F 『 E C F M E E E E 56 E E E (2) If the fault continues:
- do a check and repair the wiring from the EIU 2 (1KS2) pins AB/5H, 5K to the first terminal block (Ref. ASM 73-25/06).
(3) If the fault continues:
- replace the ECU (4000KS) (Ref. AMM TASK 73-21-60-000-001) and (Ref. AMM TASK 73-21-60-400-001).
B. Do the test given in Para. 3.
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Loss of the Channel B on the Engine 1
1. Possible Causes
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- EIU-1 (1KS1)
- ECU (4000KS)
- harness J2
- aircraft wiring
- C/B-ENGINE/ENG 1/FADEC B/AND EIU 1 (4KS1)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 73-21-60-000-001 Removal of the Electronic Control Unit (ECU)(4000KS) AMM 73-21-60-400-001 Installation of the Electronic Control Unit (ECU)(4000KS) 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 73-29-00-710-040 Operational Test of the FADEC on the ground (with
Engine Motoring) ASM 73-25/05 ASM 73-25/08
3. Fault Confirmation
__________________
A. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
121VU ENGINE/ENG1/FADEC B/AND EIU 1 4KS1 R41
B. Test
(1) If the circuit breaker (4KS1) is open, refer to Para. 4.A.(2).
(2) Do the operational test of the FADEC 1A and 1B on the ground (with engine motoring) (Ref. AMM TASK 73-29-00-710-040).
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4. Fault Isolation
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A. If the test gives the maintenance message ECU, EIU 28V, J2:
- do a check of the status of the circuit breaker (4KS1).
(1) If the circuit breaker is closed:
- disconnect the connector J2 from the ECU (4000KS) and do a check for 28VDC at pin J2/13 with the FADEC GND PWR pushbutton switch released (the ON legend is on).
(a) If there is 28VDC:
- replace the ECU (4000KS) (Ref. AMM TASK 73-21-60-000-001) and (Ref. AMM TASK 73-21-60-400-001).
(b) If there is no 28VDC:
- do a check for 28VDC at EIU 1 (1KS1) pin AC/9 (Ref. ASM 73-25/05).
1 If there is 28VDC:
_
- do a check for open or short to ground at the harness J2 between the EIU 1 (1KS1) and the ECU (4000KS), pin AC/2 to pin J2/13. Replace the harness J2 if necessary.
a If the fault continues:
_
- make sure that there is no ground signal at EIU 1 (1KS1) pin AA/5B (Ref. ASM 73-25/08).
b 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).
2 If there is no 28VDC:
_
- do a check for open or short to ground at the aircraft wiring between the circuit breaker (4KS1) and EIU 1 (1KS1) pin AC/9.
a If there is a short to ground:
_ - repair the above wiring.
b If there is no short to ground:
_ - replace the C/B-ENGINE/ENG 1/FADEC B/AND EIU 1 (4KS1).
3 Make sure that 28VDC supplies the BAT bus (Ref. ASM 73-25/05).
_
(2) If the circuit breaker (4KS1) is open:
- close the circuit breaker.
(a) If the circuit breaker trips:
- replace the EIU-1 (1KS1) (Ref. AMM TASK 73-25-34-000-040) and (Ref. AMM TASK 73-25-34-400-040)
- replace the ECU (4000KS) (Ref. AMM TASK 73-21-60-000-001) and (Ref. AMM TASK 73-21-60-400-001).
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F 『 E C F M E E E E 56 E E E (b) If the fault continues:
- do a check for a short to ground at the harness J2 between the EIU 1 (1KS1) and the ECU (4000KS), pin AC/2 to pin J2/13. 中國航空網(wǎng) www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) 發(fā)動(dòng)機(jī)燃油和控制 1(78)
