A320 Trouble Shooting Manual 排故手册 大气 AIR(26)

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R 2. Job Set-up Information
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R A. Referenced Information
R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R  AMM  73-21-50-000-002 
R  AMM  73-21-50-000-004 
R  AMM  73-21-50-000-010 
R  AMM  73-21-50-000-011 
R  AMM  73-21-50-000-026 
R  AMM  73-21-50-000-028 
R  AMM  73-21-50-000-044 
R  AMM  73-21-50-000-045 
R  AMM  73-21-50-210-001 
R  AMM  73-21-50-210-002 
R  AMM  73-21-50-400-002 
R  AMM  73-21-50-400-004 
R  AMM  73-21-50-400-010 
R  AMM  73-21-50-400-011 
R  AMM  73-21-50-400-026 
R  AMM  73-21-50-400-028 
R  AMM  73-21-50-400-044 
R  AMM  73-21-50-400-045 
R  AMM  73-21-60-000-001 
R  AMM  73-21-60-000-001 
R  AMM  73-21-60-400-001 
R 
R  AMM  73-21-60-400-001 
R  AMM  73-29-00-710-040 
R 
R  AMM  75-22-10-000-001 
R 

F EEFF : ALL E E ECES Removal of the CJ11R Harness Removal of the CJ12R Harness Removal of the J11 Harness Removal of the J12 Harness Removal of the CJ11R Harness Removal of the CJ12R Harness Removal of the HJ11 Harness Removal of the HJ12 Harness Visual Inspection of the Wiring Harness Visual Inspection of the Wiring Harnesses Installation of the CJ11R Harness Installation of the CJ12R Harness Installation of the J11 Harness Installation of the J12 Harness Installation of the CJ11R Harness Installation of the CJ12R Harness Installation of the HJ11 Harness Installation of the HJ12 Harness Removal of the Electronic Control Unit (ECU)(4000KS) Removal of the Electronic Control Unit (ECU) Installation of the Electronic Control Unit (ECU)(4000KS) Installation of the Electronic Control Unit (ECU) Operational Test of the FADEC on the Ground (with Engine non Motoring) Removal of the Low Pressure Turbine Active Clearance Control Valve (LPTACC).
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REFERENCE DESIGNATION
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AMM 75-22-10-000-002 Removal of the Low Pressure Turbine Active Clearance Control (LPTACC) Valve AMM 75-22-10-400-001 Installation of the Low Pressure Turbine Active Clearance Control Valve (LPTACC). AMM 75-22-10-400-002 Installation of the Low Pressure Turbine Active Clearance Control (LPTACC) Valve
 3. Fault Confirmation
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 A. Test
 (1) Do the operational test of the FADEC 1A and 1B on the ground (with engine non motoring) (Ref. AMM TASK 73-29-00-710-040).
 4. Fault Isolation
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R **ON A/C 001-049, 051-099, 101-105, 151-154, 201-207,
 A. The failure messages are generated if the channels A and B signals are invalid, out of range, or both channels disagree.
 (1) If the failure messages LPTC VLV, J11, ECU and LPTC VLV, J12, ECU are not confirmed:

 (a) No maintenance action is required.

 (2) If the failure messages LPTC VLV, J11, ECU and LPTC VLV, J12, ECU are not confirmed but are repetitive:

 - disconnect the CJ11R and CJ12R harnesses from the LPTC valve (LPT-A and LPT-B connectors) and visually examine the receptacles and the connectors for damaged pins or contamination (Ref. AMM TASK 73-21-50-210-001).
 (a) If damage is found:

 - repair or replace as required.

 (b) If no damage is found:

 - replace the LPTC valve (Ref. AMM TASK 75-22-10-000-001) and (Ref. AMM TASK 75-22-10-400-001).

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

 - replace the harness J11 (Ref. AMM TASK 73-21-50-000-010) and (Ref. AMM TASK 73-21-50-400-010).
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