMM 36-11-34-400-001 | Installation of the BMC |
| AMM 36-11-48-000-003 | Removal of the Bleed Air Ducts |
| AMM 36-11-48-400-004 | Installation of the Bleed Air Ducts |
| AMM 36-11-48-790-802 | Leak Check on Bleed Air Ducting in Wing Area between Bleed Air Precooler Wing Anti Ice Valve and Wing/Fuselage Connection |
| AMM 36-22-00-790-802 | Leak Check on all the Bleed Air Ducts and Packs Components |
| ASM 362201 | |
| AMM 36-22-16-000-001 | Removal of the Overheat Sensing Elements |
| AMM 36-22-16-000-002 | Removal of the Cables |
| AMM 36-22-16-000-003 | Removal of the Cables |
| 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 36-22-16-000-007 | Removal of the Cables |
| AMM 36-22-16-400-001 | Installation of the Overheat Sensing Elements |
| AMM 36-22-16-400-002 | Installation of the Cables |
| AMM 36-22-16-400-003 | Installation of the Cables |
| 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 |
| AMM 36-22-16-400-008 | Installation of the Cables |
| AMM 36-22-18-000-001 | Removal of the Fuselage Overheat Sensing-Elements (Loop A and B) |
| AMM 36-22-18-400-001 | Installation of the Fuselage Overheat Sensing-Elements (Loop A and B) |
Subtask 36-22-00-710-127-A ** ON A/C NOT FOR ALL
A. Test
4. Fault IsolationNOTE: The overheat detection threshold is between 117 and 131 degrees Celsius.
An overheat detection by one loop can occur in these conditions:
(1) Do the BITE test of the EBAS AMM 36-11-00-740-802. An overheat detection by one loop can occur in these conditions:
- High Outside Air Temperature (OAT).
- ECS supplied with hot bleed air.
In these conditions, the ambient air around the sensing elements can increase to the detection threshold but there is not an air leak.
If there is an air leak, there will be an AIR L(R) WING LEAK warning on the ECAM.
No other maintenance action is necessary if: - The overheat detection was by one loop only with high OAT and ECS supplied with hot bleed air.
- The result of the BMC BITE test is TEST OK.
Subtask 36-22-00-810-148-A ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message:
R WING LOOP B
The elements that follow can be found in the FUSELAGE:
(b) If no sensing element is damaged:
The elements that follow can be found in the WING:
b If the impedance is more than 10 kOhms:
Subtask 36-22-00-810-149-A ** ON A/C NOT FOR ALL R WING LOOP B
- Remove BMC2 (1HA2) AMM 36-11-34-000-001.
- On shelf 96VU, connect the 9240SI CONTROLLER-LOOP between connector 1HA2-AA/4F and the ground ASM 362201.
- Do a check of the impedance read on the 9240SI CONTROLLER-LOOP.
- Disconnect the 9240SI CONTROLLER-LOOP from the BMC2 connector.
- Install BMC2 (1HA2) AMM 36-11-34-400-001.
- Refer to Para. 4.C.
- Do a check of the correct installation of the sensing elements along the bleed duct.
- Do a wiring check.
- Do a visual inspection of the sensing elements and cables on the R wing loop B.
- Replace the sensing element or cable AMM 36-22-16-000-001, AMM 36-22-16-400-001, AMM 36-22-16-000-002, AMM 36-22-16-400-002, AMM 36-22-16-000-003, AMM 36-22-16-400-003, AMM 36-22-16-000-004, AMM 36-22-16-400-004, AMM 36-22-16-000-005, AMM 36-22-16-400-005, AMM 36-22-16-000-006, AMM 36-22-16-400-007, AMM 36-22-16-000-007, AMM 36-22-16-400-008.
- Disconnect the 9240SI CONTROLLER-LOOP from the BMC2 connector.
- Install BMC2 AMM 36-11-34-400-001.
- Refer to Para. 4.C.
The elements that follow can be found in the FUSELAGE:
(b) If no sensing element is damaged:
- Disconnect the connector between sensing element 69HF (found in the wing) and cable 70HF (found in the wing).
- Connect the 9240SI CONTROLLER-LOOP between BMC2 connector 1HA2-AA/4F and the ground.
- Do a check of the impedance read on the 9240SI CONTROLLER-LOOP.
NOTE: You must use a dichotomy method to find the defective sensing element:
1 If the impedance is less than 10 kOhms: - Disconnect a connector in the middle of the loop.
- Measure the resistance of one of the halves.
If the measurement is correct, you must do a check of the other half.
If the measurement is not correct, do the same operation in the defective half again until you find the defective sensing element.
- Disconnect the connector between sensing elements 79HF (found in the fuselage) and 93HF (found in the wing).
- Do a check of the impedance read or the 9240SI CONTROLLER-LOOP.
- Disconnect the connector between sensing element 75HF and cable 76HF.
- Do a check of the impedance read on the 9240SI CONTROLLER-LOOP.
* If the impedance is less than 10 kOhms:
- Replace the CABLE ASSY [76HF] AMM 36-22-18-000-001 and AMM 36-22-18-400-001. - Do a check of the impedance read on the 9240SI CONTROLLER-LOOP.
** If the impedance is less than 10 kOhms:
- Do a check and repair the wiring between pin AA/4F of BMC2 (1HA2) and cable 76HF ASM 362201.
- Connect all the cables or connectors disconnected.
- Disconnect the 9240SI CONTROLLER-LOOP from the BMC2 connector.
- Install BMC2 (1HA2) AMM 36-11-34-400-001.
- Refer to Para. 4.C.
** If the impedance is more than 10 kOhms:
- Connect all the cables or connectors disconnected.
- Disconnect the 9240SI CONTROLLER-LOOP from the BMC2 connector.
- Install BMC2 (1HA2) AMM 36-11-34-400-001.
- Refer to Para. 4.C.
* If the impedance is more than 10 kOhms:
- Disconnect the connector between sensing elements 75HF and 79HF.
- Connect the connector between sensing element 75HF and cable 76HF.
- Do a check of the impedance read on the 9240SI CONTROLLER-LOOP.
** If the impedance is less than 302 kOhms:
- Replace the OVHT SENS ELEMENT [75HF] AMM 36-22-18-000-001 and AMM 36-22-18-400-001.
- Connect all the cables or connectors disconnected.
- Disconnect the 9240SI CONTROLLER-LOOP from the BMC2 connector.
- Install BMC2 (1HA2) AMM 36-11-34-400-001.
- Refer to Para. 4.C.
** If the impedance is more than 302 kOhms:
- Disconnect the connector between sensing elements 79HF (found in the fuselage) and 93HF (found in the wing).
- Connect the connector between sensing element 75HF and sensing element 79HF.
- Do a check of the impedance read of the 9240SI CONTROLLER-LOOP.
*** If the impedance is less than 10 kOhms:
- Replace the OVHT SENS ELEMENT [79HF] AMM 36-22-18-000-001 and AMM 36-22-18-400-001.
- Connect all the cables or connectors disconnected.
- Disconnect the 9240SI CONTROLLER-LOOP from the BMC2 connector.
- Install BMC2 (1HA2) AMM 36-11-34-400-001.
- Refer to Para. 4.C.
*** If the impedance is more than 10 kOhms:
- Replace the INTERCONNECTING CABLE [93HF] AMM 36-22-18-000-001 and AMM 36-22-18-400-001.
- Connect all the cables or connectors disconnected.
- Disconnect the 9240SI CONTROLLER-LOOP from the BMC2 connector.
- Install BMC2 (1HA2) AMM 36-11-34-400-001.
- Refer to Para. 4.C.
The elements that follow can be found in the WING:
b If the impedance is more than 10 kOhms:
- Disconnect the connector between sensing element 72HF and 71HF.
- Connect the connector between sensing elements 79HF (found in the fuselage) and 93HF (found in the wing).
- Do a check of the impedance read on the 9240SI CONTROLLER-LOOP.
* If the impedance is less than 10 kOhms:
- Replace the SNSG ELEM-OVHT, R WING LOOP B [72HF] AMM 36-22-16-000-001 and AMM 36-22-16-400-001.
- Connect all the cables or connectors disconnected.
- Disconnect the 9240SI CONTROLLER-LOOP from the BMC2 connector.
- Install BMC2 (1HA2) AMM 36-11-34-400-001.
- Refer to Para. 4.C.
* If the impedance is more than 10 kOhms:
- Disconnect the connector between sensing elements 71HF and 70HF.
- Connect the connector between sensing elements 72HF and 71HF.
- Do a check of the impedance read on the 9240SI CONTROLLER-LOOP.
** If the impedance is less than 10 kOhms:
- Replace the SNSG ELEM-OVHT, R WING LOOP B [71HF] AMM 36-22-16-000-006 and AMM 36-22-16-400-007.
- Connect all the cables or connectors disconnected.
- Disconnect the 9240SI CONTROLLER-LOOP from the BMC2 connector.
- Install BMC2 (1HA2) AMM 36-11-34-400-001.
- Refer to Para. 4.C.
** If the impedance is more than 10 kOhms:
- Replace the SNSG ELEM-OVHT, R WING LOOP B [70HF] AMM 36-22-16-000-005 and AMM 36-22-16-400-005.
- Connect all the cables or connectors disconnected.
- Disconnect the 9240SI CONTROLLER-LOOP from the BMC2 connector.
- Install BMC2 (1HA2) AMM 36-11-34-400-001.
- Refer to Para. 4.C.
- Disconnect the connector between cables 67HF and 66HF.
- Connect the connector between sensing elements 69HF and 70HF.
- Do a check of the impedance read on the 9240SI CONTROLLER-LOOP.
- Disconnect the connector between sensing elements 69HF and 68HF.
- Do a check of the impedance read on the 9240SI CONTROLLER-LOOP.
* If the impedance is less than 10 kOhms:
- Replace the SNSG ELEM-OVHT, R WING LOOP B [69HF] AMM 36-22-16-000-004 and AMM 36-22-16-400-004.
- Connect all the cables or connectors disconnected.
- Disconnect the 9240SI CONTROLLER-LOOP from the BMC2 connector.
- Install BMC2 (1HA2) AMM 36-11-34-400-001.
- Refer to Para. 4.C.
* If the impedance is more than 10 kOhms:
- Disconnect the connector between sensing elements 68HF and cable 67HF.
- Connect the connector between sensing elements 69HF and 68HF.
- Do a check of the impedance read on the 9240SI CONTROLLER-LOOP.
** If the impedance is less than 10 kOhms:
- Replace the CABLE-CONNECTING, R WING LOOP B [68HF] AMM 36-22-16-000-007 and AMM 36-22-16-400-008.
- Connect all the cables or connectors disconnected.
- Disconnect the 9240SI CONTROLLER-LOOP from the BMC2 connector.
- Install BMC2 (1HA2) AMM 36-11-34-400-001.
- Refer to Para. 4.C.
** If the impedance is more than 10 kOhms:
- Replace the CABLE-CONNECTING, R WING LOOP B [67HF] AMM 36-22-16-000-003 and AMM 36-22-16-400-003.
- Connect all the cables or connectors disconnected.
- Disconnect the 9240SI CONTROLLER-LOOP from the BMC2 connector.
- Install BMC2 (1HA2) AMM 36-11-34-400-001.
- Refer to Para. 4.C.
- Disconnect the connector between sensing elements 65HF and 82HF.
- Connect the connector between cables 67HF and 66HF.
- Do a check of the impedance read on the 9240SI CONTROLLER-LOOP.
* If the impedance is less than 10 kOhms:
- Disconnect the connector between sensing element 65HF and cable 66HF.
- Do a check of the impedance read on the 9240SI CONTROLLER-LOOP.
** If the impedance is less than 10 kOhms:
- Replace the SNSG ELEM-OVHT, R WING LOOP B [66HF] AMM 36-22-16-000-005 and AMM 36-22-16-400-005.
- Connect all the cables or connectors disconnected.
- Disconnect the 9240SI CONTROLLER-LOOP from the BMC2 connector.
- Install BMC2 (1HA2) AMM 36-11-34-400-001.
- Refer to Para. 4.C.
** If the impedance is more than 10 kOhms:
- Replace the SNSG ELEM-OVHT, R WING LOOP B [65HF] AMM 36-22-16-000-006 and AMM 36-22-16-400-007.
- Connect all the cables or connectors disconnected.
- Disconnect the 9240SI CONTROLLER-LOOP from the BMC2 connector.
- Install BMC2 (1HA2) AMM 36-11-34-400-001.
- Refer to Para. 4.C.
* If the impedance is more than 10 kOhms:
- Connect the connector between sensing elements 65HF and 82HF.
- Disconnect the connector between sensing element 82HF and the cable 64HF.
- Do a check of the impedance read on the 9240SI CONTROLLER-LOOP.
** If the impedance is less than 10 kOhms:
- Replace the SNSG ELEM-OVHT, R WING LOOP B [82HF] AMM 36-22-16-000-001 and AMM 36-22-16-400-001.
- Connect all the cables or connectors disconnected.
- Disconnect the 9240SI CONTROLLER-LOOP from the BMC1 connector.
- Install BMC2 (1HA2) AMM 36-11-34-400-001.
- Refer to Para. 4.C.
** If the impedance is more than 10 kOhms:
- Replace the CABLE-CONNECTING, R WING LOOP B [64HF] AMM 36-22-16-000-002 and AMM 36-22-16-400-002.
- Connect all the cables or connectors disconnected.
- Do a check of the impedance read on the 9240SI CONTROLLER-LOOP.
*** If the impedance is less than 10 kOhms:
- Do a check and repair the wiring between pin AA/5F of BMC2 (1HA2) and cable 64HF ASM 362201.
- Connect all the cables or connectors disconnected.
- Disconnect the 9240SI CONTROLLER-LOOP from the BMC2 connector.
- Install BMC2 (1HA2) AMM 36-11-34-400-001.
- Refer to Para. 4.C.
*** If the impedance is more than 10 kOhms:
- Connect all the cables or connectors disconnected.
- Disconnect the 9240SI CONTROLLER-LOOP from the BMC2 connector.
- Install BMC2 (1HA2) AMM 36-11-34-400-001.
- Refer to Para. 4.C.
B. If the test gives the TEST OK message:
Subtask 36-22-00-710-128-A ** ON A/C NOT FOR ALL - Do the leak check of the bleed air supply system AMM 36-11-48-790-802.
- Do the leak check on the bleed air ducts AMM 36-22-00-790-802.
- Replace the duct which causes the leak AMM 36-11-48-000-003 and AMM 36-11-48-400-004.
C. Do the test given in Para. 3.