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_ -replace the CABLE ASSY (3HF2)
 -connect all the cables or connectors disconnected
 -do a check of the impedance read on the LOOP CONTROLLER (9240SI) . if the impedance is less than 3 KOhms:
 -do a check and repair the wiring between the pin AA/5B
 of the BMC2 (1HA2) and the cable 3HF2

 -disconnect the LOOP CONTROLLER (9240SI) from the BMC2
 connector

 -install the BMC2 (1HA2) (Ref. AMM TASK 36-11-34-400-001)

 -refer to Para. 4.B.
 . if the impedance is more than 3 KOhms:

 -disconnect the LOOP CONTROLLER (9240SI) from the BMC2
 connector

 -install the BMC2 (1HA2) (Ref. AMM TASK 36-11-34-400-001)

 -refer to Para. 4.B.

 B. Do the test given in para. 3.
 1 -EFF : ALL

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 Air Leak in the Left Wing with the APU in Operation
 1. Possible Causes_______________
 - ducts - seals
 2. Job Set-up Information______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R  AMM AMM AMM AMM AMM AMM AMM AMM AMM AMM AMM AMM  21-52-00-200-010 24-41-00-861-002 24-41-00-862-002 31-60-00-860-001 31-60-00-860-002 36-22-00-790-001 49-00-00-860-003 49-00-00-860-004 49-00-00-860-005 49-00-00-860-006 49-00-00-860-008 49-00-00-860-009  Hot-Air Leak-Check in the Air Conditioning BayEnergize the Aircraft Electrical Circuits from the External PowerDe-energize the Aircraft Electrical Circuits Supplied from the External PowerEIS Start ProcedureEIS Stop ProcedureLeak Check on all the Bleed Air Ducts APU Start by External Power (GTCP 36-300) APU Shutdown by External Power (GTCP 36-300)APU Start by External Power (APS 3200)APU Shutdown by External Power (APS 3200)APU Start by External Power (131-9(A))APU Shutdown by External Power (131-9(A))
 3. Fault Confirmation__________________
 A. Job Set-up
 (1) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
 (2) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. AMM TASK 31-60-00-860-001). 
R  B. Test 
R R R R R R  (1) Start the APU: - GTCP 36-300 (Ref. AMM TASK 49-00-00-860-003) or - APS 3200 (Ref. AMM TASK 49-00-00-860-005) or - 131-9(A) (Ref. AMM TASK 49-00-00-860-008).

 1 -EFF : ALL

-∞∞36-22-00∞∞∞∞∞∞∞∞∞∞Page A202
 --Aug 01/04 ---CES -

R R R (2) On the AIR COND panel 30VU, push the APU BLEED pushbutton switch (5HV) (the ON legend comes on). 
4. Fault Isolation_______________
 A. On the upper ECAM DU, if the AIR L WING LEAK warning comes into view: - do a leak test on the bleed air ducts (Ref. AMM TASK 36-22-00-790-001).
 (1) If there are leaks: - replace the defective ducts or seals as necessary.
 (2) If there is no leak: - do a hot-air leak check in the air conditioning bay (Ref. AMM TASK 21-52-00-200-010).
 (a) If there are cracks or damage on the ducts: - replace the defective ducts.
 (b) If there are leaks on the seals: - replace the defective seals.
 5. Close-up________ 
R  A. Put the aircraft back to its initial configuration. 
R R  (1) On the AIR COND panel 30VU, release the APU BLEED pushbutton switch (5HV) (the ON legend goes off). 
R R R R R R  (2) Stop the APU: - GTCP 36-300 (Ref. AMM TASK 49-00-00-860-004) or - APS 3200 (Ref. AMM TASK 49-00-00-860-006) or - 131-9(A) (Ref. AMM TASK 49-00-00-860-009). 
R R  (3) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002). 
R R  (4) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).

 1 -EFF : ALL

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 --Aug 01/04 ---CES -

R

 TASK 36-22-00-810-833
 Air Leak in the Right Wing with the APU in Operation
 1. Possible Causes_______________
 - ducts - seals
 2. Job Set-up Information______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R  AMM AMM AMM AMM AMM AMM AMM AMM AMM AMM AMM AMM  21-52-00-200-010 24-41-00-861-002 24-41-00-862-002 31-60-00-860-001 31-60-00-860-002 36-22-00-790-001 49-00-00-860-003 49-00-00-860-004 49-00-00-860-005 49-00-00-860-006 49-00-00-860-008 49-00-00-860-009  Hot-Air Leak-Check in the Air Conditioning BayEnergize the Aircraft Electrical Circuits from the External PowerDe-energize the Aircraft Electrical Circuits Supplied from the External PowerEIS Start ProcedureEIS Stop ProcedureLeak Check on all the Bleed Air Ducts APU Start by External Power (GTCP 36-300) APU Shutdown by External Power (GTCP 36-300)APU Start by External Power (APS 3200)APU Shutdown by External Power (APS 3200)APU Start by External Power (131-9(A))APU Shutdown by External Power (131-9(A))
　
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