(6DA1,6DA2,6DA3)
 AMM 34-13-00-740-002 INTERFACE TEST of the ADR
 ASM 30-31/02
 ASM 34-13/02

 3. Fault Confirmation
__________________
 A. Test
 (1) Do the operational test of the probe ice protection (Ref. AMM TASK 30-31-00-710-001).
 4. Fault Isolation
_______________
 A. If the test gives the maintenance message CHECK ADIRU 2 - L STATIC PHC2 INTERFACE:
 - do a check for ground at pin A/X of the PHC 2 (6DA2) (Ref. ASM 30-31/02).
 (1) If there is no ground:
 - replace the PHC-2 (6DA2) (Ref. AMM TASK 30-31-34-000-002) and (Ref. AMM TASK 30-31-34-400-002).
 (a) If the fault continues:

 - do a check and repair the wiring from the PHC 2 (6DA2) to the ADIRU 2 (1FP2), pin A/X to pin AA/4G (Ref. ASM 34-13/02).

 (b) If the fault continues:

 - do the INTERFACE TEST of the ADR (system 2) (Ref. AMM TASK 34-13-00-740-002)

 - do the necessary corrective actions: (TSM chapter 34).

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞30-31-00∞∞∞∞∞∞∞∞∞∞Page 292
 May 01/03R CES

 B. Do the operational test given in Para. 3.

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞30-31-00∞∞∞∞∞∞∞∞∞∞Page 293
 May 01/03R
 CES  Loss of the R Static Probe Output-Discrete from the PHC 2

 1. Possible Causes
_______________
 - PHC-2 (6DA2)

 - wiring from the PHC 2 (6DA2) to the ADIRU 2 (1FP2)

 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 30-31-00-710-001 Operational Test of the Probe Ice Protection
 AMM 30-31-34-000-002 Removal of the Probe Heat Computer (PHC)
 (6DA1,6DA2,6DA3)
 AMM 30-31-34-400-002 Installation of the Probe Heat Computer (PHC)

 (6DA1,6DA2,6DA3)
 AMM 34-13-00-740-002 INTERFACE TEST of the ADR
 ASM 30-31/02
 ASM 34-13/02

 3. Fault Confirmation
__________________
 A. Test
 (1) Do the operational test of the probe ice protection (Ref. AMM TASK 30-31-00-710-001).
 4. Fault Isolation
_______________
 A. If the test gives the maintenance message CHECK ADIRU2 R STATIC PHC 2 INTERFACE:
 - do a check for ground at pin A/Y of the PHC 2 (6DA2) (Ref. ASM 30-31/02).
 (1) If there is no ground:
 - replace the PHC-2 (6DA2), (Ref. AMM TASK 30-31-34-000-002) and (Ref. AMM TASK 30-31-34-400-002).
 (a) If the fault continues:

 - do a check and repair the wiring from the PHC 2 (6DA2) to the ADIRU 2 (1FP2) pin A/Y to pin AA/4H (Ref. ASM 34-13/02).

 (b) If the fault continues:

 - do the INTERFACE TEST of the ADR (system 2) (Ref. AMM TASK 34-13-00-740-002)

 - do the necessary corrective actions: (TSM chapter 34).

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞30-31-00∞∞∞∞∞∞∞∞∞∞Page 294
 May 01/03R CES

 B. Do the operational test given in Para. 3.

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞30-31-00∞∞∞∞∞∞∞∞∞∞Page 295
 May 01/03R
 CES  Loss of the TAT Sensor Output-Discrete from the PHC 2

 1. Possible Causes
_______________
 - PHC-2 (6DA2)

 - wiring from the PHC 2 (6DA2) to the ADIRU 2 (1FP2)

 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
34-13-00-810-910 Loss of the TAT Sensor 2 Input on the ADR2
 AMM 30-31-00-710-001 Operational Test of the Probe Ice Protection
 AMM 30-31-34-000-002 Removal of the Probe Heat Computer (PHC)

 (6DA1,6DA2,6DA3)
 AMM 30-31-34-400-002 Installation of the Probe Heat Computer (PHC)
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 除冰和排雨(52)