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时间:2011-03-29 09:37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

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 A. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU ENGINE/1/FADEC A/AND EIU 1 2KS1 A04 49VU ENGINE/1 AND 2/IGN/SYS A 1JH A03 121VU ENGINE/IGN/ENG1/SYS B 3JH1 P41 121VU ENGINE/IGN/ENG1/SYS A BAT 2JH1 P39 121VU ENGINE/ENG1/FADEC B/AND EIU 1 4KS1 R41
 B. Aircraft Maintenance Configuration
 NOTE : If the circuit breakers 2KS1, 4KS1 are opened, stop for 5 minutes
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 before you start the procedure.

 C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU ENGINE/ENG1 AND 2 FIRE EXTIG/BTL1/SQUIB/B 2WE1 Q44 121VU ENGINE/ENG1 AND 2 FIRE EXTIG/BTL1/SQUIB/A 1WE1 Q43 121VU ENGINE/ENG1 AND 2 FIRE EXTIG/BTL2/SQUIB/B 2WE2 Q42 121VU ENGINE/ENG1 AND 2 FIRE EXTIG/BTL2/SQUIB/A 1WE2 Q41
 D. Job Set-Up
 (1) On the panel 115VU, make sure that:

 (a) The ENG/MODE/CRANK/AUTO IGN/IGN selector switch is set to NORM.

 (b) The ENG MASTER 1 switch is set to OFF.

 

 (2) On the panel 22VU, make sure that the ENG/MAN START/1 pushbutton switch is released.

 (3) Do the EIS start procedure (Ref. AMM TASK 31-60-00-860-001).


 E. Test
 (1) On the panel 50VU, release the ENG/FADEC GND PWR/1 pushbutton switch (ON legend on).
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 A. If the test does not show XX on the upper ECAM DU, but shows engine 1 parameters:
 (1) Do a check and repair the wiring between the ENG/MODE/CRANK/AUTO IGN/IGN selector switch (6KS) and the EIU 1 (1KS1), (Ref. ASM 73-25/08).

 (2) If the fault continues:

 - replace the SEL SW-ENG/MODE/CRANK/AUTO IGN/IGN (6KS).

 (3) If the fault continues:


 - replace the EIU-1 (1KS1), (Ref. AMM TASK 73-25-34-000-040) and (Ref. AMM TASK 73-25-34-400-040).
 B. If the test does not show engine 1 parameters on the upper ECAM DU, but shows XX:
 (1) Make sure that there is 28VDC at the pin 9 of the connector 1KS1-AC (Ref. ASM 73-25/05).

 (a) If there is no 28VDC:

 - do a check and repair the wiring between the circuit breaker 4KS1 and the EIU 1 (1KS1).

 (b) If there is 28VDC:


 - do a check and repair the wiring between the pin 2 of the connector 1KS1-AC and the pin 13 of the connector 4000KS-J2.

 (2) If the fault continues:

 - make sure that there is 28VDC at the pin 11 of the connector 1KS1-AC (Ref. ASM 73-25/05).
 (a) If there is no 28VDC:

 - do a check and repair the wiring between the circuit breaker 2KS1 and the EIU 1 (1KS1).

 (b) If there is 28VDC:


 - do a check and repair the wiring between the pin 7 of the connector 1KS1-AC and the pin 13 of the connector 4000KS-J4.

 (3) If the fault continues:


 - replace the EIU-1 (1KS1), (Ref. AMM TASK 73-25-34-000-040) and (Ref. AMM TASK 73-25-34-400-040).
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 C. Test
 (1) Do the operational test of the Engine Interface Unit (Ref. AMM TASK 73-25-34-710-043).

 (2) Make sure that all engine 1 parameters are shown on the upper ECAM DU when you start the engine again (Ref. AMM TASK 71-00-00-710-003) or (Ref. AMM TASK 71-00-00-710-004).


 5. Close-up________
 A. Put the aircraft back to its initial configuration.
 (1) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
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 All engine 2 parameters are XX on the upper ECAM DU on ground at starting.
 1. Possible Causes
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