(1KS1,1KS2)
AMM 73-25-34-710-043 Operational Test of the Engine Interface Unit
ASM 73-25/08
3. Fault Confirmation
__________________
A. Test
(1) Make sure that the engine 2 shutdown time was of 5 minutes minimum.
(2) Do the operational test of the Engine Interface Unit (Ref. AMM TASK 73-25-34-710-043).
4. Fault Isolation
_______________
A. If the test gives the maintenance message 115VU (MASTER LEVER 2SW):
- do a check and repair the wiring between the ENG/MASTER CTL switch (2KC) and the EIU 2 (1KS2), (Ref. ASM 73-25/08).
(1) If the fault continues:
(a) Replace the CTL SW - ENG/MASTER 2 (2KS).
(b) Do the operational test of the Engine Interface Unit (Ref. AMM TASK 73-25-34-710-040).
F 『 EEFF : ALL E ∞∞73-29-00∞∞∞∞∞∞∞∞∞∞Page 211
E E Feb 01/98 E E ECES
E F 『 E C F M E E E E 56 E E E (2) 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 gives NO FAILURE message:
- replace the EIU-2 (1KS2), (Ref. AMM TASK 73-25-34-000-040) and (Ref. AMM TASK 73-25-34-400-040).
F 『 EEFF : ALL E ∞∞73-29-00∞∞∞∞∞∞∞∞∞∞Page 212
E E Feb 01/98 E E ECES
E
F 『
E C F M E
E E
E 56 E
E E
TASK 73-29-00-810-806
All engine 1 parameters are XX on the upper ECAM DU on the ground with the
FADEC GND PWR pushbutton switch set to ON.
1. Possible Causes
_______________
- wiring between the FADEC GND PWR pushbutton switch (7KS1) and the EIU 1 (1KS1)
- P/BSW-ENG/FADEC GND PWR/1 (7KS1)
2. Job Set-up Information
______________________
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 73-21-60-720-040 Functional Test of the Electronic Control Unit (ECU) ASM 73-25/08
3. Fault Confirmation
__________________
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
____
before you start the procedure.
F 『 EEFF : ALL E ∞∞73-29-00∞∞∞∞∞∞∞∞∞∞Page 213
E E Feb 01/98 E E ECES
E
F 『
E C F M E
E E
E 56 E
E E
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). 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 發動機燃油和控制 2(87)
