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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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 -wiring
 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 (1HA1, 1HA2)
 AMM 36-11-34-400-001 Installation of the BMC (1HA1, 1HA2)
 ASM 36-11/03

 3. Fault Confirmation

__________________
 A. Test
 (1) Do the BITE test of the BMC2 (Ref. AMM TASK 36-11-00-740-001).
 4. Fault Isolation
_______________
 A. If the test gives the maintenance message:
 NO DATA FROM BMC1

 -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 and repair the wiring for the ARINC 429 OUTPUT BUS from the BMC1 (1HA1) AA/10C, 11C to the BMC 2 (1HA2) AA/1D, 2D, (Ref. ASM 36-11/03).
 B. Do the test given in para. 3.
 1
 -EFF : ALL


-∞∞36-11-00∞∞∞∞∞∞∞∞∞∞Page A211
 --Feb 01/05R ---CES -

 


 Loss of the BMC2
 1. Possible Causes
_______________
 -BMC-2 (1HA2)
 -wiring
 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 (1HA1, 1HA2)
 AMM 36-11-34-400-001 Installation of the BMC (1HA1, 1HA2)
 ASM 36-11/03

 3. Fault Confirmation

__________________
 A. Test
 (1) Do the BITE test of the BMC1 (Ref. AMM TASK 36-11-00-740-001).
 4. Fault Isolation
_______________
 A. If the test gives the maintenance message:
 NO DATA FROM BMC2

 -replace the BMC-2 (1HA2) (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 and repair the wiring for the ARINC 429 OUTPUT BUS from the BMC2 (1HA2) AA/10C, 11C to the BMC1 (1HA1) AA/1D, 2D, (Ref. ASM 36-11/03).
 B. Do the test given in para. 3.
 1
 -EFF : ALL


-∞∞36-11-00∞∞∞∞∞∞∞∞∞∞Page A212
 --Feb 01/05R ---CES -

 


 Loss of the Power Supply of the Bleed Pressure-Regulator Valve of the Engine 1
 1. Possible Causes
_______________
 -BMC-1 (1HA1)

 -
wiring between the BMC1 pin AB/1B and the ground terminal

 -
wiring between the BMC1 pin AA/8A and the circuit breaker (3HA1)


 -C/B-BLEED VLV ENG 1 (3HA1)
 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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. Not applicable.

 4. Fault Isolation
_______________

 A. Table of the circuit breakers used in this procedure:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU AIR BLEED/ENG 1/CTL 3HA1 D12
 B. If the fault symptom is identified by the maintenance message CHECK PRESS REG V PWR SPLY:
 -do a check of the status of the circuit breaker (3HA1).
 (1) If the circuit breaker (3HA1) is closed:
 -do a check for 28VDC at pin AA/8A of the BMC1 (1HA1) (Ref. ASM 36-11/01).
 (a) If there is 28VDC:
 -replace the BMC-1 (1HA1) (Ref. AMM TASK 36-11-34-000-001) and (Ref. AMM TASK 36-11-34-400-001).
 1
 -EFF : ALL


-∞∞36-11-00∞∞∞∞∞∞∞∞∞∞Page A213
 --Feb 01/05R ---CES -


 (b) If there is no 28VDC:
 -do a check for ground at pin AB/1B of the BMC1 (1HA1).
 1_ If there is no ground:
 - repair the wiring between the BMC1 pin AB/1B and the ground
 
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