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时间:2011-03-28 18:37来源:蓝天飞行翻译 作者:航空
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 * repair the wiring which has no continuity.
 (3) If the fault continues:
 - do a check for 28VDC at pin AC/3 of the DMC3 (1WT3) (Ref. ASM 31-61/02).
 (a) If there is 28VDC:

 - replace the DMC-3 (1WT3) (Ref. AMM TASK 31-63-34-000-001) and (Ref. AMM TASK 31-63-34-400-001).

 (b) If there is no 28VDC:


 - do a check for a ground signal at pin AC/11 of the DMC3 (1WT3) (Ref. ASM 31-61/02).
 1_ If there is no ground signal:
 - repair the wiring from DMC3 (1WT3) pin AC/11 to the ground
 terminal.

 2 If there is a ground signal:
_

 - do a check of the wiring from DMC3 (1WT3) pin AC/3 to the circuit breaker (21WT3) (Ref. ASM 31-61/02).
 a If there is no continuity:
_

 - repair the wiring. b If there is continuity:
_ - replace the C/B-EIS/DMC3/SWTG (21WT3).

 (4) If the fault continues:
 - do a check for a ground signal at pin AB/8H, 4C of the DMC1 (1WT1).
 (a) If there is no ground signal:
 - do a check for a ground signal at pin AA/2 of the EIS DMC selector switch (18WT) (Ref. ASM 31-68/02).
 1 If there is no ground signal:
_

 - replace the SEL SW-EIS DMC (18WT). 2 If there is a ground signal:
_

 - do a check of the wiring from EIS DMC selector switch (18WT) pin 2 to DMC1 (1WT1) pin AB/8H, 4C.
 a If there is no continuity:
_

 - repair the wiring. b If there is continuity:
_

 - replace the DMC-1 (1WT1) (Ref. AMM TASK 31-63-34-000-001) (Ref. AMM TASK 31-63-34-400-001).
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-149, 151-199, ∞∞31-63-82∞∞∞∞∞∞∞∞∞∞Page 213
 201-299, 301-399, Aug 01/05 CES

 

 (b) If there is a ground signal:
 - do a check for a ground signal at pin AB/4C of the DMC3 (1WT3) (Ref. ASM 31-68/02).
 1 If there is no ground signal:
_

 - do a check of the wiring from DMC3 (1WT3) pin AB/4C to the first terminal block (Ref. ASM 31-68/02).
 a If there is no continuity:
_

 - repair the wiring.
 b If there is continuity:

_

 - replace the DMC-3 (1WT3) (Ref. AMM TASK 31-63-34-000-001) and (Ref. AMM TASK 31-63-34-400-001).
 C. Do the EIS start procedure (CAPT ND only) (Ref. AMM TASK 31-60-00-860-001) and make sure that the CAPT ND comes on.
 5. Close-up
________
 A. Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-149, 151-199, ∞∞31-63-82∞∞∞∞∞∞∞∞∞∞Page 214
 201-299, 301-399, Aug 01/05 CES

 

 Loss of the Upper ECAM DU
 1. Possible Causes
_______________
 - DU-ECAM, UPPER (4WT1)

 - CTL PNL-ECAM (6WT)

 - DMC-3 (1WT3)

 - DMC-1 (1WT1)

 - wiring

 - C/B-EIS/ECAM DU/UPPER/SPLY (13WT1)

 - C/B-EIS/ECAM DU/UPPER/SWTG (24WT1)

 - RELAY-BUS1 TO ESS BUS SWTG, DMC3 (26WT)

 - C/B-EIS/DMC3/SWTG (21WT3)

 - SEL SW-EIS DMC (18WT)


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 31-60-00-860-001 EIS Start Procedure AMM 31-60-00-860-002 EIS Stop Procedure AMM 31-61-12-000-001 Removal of the ECAM Control Panel (6WT) AMM 31-61-12-400-001 Installation of the ECAM Control Panel (6WT) AMM 31-63-22-000-001 Removal of the Display Unit
 (2WT1,2WT2,3WT1,3WT2,4WT1,4WT2) AMM 31-63-22-400-001 Installation of the Display Unit
 (2WT1,2WT2,3WT1,3WT2,4WT1,4WT2) AMM 31-63-34-000-001 Removal of the DMC (1WT1,1WT2,1WT3) AMM 31-63-34-400-001 Installation of the DMC (1WT1,1WT2,1WT3) ASM 31-61/02 ASM 31-68/01 ASM 31-68/02
 3. Fault Confirmation
__________________
 A. Job Set-Up Do the EIS start procedure (upper ECAM DU only) (Ref. AMM TASK 31-60-00-860-001).
 B. Test
 Make sure that the upper ECAM DU stays off.

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-149, 151-199, ∞∞31-63-82∞∞∞∞∞∞∞∞∞∞Page 215
 201-299, 301-399, Aug 01/05 CES

 

 4. Fault Isolation
 
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