R . pins 4 and 5 (80 to 109.5 ohms)
R . pins 6 and 7 (85 to 115 ohms)
R . pins 2 and 3 (85 to 115 ohms)
R . pins 4 and 1 (> 10 megohms)
R . pins 6 and 1 (> 10 megohms)
R . pins 2 and 1 (> 10 megohms)
R . pin 4 and the ground (> 10 megohms)
R . pin 6 and the ground (> 10 megohms)
R . pin 2 and the ground (> 10 megohms).
R 3_ If the resistance values are in the specified limits:
R - replace the ECU (4000KS) (Ref. AMM TASK 73-21-60-000-001)
R and (Ref. AMM TASK 73-21-60-400-001).
R 4_ If the resistance values are out of the specified limits:
R - disconnect the HJ11 harness from the CJ11R harness located
R at the 6 o'clock junction box and do an electrical
R resistance test through the CJ11R harness between:
R . pins 20 and 21 (80 to 109.5 ohms)
R . pins 7 and 19 (85 to 115 ohms)
R . pins 2 and 9 (85 to 115 ohms)
R . pins 20 and 8 (> 10 megohms)
R . pins 7 and 8 (> 10 megohms)
R . pins 2 and 8 (> 10 megohms)
R . pin 20 and the ground (> 10 megohms)
R . pin 7 and the ground (> 10 megohms)
R . pin 2 and the ground (> 10 megohms).
R 5_ If the resistance values are in the specified limits:
R - replace the harness HJ11 (ECU to the 6 o'clock junction box)
R (Ref. AMM TASK 73-21-50-000-044) and (Ref. AMM TASK 73-21-
50-400-044).
R 6_ If the resistance values are out of the specified limits:
R - replace the harness CJ11R (Ref. AMM TASK 73-21-50-000-026)
R and (Ref. AMM TASK 73-21-50-400-026).
R
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R B. Do the test given in Para. 3.A.
R (1) No additional maintenance action is required if the fault is not
R confirmed.
R (2) Repeat the fault isolation procedure if the fault continues.
R
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TASK 75-22-00-810-803
Loss of the Feedback Signal from the LPTC Valve - Engine 1 - Channel B
1. Possible Causes
_______________
- LPTC valve
- ECU (4000KS)
- harness HJ12
- harness CJ12R
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 73-21-50-000-028 Removal of the CJ12R Harness AMM 73-21-50-000-045 Removal of the HJ12 Harness AMM 73-21-50-210-002 Visual Inspection of the Wiring Harnesses AMM 73-21-50-400-028 Installation of the CJ12R Harness AMM 73-21-50-400-045 Installation of the HJ12 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 75-22-10-000-002 Removal of the Low Pressure Turbine Active Clearance Control (LPTACC) Valve AMM 75-22-10-400-002 Installation of the Low Pressure Turbine Active Clearance Control (LPTACC) Valve
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).
4. Fault Isolation
_______________
A. The fault message is generated if the channel B signal is invalid, out of range.
(1) If the failure message LPTC VLV, J12, ECU is not confirmed: R
R (a) No maintenance action is required.
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(2) If the failure message LPTC VLV, J12, ECU is not confirmed but is
repetitive: R - disconnect the CJ12R harness (LPT-B) connector (located in the R right core compartment) from the LPTC valve and visually examine R the receptacles and the connectors for damaged pins or R contamination (Ref. AMM TASK 73-21-50-210-002).
R (a) If damage is found:
R - repair or replace as required.
R (b) If no damage is found: 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320 Trouble Shooting Manual 排故手册 大气 AIR(21)
