∞∞75-22-00∞∞∞∞∞∞∞∞∞∞Page 230
E Aug 01/01EE -------------------------------------------------------------------------------

 F  『
 E  C F M  E
 E  E
 E  56  E
 E  E

REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
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
__________________
 A. Test
 (1) Do the operational test of the FADEC 2A and 2B on the ground (with engine non motoring) (Ref. AMM TASK 73-29-00-710-040).
 4. Fault Isolation
_______________
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).
 F 『 EEFF : ALL E ∞∞75-22-00∞∞∞∞∞∞∞∞∞∞Page 231
 E E May 01/05 E E ECES
E

 F 『
 E C F M E
 E E
 E 56 E
 E E

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

 - replace the harness CJ11R (located in the right core compartment) (Ref. AMM TASK 73-21-50-000-002) (Ref. AMM TASK 73-21-50-400-002).

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

 - replace the harness J12 (Ref. AMM TASK 73-21-50-000-011) and (Ref. AMM TASK 73-21-50-400-011).

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

 - replace the harness CJ12R (located in the right core compartment) (Ref. AMM TASK 73-21-50-000-004) (Ref. AMM TASK 73-21-50-400-004).
 (3) If the failure message LPTC VLV, J11, ECU is confirmed on channel A:
 - disconnect the CJ11R harness (LPT-A) connector (located in the right core compartment) from the LPTC valve 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:

 - do the electrical resistance test through the LPTC valve between: . pins 2 and 3 (80 to 109.5 ohms) . pins 4 and 5 (85 to 115 ohms) . pins 6 and 7 (85 to 115 ohms) . pin 2 and the ground (> 10 megohms) . pin 4 and the ground (> 10 megohms) . pin 6 and the ground (> 10 megohms).

 (c) If the resistance values are out of the specified limits:

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

 (d) If the resistance values are in the specified limits:

 - connect the CJ11R harness (LPT-A) connector to the LPTC valve receptacle (located in the right core compartment),

 - disconnect the J11 harness from the ECU (4000KS) and visually examine the receptacles and the connectors for damaged pins or contamination (Ref. AMM TASK 73-21-50-210-001).

 1 If damage is found:
_ - repair or replace as required.
 2 If no damage is found:
_
 - do an electrical resistance test through the J11 harness between: . pins 4 and 5 (80 to 109.5 ohms) . pins 6 and 7 (85 to 115 ohms)
 F 『R EEFF : 001-049, 051-099, 101-105, 151-154, E ∞∞75-22-00∞∞∞∞∞∞∞∞∞∞Page 232 E E201-207, May 01/05 E E ECES
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 大氣 AIR(31)