• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-28 18:37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

 4. Fault Isolation
_______________
 A. Read the Post Flight Report
 (1) If the PFR gives the maintenance message:
 DMC2(1WT2)/DU EWD(4WT1)/DU PFD FO(2WT2)

 - replace the DMC-2 (1WT2) and the DU-ECAM, UPPER (4WT1) (Ref. AMM TASK 31-63-34-000-001) (Ref. AMM TASK 31-63-34-400-001) (Ref. AMM TASK 31-63-22-000-001) (Ref. AMM TASK 31-63-22-400-001)
 B. Do the EIS system test (Ref. AMM TASK 31-60-00-740-004)
 (1) If the test gives the maintenance message DU PFD FO(2WT2)/DMC2(1WT2)
 - replace the PFD-F/O (2WT2) (Ref. AMM TASK 31-63-22-000-001) and (Ref. AMM TASK 31-63-22-400-001) Feedback Message from the DMC1 on the FO ND DU

 


 1. Possible Causes
_______________
 - DMC-1 (1WT1)

 - DU-ECAM, LOWER (4WT2)

 - ND-F/O (3WT2)


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 31-60-00-740-004 EIS System Test AMM 31-63-22-000-001 Removal of the Display Unit (2WT1,2WT2,3WT1,3WT2,4WT1,4WT2) AMM 31-63-22-400-001 Installation of the Display Unit
 (2WT1,2WT2,3WT1,3WT2,4WT1,4WT2) AMM 31-63-34-000-001 Removal of the DMC (1WT1,1WT2,1WT3) AMM 31-63-34-400-001 Installation of the DMC (1WT1,1WT2,1WT3)
 3. Fault Confirmation
__________________
 A. Test
 - Not applicable, the fault cannot be confirmed.
 4. Fault Isolation
_______________
 A. Read the Post Flight Report
 (1) If the PFR gives the maintenance message:
 DMC1(1WT1)/DU SD(4WT2)/DU ND FO(3WT2)

 - replace the DMC-1 (1WT1) and the DU-ECAM, LOWER (4WT2) (Ref. AMM TASK 31-63-34-000-001) (Ref. AMM TASK 31-63-34-400-001) (Ref. AMM TASK 31-63-22-000-001) (Ref. AMM TASK 31-63-22-400-001)
 B. Do the EIS system test (Ref. AMM TASK 31-60-00-740-004)
 (1) If the test gives the maintenance message DU ND FO(3WT2)/DMC1(1WT1)
 - replace the ND-F/O (3WT2) (Ref. AMM TASK 31-63-22-000-001) and (Ref. AMM TASK 31-63-22-400-001) Feedback Message from the DMC1 on the CAPT ND DU

 

 1. Possible Causes
_______________
 - DMC-1 (1WT1)

 - DU-ECAM, LOWER (4WT2)

 - ND-CAPT (3WT1)


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 31-60-00-740-004 EIS System Test AMM 31-63-22-000-001 Removal of the Display Unit (2WT1,2WT2,3WT1,3WT2,4WT1,4WT2) AMM 31-63-22-400-001 Installation of the Display Unit
 (2WT1,2WT2,3WT1,3WT2,4WT1,4WT2) AMM 31-63-34-000-001 Removal of the DMC (1WT1,1WT2,1WT3) AMM 31-63-34-400-001 Installation of the DMC (1WT1,1WT2,1WT3)
 3. Fault Confirmation
__________________
 A. Test
 - Not applicable, the fault cannot be confirmed.
 4. Fault Isolation
_______________
 A. Read the Post Flight Report
 (1) If the PFR gives the maintenance message:
 DMC1(1WT1)/DU SD(4WT2)/DU ND CAPT(3WT1)

 - replace the DMC-1 (1WT1) and the DU-ECAM, LOWER (4WT2) (Ref. AMM TASK 31-63-34-000-001) (Ref. AMM TASK 31-63-34-400-001) (Ref. AMM TASK 31-63-22-000-001) (Ref. AMM TASK 31-63-22-400-001)
 B. Do the EIS system test (Ref. AMM TASK 31-60-00-740-004)
 (1) If the test gives the maintenance message DU ND CAPT(3WT1)/DMC1(1WT1)
 - replace the ND-CAPT (3WT1) (Ref. AMM TASK 31-63-22-000-001) and (Ref. AMM TASK 31-63-22-400-001) Feedback Message from the DMC3 on the FO ND DU

 

 1. Possible Causes
_______________
 - DMC-3 (1WT3)

 - DU-ECAM, LOWER (4WT2)

 - ND-F/O (3WT2)


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 31-60-00-740-004 EIS System Test AMM 31-63-22-000-001 Removal of the Display Unit (2WT1,2WT2,3WT1,3WT2,4WT1,4WT2) AMM 31-63-22-400-001 Installation of the Display Unit
 (2WT1,2WT2,3WT1,3WT2,4WT1,4WT2) AMM 31-63-34-000-001 Removal of the DMC (1WT1,1WT2,1WT3) AMM 31-63-34-400-001 Installation of the DMC (1WT1,1WT2,1WT3)
 3. Fault Confirmation
__________________
 A. Test
 - Not applicable, the fault cannot be confirmed.
 4. Fault Isolation
 
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 指示和记录系统 3(96)