• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-28 13:22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

 (a) If the voltage is more than 22VDC:

 - replace the STAT INV (3XB) (Ref. AMM TASK 24-28-51-000-001) and (Ref. AMM TASK 24-28-51-400-001).

 (b) If the voltage is less than 22VDC:


 - replace the BAT-1 (2PB1) and BAT-2 (2PB2) (Ref. AMM TASK 24-38-51-000-001) and (Ref. AMM TASK 24-38-51-400-001).
 C. If the test shows the frequency indication in amber:
 - replace the STAT INV (3XB) (Ref. AMM TASK 24-28-51-000-001) and (Ref. AMM TASK 24-28-51-400-001).
 D. If the test shows that amber crosses replace the voltage and frequency indications:
 - do a check of the status of the circuit breaker (27WV).
 (1) If the circuit breaker is closed:
 - do a check for 115VAC at the pin 2 of the circuit breaker (27WV).
 (a) If there is 115VAC:

 - do a check and repair the wiring between: . the pin 2 of the circuit breaker (27WV) and the first branch point, . the branch point and the pins AE/8B of the SDAC 1 (1WV1) and the SDAC 2 (1WV2) (Ref. ASM 24-24/02).

 (b) If there is no 115VAC:


 - do a check and repair the wiring between the pin 1 of the circuit breaker (27WV) and the pin 1 of the circuit breaker AC ESS/BUS/EMER CNTOR/SPLY (15PC) (Ref. ASM 24-35/01).
 「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 ∞∞24-28-00∞∞∞∞∞∞∞∞∞∞Page 210
 Feb 01/03R CES


 (2) If the circuit breaker is open:
 - close it.
 (a) Do a check of the wiring for a short to ground between the pin 2 of the circuit breaker (27WV) and the first branch point (Ref. ASM 24-24/02).
 1 If the wiring is not correct:
_
 - repair it.
 2 If the wiring is correct:

_
 - replace the C/B-EMER/GEN/REF (27WV). R E. Do the test given in para. 3.


 DC GENERATION - FAULT ISOLATION PROCEDURES
__________________________________________
 TASK 24-30-00-810-801
 Failure of the TR1 or TR1 Contactor or Related Wiring
 1. Possible Causes
_______________
 - CNTOR-TR 1 (5PU1)

 - TR-1 (1PU1)

 - wiring

 - C/B - TR1 SPLY (2PU1)

 - C/B - TR1 CNTOR SPLY (4PU1)


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
AMM 24-32-51-000-001 Removal of the Transformer Rectifier (1PU1, 1PU2) AMM 24-32-51-400-001 Installation of the Transformer Rectifier (1PU1, 1PU2) AMM 24-32-55-000-001 Removal of the Transformer 1(2) Contactor (5PU1, 5PU2, 14PU) AMM 24-32-55-400-001 Installation of the Transformer 1(2) Contactor (5PU1, 5PU2, 14PU) AMM 24-41-00-861-002 Energize the Aircraft Electrical Circuits from Engine 1(2) AMM 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2) AMM 31-32-00-860-004 Procedure to Get Access to the SYSTEM
 REPORT/TEST/ELEC Page
 AMM 31-60-00-860-001 EIS Start Procedure
 AMM 31-60-00-860-002 EIS Stop Procedure
 ASM 24-32/02

 3. Fault Confirmation
__________________
 A. Job Set-up
 (1) Aircraft Maintenance Configuration
 (a) Energize the aircraft electrical circuits
 (Ref. AMM TASK 24-41-00-861-002).


 (b) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. AMM TASK 31-60-00-860-001).


 「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 ∞∞24-30-00∞∞∞∞∞∞∞∞∞∞Page 201
 Feb 01/98 CES


 (c) On the MCDU, get the SYSTEM REPORT/TEST/ELEC page (Ref. AMM TASK 31-32-00-860-004).
 B. Test
 NOTE : Before you do the test of the TR1, make sure that the AC BUS 1
____
 supplies its primary winding, in any RESET mode.

 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the ECAM control panel:
- push the ELEC key.
2. On the MCDU:
- push the line key adjacent to the TR1 indication,

 - push the line key adjacent to the RESET indication.


On the upper ECAM DU:
- the TR1 FAULT message comes into view.

 On the lower ECAM DU, on the ELEC page:

 - the line connection between the TR1 and the DC1 busbar is not shown,

 - the DC BAT busbar energizes the DC1 busbar,
 
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 电源 3(36)