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时间:2011-03-28 23:25来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 -
wiring between pin A/2 of the bleed regulated-pressure transducer (8HA1) and the ground terminal

 -
wiring from the bleed regulated-pressure transducer (8HA1) pins A/3 and A/4 to the BMC1 (1HA1) pins AA/12B and AA/11B

 -
wiring from pin A/1 of the bleed regulated-pressure transducer (8HA1) to the circuit breaker (2HA1)


 -C/B-BMC 1 (2HA1)
 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 36-11-16-000-001 Removal of the Bleed Regulated Pressure Transducer (8HA1,8HA2) AMM 36-11-16-400-001 Installation of the Bleed Regulated Pressure
 Transducer (8HA1,8HA2) AMM 36-11-34-000-001 Removal of the BMC (1HA1, 1HA2) AMM 36-11-34-400-001 Installation of the BMC (1HA1, 1HA2) ASM 36-11/01
 3. Fault Confirmation
__________________
 A. Test.
 (1) Not applicable, the fault is evident.
 4. Fault Isolation
_______________
 A. Table of the circuit breakers used in this procedure:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU AIR BLEED/ENG 1/MONG 2HA1 D11
 1
 -EFF : ALL


-∞∞36-11-00∞∞∞∞∞∞∞∞∞∞Page 243
 --Feb 01/05R ---CES -


 B. If the fault symptom is identified by the maintenance message: REG-PRESS XDCR 8HA1
 -do a check of the status of the circuit breaker (2HA1)
 (1) If the circuit breaker is closed
 -do a check for 28VDC at pin A/1 of the bleed regulated-pressure transducer (8HA1) (Ref. ASM 36-11/01).
 (a) If there is no 28VDC
 -do a check of the wiring between pin A/1 of the bleed regulated-pressure transducer (8HA1) and the circuit breaker (2HA1).
 1 If there is no continuity:
_ -repair the above wiring.
 2 If there is continuity:
_ -replace the circuit breaker (2HA1).
 (b) If there is 28VDC
 -do a check for ground at pin A/2 of the bleed regulated-pressure transducer (8HA1).
 1 If there is no ground signal:
_
 -repair the wiring between pin A/2 of the bleed regulated-pressure transducer (8HA1) and the ground terminal.
 2 If there is a ground signal:
_
 -replace the XDCR-BLEED REGULATED PRESS, ENG 1 (8HA1) (Ref. AMM TASK 36-11-16-000-001) and (Ref. AMM TASK 36-11-16-400-001).
 a If the fault continues:
_
 -do a check and repair the wiring from the bleed regulated-pressure transducer (8HA1) pins A/3 and A/4 to the BMC1 (1HA1) pins AA/12B and AA/11B (Ref. ASM 36-11/01)
 (2) If the circuit breaker is open
 -close the circuit breaker.
 (a) If the circuit breaker trips
 -replace the BMC-1 (1HA1) (Ref. AMM TASK 36-11-34-000-001) and (Ref. AMM TASK 36-11-34-400-001).
 1_ If the fault continues:
 - do a check for short to ground on the wiring from pin A/1 of
 the bleed regulated-pressure transducer (8HA1) to the
 circuit breaker (2HA1).

 1
 -EFF : ALL


-∞∞36-11-00∞∞∞∞∞∞∞∞∞∞Page 244

 --Feb 01/05R ---CES -

 

 a If there is a short to ground:
_
 -repair the above wiring b If there is no short to ground:
_ -replace the C/B-BMC 1 (2HA1).
 C. After the subsequent flight, make sure that the fault does not continue.
 1
 -EFF : ALL


-∞∞36-11-00∞∞∞∞∞∞∞∞∞∞Page 245
 --Feb 01/05R ---CES -


 Loss of the Bleed Regulated-Pressure Transducer of the Engine 2
 1. Possible Causes
_______________
 -XDCR-BLEED REGULATED PRESS, ENG 2 (8HA2)
 -BMC-2 (1HA2)
 -
wiring between pin A/1 of the bleed regulated-pressure transducer (8HA2) and the circuit breaker (2HA2)

 -
wiring between pin A/2 of the bleed regulated-pressure transducer (8HA2) and the ground terminal

 -
wiring from the bleed regulated-pressure transducer (8HA2) pins A/3 and A/4 to the BMC2 (1HA2) pins AA/12B and AA/11B

 -
wiring from pin A/1 of the bleed regulated-pressure transducer (8HA2) to the circuit breaker (2HA2)


 -C/B-BMC 2 (2HA2)
 2. Job Set-up Information
______________________
 A. Referenced Information
 
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