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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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 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. CP2011  * stoddard solvent (Ref. 70-30-00)
 C. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 73-21-50-000-042 Removal of the HJ9 Harness AMM 73-21-50-210-002 Visual Inspection of the Wiring Harnesses AMM 73-21-50-400-042 Installation of the HJ9 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 2A on the ground (with engine non motoring) (Ref. AMM TASK 73-29-00-710-040).
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 4. Fault Isolation
_______________

R A. The failure message is generated if channel A and channel B inputs from
R the N1 sensor disagree.

R (1) If the failure message N1 SNSR, J9, ECU* is not confirmed:

R (a) No maintenance action is required.

R (2) If the failure message N1 SNSR, J9, ECU* is not confirmed but is
R repetitive:
R - disconnect HJ9 harness from the N1 sensor (N1-A connector).

R (a) Visually examine the receptacle and the connector for damaged
R pins or contamination (Ref. AMM TASK 73-21-50-210-002).

R 1_ If damage is found:
R - repair or replace as required.

R 2_ If no damage is found:
R - do a cleaning of the connector and receptacle using a
R bristle brush with stoddard solvent (Material No. CP2011)
R (Ref. AMM TASK 73-21-50-210-002).

R (b) If the failure continues during the subsequent flights:
R - replace the SENSOR-N1 ROTATIONAL SPD (4000EV) (Ref. AMM TASK
R 77-11-10-000-002) and (Ref. AMM TASK 77-11-10-400-002).

R (c) If the failure continues during the subsequent flights:
R - replace the ECU (4000KS) (Ref. AMM TASK 73-21-60-000-001) and
R (Ref. AMM TASK 73-21-60-400-001).

R (d) If the failure continues during the subsequent flights:
R - replace the HJ9 harness (Ref. AMM TASK 73-21-50-000-042) and
R (Ref. AMM TASK 73-21-50-400-042).

R (3) If the failure message N1 SNSR, J9, ECU* is confirmed:
R - disconnect the HJ9 harness from the N1 sensor (N1-A connector).

R (a) Visually examine the receptacle and the connector for damaged
R pins or contamination (Ref. AMM TASK 73-21-50-210-002).

R 1_ If damage is found:
R - repair or replace as required.

R 2_ If no damage is found:
R - do the electrical resistance test through the N1 sensor
R (4000EV) (channel A) between:

R . pins 1 and 2 (40 to 80 ohms)
R
R for S/N different than 25451 and up:


R . pins 1 and 3 (>5 kiloohms)

 

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

R  for S/N 25451 and up: 
R  . pins 1 and 3 (>10 megohms) 
R  . pin 1 and the ground (>10 megohms). 
R  a_  If the resistance values are out of the specified limits:
R  - replace the N1 sensor (4000EV) (Ref. AMM TASK 77-11-10-
R  000-002) and (Ref. AMM TASK 77-11-10-400-002). 
R  b_  If the resistance values are in the specified limits:
R  - connect the HJ9 harness to the N1 sensor. 
R  (b) Disconnect the HJ9 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). 
R  1_  If damage is found:
R  - repair or replace as required. 
R  2_  If no damage is found:
 
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