• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-28 13:28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

 - wiring of the annunciator light test and interface board (5LP)


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 26-12-00-710-001 Operational Check of Loop/Squib AMM 33-14-33-000-001 Removal of the Annunciator-Light Test and Interface-Board (1LP, 2LP, 3LP, 4LP, 5LP, 6LP, 7LP, R 8LP, 9LP, 10LP, 11LP, 12LP, 18LP, 19LP, 20LP) AMM 33-14-33-400-001 Installation of the Annunciator-Light Test and Interface-Board (1LP, 2LP, 3LP, 4LP, 5LP, 6LP, 7LP, R 8LP, 9LP, 10LP, 11LP, 12LP, 18LP, 19LP, 20LP) ASM 26-12/01
 3. Fault Confirmation
__________________
 A. Test
 (1) Do the operational test of the engine fire and overheat detection (loop/squib) (Ref. AMM TASK 26-12-00-710-001).
 4. Fault Isolation
_______________
 A. If during the test, the first and third rows of the legend of the ENG 1 FIRE pushbutton switch and the FIRE legend of the ENG/1 FIRE/FAULT annunciator do not come on:
 - replace the BOARD-ANN LT TEST & INTFC (5LP) (Ref. AMM TASK 33-14-33-000-001) and (Ref. AMM TASK 33-14-33-400-001).
 (1) If the fault continues:
 - do a check and repair the wiring of the annunciator light test and interface board (5LP), from pin A/33 to the first terminal block (Ref. ASM 26-12/01).
 B. Do the test given in para. 3.
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞26-12-00∞∞∞∞∞∞∞∞∞∞Page 249
 May 01/05 CES Loss of the Second and Fourth Rows of the Legend of the ENG 2 FIRE Pushbutton Switch and the FIRE Legend of the ENG/2 FIRE/FAULT Annunciator

 


 1. Possible Causes
_______________
 - BOARD-ANN LT TEST & INTFC (5LP)

 - wiring of the annunciator light test and interface board (5LP)


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 26-12-00-710-001 Operational Check of Loop/Squib AMM 33-14-33-000-001 Removal of the Annunciator-Light Test and Interface-Board (1LP, 2LP, 3LP, 4LP, 5LP, 6LP, 7LP, R 8LP, 9LP, 10LP, 11LP, 12LP, 18LP, 19LP, 20LP) AMM 33-14-33-400-001 Installation of the Annunciator-Light Test and Interface-Board (1LP, 2LP, 3LP, 4LP, 5LP, 6LP, 7LP, R 8LP, 9LP, 10LP, 11LP, 12LP, 18LP, 19LP, 20LP) ASM 26-12/01
 3. Fault Confirmation
__________________
 A. Test
 (1) Do the operational test of the engine fire and overheat detection (loop/squib) (Ref. AMM TASK 26-12-00-710-001).
 4. Fault Isolation
_______________
 A. If during the test, the second and fourth rows of the legend of the ENG 2 FIRE pushbutton switch and the FIRE legend of the ENG/2 FIRE/FAULT annunciator do not come on:
 - replace the BOARD-ANN LT TEST & INTFC (5LP) (Ref. AMM TASK 33-14-33-000-001) and (Ref. AMM TASK 33-14-33-400-001).
 (1) If the fault continues:
 - do a check and repair the wiring of the annunciator light test and interface board (5LP), from pin A/20 to the first terminal block (Ref. ASM 26-12/01).
 B. Do the test given in para. 3.
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞26-12-00∞∞∞∞∞∞∞∞∞∞Page 250
 May 01/05 CES Loss of the FLT/GND Discrete from the Engine 1 FDU

 


 1. Possible Causes
_______________
 - FDU-ENG1 (2WD1)

 - LGCIU-1 (5GA1)

 - LGCIU-2 (5GA2)

 - wiring of the FLT/GND discrete from the engine 1 FDU (2WD1) to the LGCIU 1 (5GA1)

 - wiring of the FLT/GND discrete from the engine 1 FDU (2WD1) to the LGCIU 2 (5GA2)


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 26-12-00-710-002  Operational Test of the Engine Fire and Overheat Detection with the Centralized Fault Display System (CFDS)
 AMM 26-12-34-000-001 Removal of the Engine Fire-Detection Unit (FDU) (2WD1,2WD2) AMM 26-12-34-400-001 Installation of the Engine Fire-Detection Unit (FDU)
 (2WD1,2WD2)
 AMM 32-31-71-000-001 Removal of the LGCIU (5GA1, 5GA2)
 
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 FIRE PROTECTION 防火(46)