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时间:2011-03-29 14:34来源:蓝天飞行翻译 作者:航空
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121VU ENGINE/ENG1 AND 2/EVMU 1EV R44
 B. Do the operational test of the Central Warning Systems (SDAC) (Ref. AMM TASK 31-50-00-710-001).
 4. Fault Isolation
_______________
 A. If the test gives the maintenance message SDAC1 : NO DATA FROM EVMU:
 - replace the EVMU (2EV) (Ref. AMM TASK 77-32-34-000-042) and (Ref. AMM TASK 77-32-34-400-042).
 (1) If the fault continues:
 - do a check and repair the wiring from the EVMU (2EV) pins AA/13A, 13C to the first terminal block (Ref. ASM 77-32/02).
 B. Do the test given in Para. 3.
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 TASK 77-30-00-810-832


 Loss of the EVMU Output Bus
 1. Possible Causes
_______________
 - EVMU (2EV)

 - wiring from the EVMU (2EV) pins AA/13A, 13C to the first terminal block


 2. Job Set-up Information
______________________
 A. Referenced Information
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REFERENCE DESIGNATION
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AMM 31-50-00-710-001 Ground Scanning of the Central Warning System AMM 77-32-34-000-042 Removal of the Engine Vibration Monitoring Unit (EVMU) AMM 77-32-34-400-042 Installation of the Engine Vibration Monitoring Unit (EVMU) ASM 77-32/02
 3. Fault Confirmation
__________________
 A. Make sure that this(these) circuit breaker(s) is(are) closed:
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PANEL DESIGNATION IDENT. LOCATION
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121VU ENGINE/ENG1 AND 2/EVMU 1EV R44
 B. Do the operational test of the Central Warning Systems (SDAC) (Ref. AMM TASK 31-50-00-710-001).
 4. Fault Isolation
_______________
 A. If the test gives the maintenance message SDAC2 : NO DATA FROM EVMU:
 - replace the EVMU (2EV) (Ref. AMM TASK 77-32-34-000-042) and (Ref. AMM TASK 77-32-34-400-042).
 (1) If the fault continues:
 - do a check and repair the wiring from the EVMU (2EV) pins AA/13A, 13C to the first terminal block (Ref. ASM 77-32/02).
 B. Do the test given in Para. 3.
 F 『 EEFF : ALL E ∞∞77-30-00∞∞∞∞∞∞∞∞∞∞Page 225
 E E Feb 01/98 E E ECES
E

 

 


 
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