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时间:2011-03-29 14:34来源:蓝天飞行翻译 作者:航空
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 NOTE 3 : For the trouble shooting, do the procedure for the plug which is shown on the fault message and not the channel which is given at the end of the post flight report.
 - do a check for open or short to ground of the harness J9 between the ECU (4000KS) and the control alternator pins J9/4, 5, 13, 14, 15 to pins J9/2, 3, 4, 5 (Ref. ASM 73-25/18).
 F 『 EEFF : ALL E ∞∞77-10-00∞∞∞∞∞∞∞∞∞∞Page 201
 E E May 01/05 E E ECES
E F 『 E C F M E E E E 56 E E E (1) If the wiring is not correct:


 - repair the above wiring.
 (2) If the wiring is correct:
 - disconnect the harness J9 from the ECU (4000KS) and do a check of the ECU cable resistance between: . pins 5 and 13 (< 1 Ohm) . pins 5 and 14 (< 1 Ohm) . pins 5 and 15 (< 1 Ohm) . pins 5 and 4 (> 10 Megohms) . pin 5 and the ground (> 10 Megohms).
 (a) If the resistance values are in the specified limits:

 - replace the ECU (4000KS) (Ref. AMM TASK 73-21-60-000-001) and (Ref. AMM TASK 73-21-60-400-001).

 (b) If the resistance values are out of the specified limits:


 - disconnect the harness J9 from the control alternator and do a check of the alternator resistance between: . pins 2 and 5 (< 1 Ohm) . pins 3 and 5 (< 1 Ohm) . pins 4 and 5 (< 1 Ohm) . pin 5 and the ground (> 10 Megohms).
 1 If the resistance values are in the specified limits:
_
 - replace the harness J9 (Ref. AMM TASK 73-21-50-000-042) and (Ref. AMM TASK 73-21-50-400-042).
 2 If the resistance values are out of the specified limits:
_
 - replace the control alternator (Ref. AMM TASK 73-21-30-000-001) and (Ref. AMM TASK 73-21-30-400-001).
 F 『R EEFF : 001-049, 051-099, 101-105, 151-154, E ∞∞77-10-00∞∞∞∞∞∞∞∞∞∞Page 202
 E E201-207, May 01/05 E E ECES
E TASK 77-10-00-810-810

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


 Loss of the ECU Cross Channel on Engine 2
 1. Possible Causes
_______________
 - harness J9

 - ECU (4000KS)

 - control alternator


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 73-21-30-000-001 Removal of the Control Alternator AMM 73-21-30-400-001 Installation of the Control Alternator AMM 73-21-50-000-042 Removal of the HJ9 Harness AMM 73-21-50-400-042 Installation of the HJ9 Harness 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) ASM 73-25/18
 3. Fault Confirmation
__________________
 A. Not Applicable
 4. Fault Isolation
_______________
 A. If the test gives the maintenance message ALT, ECU, J9:
 NOTE 1 : In the usual operating condition, a fault of the harness J9
 is detected with the test of the channel A.
 NOTE 2 : When a cross channel fault occurs, the harness fault is
 detected during the test on the opposite channel.

 NOTE 3 : For the trouble shooting, do the procedure for the plug which is shown on the fault message and not the channel which is given at the end of the post flight report.
 - do a check for open or short to ground of the harness J9 between the ECU (4000KS) and the control alternator pins J9/4, 5, 13, 14, 15 to pins J9/2, 3, 4, 5 (Ref. ASM 73-25/18).
 (1) If the wiring is not correct:
 - repair the above wiring.
 F 『R EEFF : 001-049, 051-099, 101-105, 151-154, E ∞∞77-10-00∞∞∞∞∞∞∞∞∞∞Page 203
 E E201-207, May 01/05 E E ECES
E F 『 E C F M E E E E 56 E E E (2) If the wiring is correct:


 - disconnect the harness J9 from the ECU (4000KS) and do a check of the ECU cable resistance between: . pins 5 and 13 (< 1 Ohm) . pins 5 and 14 (< 1 Ohm) . pins 5 and 15 (< 1 Ohm) . pins 5 and 4 (> 10 Megohms) . pin 5 and the ground (> 10 Megohms).
 (a) If the resistance values are in the specified limits:

 - replace the ECU (4000KS) (Ref. AMM TASK 73-21-60-000-001) and (Ref. AMM TASK 73-21-60-400-001).

 (b) If the resistance values are out of the specified limits:


 - disconnect the harness J9 from the control alternator and do a check of the alternator resistance between: . pins 2 and 5 (< 1 Ohm) . pins 3 and 5 (< 1 Ohm) . pins 4 and 5 (< 1 Ohm) . pin 5 and the ground (> 10 Megohms).
 
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