• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-29 09:16来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 3. Fault Confirmation__________________
 A. Do the operational test of the APU (Ref. AMM TASK 49-00-00-710-008).
 4. Fault Isolation_______________
 A. If an APU auto shutdown occurs during the operational test of the APU and the test gives the maintenance message:
 EGT TC1 P30 AND ECB (59KD):
 - replace the EGT THERMOCOUPLE 1 (8057KM1) (Ref. AMM TASK 49-72-15-000-001) and (Ref. AMM TASK 49-72-15-400-002).

 - replace the ECB (59KD) (Ref. AMM TASK 49-61-34-000-002) and (Ref. AMM TASK 49-61-34-400-002).

 

 

 B. Do the operational test of the APU (Ref. AMM TASK 49-00-00-710-008).

 NOTE : After the subsequent flight, make sure that the fault does not
____ continue.

 (1) If the APU CLASS 3 FAULTS page gives the maintenance message EGT TC1 P30 after the subsequent flight:
 - do the applicable trouble shooting procedure (Ref. TASK 49-70-00-810-813).


 TASK 49-00-00-810-891

 

 APU AUTO SHUT DOWN - SENSOR FAILURE, EGT Thermocouple 2 and ECB 59KD Fault (APS 3200)
 1. Possible Causes_______________
 - EGT THERMOCOUPLE 2 (8057KM2)

 - ECB (59KD)


 2. Job Set-up Information______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
49-70-00-810-814  EGT-Thermocouple 2 Defective (APS 3200)
 AMM 49-00-00-710-008  Operational Test of the APU (APS 3200)
 AMM 49-61-34-000-002  Removal of the Electronic Control Box (ECB) (59KD) (APS 3200)
 AMM 49-61-34-400-002  Installation of the Electronic Control Box (ECB) (59KD) (APS 3200)
 AMM 49-72-15-000-001  Removal of the Thermocouple (8057KM1) and (8057KM2) (APS 3200)
 AMM 49-72-15-400-002  Installation of the Thermocouple (8057KM1) and (8057KM2) (APS 3200)
 3. Fault Confirmation__________________
 A. Do the operational test of the APU (Ref. AMM TASK 49-00-00-710-008).
 4. Fault Isolation_______________
 A. If an APU auto shutdown occurs during the operational test of the APU and the test gives the maintenance message:
 EGT TC2 P31 AND ECB (59KD):
 - replace the EGT THERMOCOUPLE 2 (8057KM2) (Ref. AMM TASK 49-72-15-000-001) and (Ref. AMM TASK 49-72-15-400-002).

 - replace the ECB (59KD) (Ref. AMM TASK 49-61-34-000-002) and (Ref. AMM TASK 49-61-34-400-002).

 

 

 B. Do the operational test of the APU (Ref. AMM TASK 49-00-00-710-008).

 NOTE : After the subsequent flight, make sure that the fault does not
____ continue.

 (1) If the APU CLASS 3 FAULTS page gives the maintenance message EGT TC2 P31 after the subsequent flight.
 - do the applicable trouble shooting procedure (Ref. TASK 49-70-00-810-814)


 TASK 49-00-00-810-892

 

 APU AUTO SHUT DOWN - SENSOR FAILURE, Oil Sump and Generator-Oil Temperature Sensor Fault (APS 3200)
 1. Possible Causes
_______________
 - GEN-APU (8XS)

 - wiring

 - OIL TEMPERATURE SENSOR (8084KM)

 - ECB (59KD)


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
AMM 24-23-51-000-001 Removal of the APU Generator 8XS
 AMM 24-23-51-400-001 Installation of the APU Generator 8XS
 AMM 49-00-00-710-005 Self-Test of the ECB (APS 3200)
 AMM 49-61-34-000-002 Removal of the Electronic Control Box (ECB) (59KD)

 (APS 3200) AMM 49-61-34-400-002 Installation of the Electronic Control Box (ECB) (59KD) (APS 3200) AMM 49-91-51-000-002 Removal of the Oil-Sump Temperature Sensor (8084KM) (APS 3200) AMM 49-91-51-400-002 Installation of the Oil-Sump Temperature Sensor (8084KM) (APS 3200) ASM 49-61/02
 3. Fault Confirmation
__________________
 A. Do the self-test of the ECB (Ref. AMM TASK 49-00-00-710-005).
 4. Fault Isolation
_______________
 A. If the APU Last Leg Report gives the maintenance message:
 OIL TEMP SNSR (8084KM) AND GENERATOR (8XS)
 Fault Code Number: 122
 Additionally:
 Fault Code Number: 010 or 011 and 012 or 013

 NOTE : FCN 010-013 on Class 3 Faults Page
____

 NOTE : The APU SHUTDOWNS report gives the maintenance message:
____ SENSOR FAILURE - OIL TEMP SNSR 8084KM AND GENERATOR 8XS APU Auto Shut Down Fault Code Number: 122
 
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 机载辅助动力 1(92)