• 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

 3. Fault Confirmation
__________________
 A. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU ENGINE/2/FADEC A/AND EIU 2 2KS2 A05
R  **ON A/C 106-149, 303-399,
R B. Test
R Do the EIS input test (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).
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 106-149, 303-399, 401-499, ∞∞31-63-00∞∞∞∞∞∞∞∞∞∞Page A258
 Aug 01/05 CES

 

R  **ON A/C 106-149, 303-399, 401-499,
 4. Fault Isolation_______________ 
R  **ON A/C 401-499,
 A. If the test gives the maintenance message EEC(E2-4000KS)BUS EEC2A/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 the DMC 3 (1WT3) pins AE/1A, 1B to the first terminal block (Ref. ASM 31-62/01). 
R  **ON A/C 106-149, 303-399, 401-499,
 B. Do the test given in Para. 3.B.

 


 Loss of the EEC 2 Channel B Output Bus by the DMC 3
 1. Possible Causes
_______________
 - DMC-3 (1WT3)

 - wiring


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
R  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 31-62/01
 3. Fault Confirmation
__________________
 A. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------
PANEL DESIGNATION  IDENT. LOCATION
 -------------------------------------------------------------------------------
121VU ENGINE/ENG2/FADEC B  4KS2 Q40
R  **ON A/C 106-149, 303-399,
R B. Test
R Do the EIS input test (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).
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 106-149, 303-399, 401-499, ∞∞31-63-00∞∞∞∞∞∞∞∞∞∞Page A260
 Aug 01/05 CES

 

R  **ON A/C 106-149, 303-399, 401-499,
 4. Fault Isolation_______________ 
R  **ON A/C 401-499,
 A. If the test gives the maintenance message EEC(E2-4000KS)BUS EEC2B/DMC3: - 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 the DMC 3 (1WT3) pins AE/15A, 15B to the first terminal block (Ref. ASM 31-62/01). 
R  **ON A/C 106-149, 303-399, 401-499,
 B. Do the test given in Para. 3.B.

 

 

 TASK 31-63-00-810-894
 Loss of the FAC 1 Output Bus by the DMC 2
 1. Possible Causes
_______________
 - DMC-2 (1WT2)

 - 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 22-65/01
 ASM 31-62/01

 3. Fault Confirmation
__________________
 A. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU AUTO FLT/FAC1/28VDC 5CC1 B04 49VU AUTO FLT/FAC1/26VAC 14CC1 B03
 
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(71)