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时间:2011-03-28 23:25来源:蓝天飞行翻译 作者:航空
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 -disconnect the LOOP CONTROLLER (9240SI) from the BMC2 connector
 -do a visual inspection of the sensing elements and cables on the engine 2 pylon loop.
 (a)
 If a sensing element or cable is damaged:

 -replace the sensing element or cable (Ref. AMM TASK 36-22-15-000-001) and (Ref. AMM TASK 36-22-15-400-001)
 -disconnect the LOOP CONTROLLER (9240SI) from the BMC2 connector
 -install the BMC2 (Ref. AMM TASK 36-11-34-400-001)
 -refer to Para. 4.C.

 (b)
 If no sensing element is damaged:


 -disconnect the connector between the cable 2HF2 and the sensing element 1HF2
 -connect the LOOP CONTROLLER (9240SI) between the connector 1HA2-AA/6B and the ground
 -do a check of the impedance read on the LOOP CONTROLLER (9240SI).
 1_ If the impedance is less than 3 KOhms:
 - replace the CABLE-CONNECTING, ENG 2 PYLON (2HF2) (Ref. AMM
 TASK 36-22-15-000-001) and (Ref. AMM TASK 36-22-15-400-001)
 - do a check of the impedance read on the LOOP CONTROLLER
 (9240SI).

 1
 -EFF : ALL


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 2
_

 a If the impedance is less than 3 KOhms:
_
 -do a check and repair the wiring between the pin 6B of the BMC2 connector (1HA2-AA) and the cable 2HF2
 -connect all the cables or connectors disconnected
 -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.C.
 b If the impedance is more than 3 KOhms:
_ -connect all the cables or connectors disconnected
 -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.C.
If the impedance is more than 3 KOhms:
 -disconnect the connector between the cable 3HF2 and the sensing element 1HF2
 -connect the connector between the cable 2HF2 and the sensing element 1HF2
 -do a check of the impedance read on the LOOP CONTROLLER (9240SI).
 a If the impedance is less than 3 KOhms:
_ -replace the SNSG ELEM-OVHT, ENG 2 PYLON (1HF2)
 -disconnect the LOOP CONTROLLER (9240SI) from the BMC2 connector
 -install the BMC-2 (1HA2) which is removed (Ref. AMM TASK 36-11-34-400-001)
 -refer to Para. 4.C.
 b If the impedance is more than 3 KOhms:
_ -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 5B of the BMC2 connector (1HA2-AA) 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.C.
 . 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.C.
 1
 -EFF : ALL


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 --Feb 01/03R ---CES -

 

 C. After the subsequent flight, make sure that the fault does not continue.

 1
 -EFF : ALL


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 --Feb 01/03R ---CES -

 

 Air Leak from the APU in the Aft Cargo Compartment
 1. Possible Causes
_______________
 -ducts
 -seals
 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
R AMM 36-12-00-790-001 Leak Test of the APU Bleed-Air Supply-System
 3. Fault Confirmation
__________________
 A. Test
 (1) Do the Leak Test of the APU Bleed Air Supply System (Ref. AMM TASK 36-12-00-790-001).
 4. Fault Isolation
_______________
 A. If the cause of the leak is a cracked/damaged duct:
 -repair or replace the defective ducts.
 B. If the cause of the leak is a defective seal:
 -replace the defective seals.
 C. After the subsequent flight, make sure that the fault does not continue.
 
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