• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-28 18:34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

PANEL DESIGNATION IDENT. LOCATION
 -------------------------------------------------------------------------------
121VU EIS/FWC2/SPLY 2WW Q07
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
 B. Test Do the EIS input test (system 1) (Ref. AMM TASK 31-60-00-740-002).
R **ON A/C 401-499,
 B. Test Do the Ground Scanning Test of the DMC (Ref. AMM TASK 31-60-00-740-007).

 


 4. Fault Isolation
_______________
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
 A. If the test gives the maintenance message:
 DMC1: NO FWC2 DATA

 - replace the DMC-1 (1WT1) (Ref. AMM TASK 31-63-34-000-001) and (Ref. AMM TASK 31-63-34-400-001).
 (1) If the fault continues:
 - do a check and repair the wiring from DMC1 (1WT1) pins AA/10J, 10K to the first terminal block (Ref. ASM 31-52/05).
R **ON A/C 401-499,
 A. If the test gives the maintenance message:
 FWC2(1WW2) BUSX DATA/DMC1(1WT1)

 - replace the DMC-1 (1WT1) (Ref. AMM TASK 31-63-34-000-001) and (Ref. AMM TASK 31-63-34-400-001).
 (1) If the fault continues:
 - do a check and repair the wiring from DMC1 (1WT1) pins AD/8C, 8D to the first terminal block (Ref. ASM 31-52/05).
 **ON A/C ALL
 B. Do the test given in Para. 3.B.

 


 Loss of the ARINC 429 Link from the FWC2 to the DMC3
 1. Possible Causes
_______________
 - DMC-3 (1WT3)

 - wiring


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
AMM 31-60-00-740-002 EIS Input Test
 AMM 31-60-00-740-007 GROUND SCANNING Test of the DMC
 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)
 ASM 31-52/05

 3. Fault Confirmation
__________________
 A. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
 -------------------------------------------------------------------------------
121VU EIS/FWC2/SPLY 2WW Q07
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
 B. Test Do the EIS input test (system 3) (Ref. AMM TASK 31-60-00-740-002).
R **ON A/C 401-499,
 B. Test Do the Ground Scanning Test of the DMC (Ref. AMM TASK 31-60-00-740-007).

 


 4. Fault Isolation
_______________
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
 A. If the test gives the maintenance message:
 DMC3: NO FWC2 DATA

 - replace the DMC-3 (1WT3) (Ref. AMM TASK 31-63-34-000-001) and (Ref. AMM TASK 31-63-34-400-001).
 (1) If the fault continues:
 - do a check and repair the wiring from DMC3 (1WT3) pins AA/10J, 10K to the first terminal block (Ref. ASM 31-52/05).
R **ON A/C 401-499,
 A. If the test gives the maintenance message:
 FWC2(1WW2) BUSX DATA/DMC3(1WT3)

 - replace the DMC-3 (1WT3) (Ref. AMM TASK 31-63-34-000-001) and (Ref. AMM TASK 31-63-34-400-001).
 (1) If the fault continues:
 - do a check and repair the wiring from DMC3 (1WT3) pins AD/8C, 8D to the first terminal block (Ref. ASM 31-52/05).
 **ON A/C ALL
 B. Do the test given in Para. 3.B.

 

 TASK 31-63-00-810-967
 Loss of the ILS 1 Test Display
 1. Possible Causes
_______________
 - DMC-1 (1WT1)

 - RECEIVER-ILS, 1 (2RT1)

 - wiring of the ILS 1 INPUT signal


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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)
 AMM 34-36-00-740-002 BITE Test of the ILS
 AMM 34-36-31-000-001 Removal of the ILS Receiver (2RT1,2RT2)
 AMM 34-36-31-400-001 Installation of the ILS Receiver (2RT1,2RT2)
 ASM 34-36/01

 3. Fault Confirmation
__________________
 A. Test Do the BITE test of the ILS (system 1) (Ref. AMM TASK 34-36-00-740-002).
 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 2(107)