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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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No specific  bristle brush
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. CP2011  * stoddard solvent (Ref. 70-30-00)
 C. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 73-21-50-000-043 Removal of the HJ10 Harness AMM 73-21-50-210-002 Visual Inspection of the Wiring Harnesses AMM 73-21-50-400-043 Installation of the HJ10 Harness AMM 73-21-60-000-001 Removal of the Electronic Control Unit (ECU) AMM 73-21-60-400-001 Installation of the Electronic Control Unit (ECU) AMM 73-29-00-710-040 Operational Test of the FADEC on the Ground (with
 Engine non Motoring) AMM 77-11-10-000-002 Removal of the N1 Speed Sensor (4000EV) AMM 77-11-10-400-002 Installation of the N1 Speed Sensor (4000EV)
 3. Fault Confirmation
__________________

 A. Do the operational test of the FADEC 1B on the ground (with engine non motoring) (Ref. AMM TASK 73-29-00-710-040).
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 4. Fault Isolation
_______________

 A. The failure message is generated if channel B input from the N1 sensor is invalid or out of range.
 (1) If the failure message N1 SNSR, J10, ECU is not confirmed: R
R (a) No maintenance action is required.
 (2) If the failure message N1 SNSR, J10, ECU is not confirmed but is repetitive:
 - disconnect HJ10 harness from the N1 sensor (N1-B connector).
R (a) Visually examine the receptacle and the connector for damaged R pins or contamination (Ref. AMM TASK 73-21-50-210-002).
 1 If damage is found:
_ - repair or replace as required.

 2 If no damage is found:
_

 - do a cleaning of the connector and receptacle using a bristle brush with stoddard solvent (Material No. CP2011) (Ref. AMM TASK 73-21-50-210-002).
 (b) If the failure continues during the subsequent flights:

 - replace the SENSOR-N1 ROTATIONAL SPD (4000EV) (Ref. AMM TASK 77-11-10-000-002) and (Ref. AMM TASK 77-11-10-400-002).

 (c) If the failure continues during the subsequent flights:

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

 (d) If the failure continues during the subsequent flights:


 - replace the HJ10 harness (Ref. AMM TASK 73-21-50-000-043) and (Ref. AMM TASK 73-21-50-400-043).
 (3) If the failure message N1 SNSR, J10, ECU is confirmed: R - disconnect the HJ10 harness from the N1 sensor (N1-B connector).
R (a) Visually examine the receptacle and the connector for damaged R pins or contamination (Ref. AMM TASK 73-21-50-210-002).
 1 If damage is found:
_ - repair or replace as required.

 2 If no damage is found:
_ R - do the electrical resistance test through the N1 sensor R (4000EV) (channel B) between:
 . pins 1 and 2 (40 to 80 ohms)
 for S/N different than 25451 and up:
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 . pins 1 and 3 (>5 kiloohms)


R . pin 1 and the ground (>10 megohms)

 for S/N 25451 and up: . pins 1 and 3 (>10 megohms)

R . pin 1 and the ground (>10 megohms).


 a If the resistance values are out of the specified limits:
_

 - replace the N1 sensor (4000EV) (Ref. AMM TASK 77-11-10-000-002) and (Ref. AMM TASK 77-11-10-400-002).
 b If the resistance values are in the specified limits:
_ R - connect the HJ10 harness to the N1 sensor.
R (b) Disconnect the HJ10 harness from the ECU (4000KS) and visually R examine the receptacle and the connector for damaged pins or R contamination (Ref. AMM TASK 73-21-50-210-002).
 1 If damage is found:
_ - repair or replace as required.

 2 If no damage is found:
_ R - do the electrical resistance test through the HJ10 harness R between:
 . pins 16 and 17 (40 to 80 ohms)
 for S/N different than 25451 and up: . pins 16 and 6 (>5 kiloohms)
R . pin 16 and the ground (>10 megohms)

 for S/N 25451 and up: . pins 16 and 6 (>10 megohms)
 
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