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时间:2011-03-29 09:37来源:蓝天飞行翻译 作者:航空
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 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 non Motoring)
 ASM 73-25/06
 3. Fault Confirmation__________________
 A. Test
 (1) Do the operational test of the FADEC 1B on the ground (with engine non motoring) (Ref. AMM TASK 73-29-00-710-040).
 4. Fault Isolation_______________
 A. If the test gives the maintenance message CFDIU, EIU (155), J3*:
 - do a check for open or short to ground at pins AB/5A, 5C to pins J3/22, 23 of the harness J3 from EIU-1 (1KS1) to ECU (4000KS) (Ref. ASM 73-25/06).
 (1) If the wiring is not correct:

 - repair the above harness J3.

 (2) If the wiring is correct:


 - replace the EIU-1 (1KS1) (Ref. AMM TASK 73-25-34-000-040) and (Ref. AMM TASK 73-25-34-400-040).
 F 『 EEFF : ALL E ∞∞73-25-00∞∞∞∞∞∞∞∞∞∞Page A238
 E E Aug 01/05 ERE
ECES  F 『 E C F M E E E E 56 E E E (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.A.
 F 『 EEFF : ALL E ∞∞73-25-00∞∞∞∞∞∞∞∞∞∞Page A239
 E E Aug 01/05 ERE
ECES


 F 『
 E C F M E
 E E
 E 56 E
 E E

 

 TASK 73-25-00-810-943
 Loss of Data on the ARINC Bus from the EIU to the Fadec on Engine 2
 1. Possible Causes
_______________
 - EIU-2 (1KS2)

 - harness J3 from EIU-2 (1KS2) to ECU (4000KS)

 - ECU (4000KS)


 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 non Motoring) ASM 73-25/06
 3. Fault Confirmation
__________________
 A. Do the operational test of the FADEC 2B on the ground (with engine non motoring) (Ref. AMM TASK 73-29-00-710-040).
 4. Fault Isolation
_______________
 A. If the test gives the maintenance message CFDIU, EIU (155), J3*:
 - do a check for open or short to ground at pins AB/5A, 5C to pins J3/22, 23 of the harness J3 from EIU-2 (1KS2) to ECU (4000KS) (Ref. ASM 73-25/06).
 (1) If the wiring is not correct:

 - repair the above harness J3.

 (2) If the wiring is correct:

 - replace the EIU-2 (1KS2) (Ref. AMM TASK 73-25-34-000-040) and (Ref. AMM TASK 73-25-34-400-040).

 (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).
 F 『 EEFF : ALL E ∞∞73-25-00∞∞∞∞∞∞∞∞∞∞Page A240
 E E Aug 01/05 E
RE ECES
E F 『 E C F M E E E E 56 E E E

 

 

 B. Do the test given in Para. 3.A.
 F 『 EEFF : ALL E ∞∞73-25-00∞∞∞∞∞∞∞∞∞∞Page A241
 E E Aug 01/05 ERE
ECES  TASK 73-25-00-810-946


 F  『
 E  C F M  E
 E  E
 E  56  E
 E  E

 

 Loss of the 28VDC Power Supply of the ECU on the Engine 1
 1. Possible Causes
_______________
 - EIU-1 (1KS1)

 - ECU (4000KS)

 - aircraft wiring

 - C/B-ENGINE/ENG 1/FADEC B/AND EIU 1 (4KS1)

 - harness J2


 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
 
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