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时间:2011-03-29 09:34来源:蓝天飞行翻译 作者:航空
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______________________
 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 73-29-00-710-040 Operational Test of the FADEC on the Ground (with Engine non Motoring)
 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 ECU (PS12 SENSOR):
 - replace the ECU (4000KS) (Ref. AMM TASK 73-21-60-000-001) (Ref. AMM TASK 73-21-60-400-001).
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 Loss of the Signal of the Channel B TCC-Sensor on Engine 1
 1. Possible Causes
_______________
 - TCC sensor

 - harness CJ13

 - harness HJ13

 - ECU (4000KS)


 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific bristle brush No specific soft nose pliers
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. CP2011  * stoddard solvent (Ref. 70-30-00)
 C. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 73-21-50-000-029 Removal of the CJ13 Harness AMM 73-21-50-000-046 Removal of the HJ13 Harness AMM 73-21-50-210-002 Visual Inspection of the Wiring Harnesses AMM 73-21-50-400-029 Installation of the CJ13 Harness AMM 73-21-50-400-046 Installation of the HJ13 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 73-21-70-000-002 Removal of the High Pressure Turbine Clearance
 Control (HPTCC) Sensor AMM 73-21-70-400-002 Installation of the High Pressure Turbine Clearance Control (HPTCC) Sensor AMM 73-29-00-710-040 Operational Test of the FADEC on the Ground (with Engine non Motoring)
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 3. Fault Confirmation
__________________
 A. Do the operational test of the FADEC 1 on the ground (with engine non motoring) (Ref. AMM TASK 73-29-00-710-040).
 4. Fault Isolation
_______________
 A. For configuration pre SB CFMI73-046
 NOTE : The failure message is triggered if the TCC sensor channel B input
____ is invalid (signal out of range) and the fault lasts for more than 20 seconds.
 (1) If the failure message TCC SNSR, J13, ECU is not confirmed:

 (a) Do the following trouble shooting at next maintenance opportunity:
 - disconnect the CJ13 connector (TCC-B) from the TCC sensor (3 O'Clock).

 - visually examine the harness connector and sensor receptacle for damaged pins or contamination/oxidation.

 - if damage is found, repair or replace as required.

 - 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).

 - connect the harness connector to the sensor. Tighten the connector by hand plus one eighth of a turn. If necessary use soft nose pliers.

 

 (2) If the failure message TCC SNSR, J13, ECU is not confirmed but is repetitive:


 (a) Do the following trouble shooting at next maintenance opportunity:
 - disconnect the CJ13 connector (TCC-B) from the TCC sensor (3 O'Clock).

 - do a cleaning of the harness connector using a bristle brush with stoddard solvent (Material No. CP2011) (Ref. AMM TASK 73-21-50-210-002).
 
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