- EIU-2 (1KS2)
- wiring between the ENG/MODE/CRANK/AUTO IGN/IGN selector switch (6KS) and the EIU 2 (1KS2)
- wiring between the circuit breaker 2KS2 and the EIU 2 (1KS2)
- wiring between the pin 7 of the connector 1KS2-AC and the pin 13 of the connector 4000KS-J1
- wiring between the circuit breaker 4KS2 and the EIU 2 (1KS2)
- wiring between the pin 2 of the connector 1KS2-AC and the pin 13 of the connector 4000KS-J2
2. Job Set-up Information
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A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 31-60-00-860-001 EIS Start Procedure AMM 31-60-00-860-002 EIS Stop Procedure AMM 71-00-00-710-003 Engine Automatic Start AMM 71-00-00-710-004 Engine Manual Start AMM 73-25-34-000-040 Removal of the Engine Interface Unit (EIU)
(1KS1,1KS2) AMM 73-25-34-400-040 Installation of the Engine Interface Unit (EIU)
(1KS1,1KS2) AMM 73-25-34-710-043 Operational Test of the Engine Interface Unit ASM 73-25/05 ASM 73-25/08
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A. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU ENGINE/2/FADEC A/AND EIU 2 2KS2 A05 49VU ENGINE/1 AND 2/IGN/SYS A 1JH A03 121VU ENGINE/IGN/ENG2/SYS B 3JH2 P42 121VU ENGINE/IGN/ENG2/SYS A BAT 2JH2 P40 121VU ENGINE/ENG2/FADEC B 4KS2 Q40
B. Aircraft Maintenance Configuration
NOTE : If the circuit breakers 2KS2, 4KS2 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 2 switch is set to OFF.
(2) On the panel 22VU, make sure that the ENG/MAN START/2 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/2 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 2 parameters:
(1) Do a check and repair the wiring between the ENG/MODE/CRANK/AUTO IGN/IGN selector switch (6KS) and the EIU 2 (1KS2), (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-2 (1KS2), (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 2 parameters on the upper ECAM DU, but shows XX:
(1) Make sure that there is 28VDC at the pin 11 of the connector 1KS2-AC (Ref. ASM 73-25/05).
(a) If there is no 28VDC:
- do a check and repair the wiring between the circuit breaker 2KS2 and the EIU 2 (1KS2).
(b) If there is 28VDC:
- do a check and repair the wiring between the pin 7 of the connector 1KS2-AC and the pin 13 of the connector 4000KS-J1.
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本文链接地址：A320 Trouble Shooting Manual 排故手册 发动机燃油和控制 2(85)
