- replace the SPEED SENSOR (8060KM2) (Ref. AMM TASK 49-71-13-000-001) and (Ref. AMM TASK 49-71-13-400-001).
 (1) If the fault continues after the first flight on the subsequent day:

 - replace the ECB (59KD) (Ref. AMM TASK 49-61-34-000-001) and (Ref. AMM TASK 49-61-34-400-001).

 (2) If the fault continues after the first flight on the subsequent day:

 - do a check and repair the wiring from the ECB (59KD) AB/B5, B6 to the SPEED SENSOR 2 P27/1, 2 (Ref. ASM 49-61/02).
R **ON A/C 001-003, 051-099, 401-499,
 B. Do the operational test of the APU (Ref. AMM TASK 49-00-00-710-004).
 NOTE : Make an entry in the applicable logbook that you must read the APU
____ CLASS 3 FAULTS after the first flight on the subsequent day.

 TASK 49-70-00-810-803
 Thermocouple Rake 1 Defective (GTCP 36-300)
 1. Possible Causes
_______________
 - EGT THERMOCOUPLE RAKE 1

 - ECB (59KD)

 - wiring

 - EGT THERMOCOUPLE RAKE (8057KM1)

 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
AMM 49-00-00-710-004 Operational Test of the APU (4005KM) (GTCP 36-300) AMM 49-61-34-000-001 Removal of the Electronic Control Box (ECB) (59KD) (GTCP 36-300) AMM 49-61-34-400-001 Installation of the Electronic Control Box (ECB) (59KD) (GTCP 36-300) AMM 49-72-15-000-001 Removal of the Thermocouple (8057KM1) and (8057KM2) (APS 3200) AMM 49-72-15-400-001 Installation of the Thermocouple Probes (8057KM1) and (8057KM2) (GTCP 36-300) ASM 49-61/02
 3. Fault Confirmation
__________________
 A. Do the operational test of the APU (Ref. AMM TASK 49-00-00-710-004).
 4. Fault Isolation
_______________
 **ON A/C 001-003, 051-062,
 A. If the test gives the maintenance message EGT TC RAKE 1:
 - replace the EGT THERMOCOUPLE RAKE 1 (Ref. AMM TASK 49-72-15-000-001) and (Ref. AMM TASK 49-72-15-400-001).
 (1) If the fault continues after the first flight on the subsequent day:

 - replace the ECB (59KD) (Ref. AMM TASK 49-61-34-000-001) and (Ref. AMM TASK 49-61-34-400-001).

 (2) If the fault continues after the first flight on the subsequent day:

 - do a check and repair the wiring from the ECB (59KD) AB/A6, A7 to the EGT THERMOCOUPLE RAKE 1 studs/alumel, chromel (Ref. ASM 49-61/02).

R **ON A/C 063-099, 401-499,
 A. If the test gives the maintenance message:
 EGT TCPLE RAKE (8057KM1)
 with the LRU TROUBLE SHOOT DATA menu information:
 EGT 1 SENSOR SHOWS OUT OF RANGE LOW
 Fault Code Number: 042
 or
 EGT 1 SENSOR DISAGREES WITH EGT2 SENSOR > 166C
 Fault Code Number: 043

 - replace the EGT THERMOCOUPLE RAKE (8057KM1) (Ref. AMM TASK 49-72-15-000-001) and (Ref. AMM TASK 49-72-15-400-001).
 (1) If the fault continues after the first flight on the subsequent day:

 - replace the ECB (59KD) (Ref. AMM TASK 49-61-34-000-001) and (Ref. AMM TASK 49-61-34-400-001).

 (2) If the fault continues after the first flight on the subsequent day:

 - do a check and repair the wiring from the ECB (59KD) AB/A6, A7 to the EGT THERMOCOUPLE RAKE 1 studs/alumel, chromel (Ref. ASM 49-61/02).
R **ON A/C 001-003, 051-099, 401-499,
 B. Do the operational test of the APU (Ref. AMM TASK 49-00-00-710-004).
 NOTE : Make an entry in the applicable logbook that you must read the APU
____ CLASS 3 FAULTS after the first flight on the subsequent day.

 TASK 49-70-00-810-804

 Thermocouple Rake 2 Defective (GTCP 36-300)
 1. Possible Causes
_______________
 - EGT THERMOCOUPLE RAKE 2

 - ECB (59KD)

 - wiring

 - EGT THERMOCOUPLE RAKE (8057KM2)

 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
AMM 49-00-00-710-004 Operational Test of the APU (4005KM) (GTCP 36-300) AMM 49-61-34-000-001 Removal of the Electronic Control Box (ECB) (59KD) (GTCP 36-300) AMM 49-61-34-400-001 Installation of the Electronic Control Box (ECB) (59KD) (GTCP 36-300) AMM 49-72-15-000-001 Removal of the Thermocouple (8057KM1) and (8057KM2) (APS 3200) AMM 49-72-15-400-001 Installation of the Thermocouple Probes (8057KM1) and (8057KM2) (GTCP 36-300) ASM 49-61/02
　
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 機載輔助動力 2(157)