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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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 . pins 1 and 2 (40 to 80 ohms)


 for S/N different than 25451 and up: . 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 HJ9 harness to the N1 sensor. R
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:
_ - repair or replace as required.

 2 If no damage is found:
_ R - do the electrical resistance test through the HJ9 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)

R . pin 16 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:
_

 - replace the HJ9 harness (Ref. AMM TASK 73-21-50-000-042) and (Ref. AMM TASK 73-21-50-400-042).
 F 『 EEFF : ALL E ∞∞77-10-00∞∞∞∞∞∞∞∞∞∞Page 253
 E E Aug 01/99 E E ECES
E F 『 E C F M E E E E 56 E E E B. Do the test given in Para. 3.A.

 


 (1) No additional maintenance action is required if the fault is not confirmed.

 (2) Repeat the fault isolation procedure if the fault continues.


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ECES  TASK 77-10-00-810-828

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 Loss of the Feedback Signal of the N1 Speed Sensor - Engine 1 - Channel B
 1. Possible Causes
_______________

 - SENSOR-N1 ROTATIONAL SPD (4000EV)

 - ECU (4000KS)

 - HJ10 harness

 

 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
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 A and channel B inputs from R the N1 sensor disagree.
 (1) If the failure message N1 SNSR, J10, ECU* is not confirmed: R
R (a) No maintenance action is required.
 
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