• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-29 14:34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

 AMM 73-25-34-710-040  Operational Test of the Engine Interface Unit (1KS1,1KS2)
 AMM 73-29-00-710-040  Operational Test of the FADEC on the Ground (with Engine non Motoring)
 ASM 73-25/06
 3. Fault Confirmation__________________
 A. Test
 (1) Do the operational test of the Engine Interface Unit (EIU) through the Centralized Fault Display System (CFDS) (Ref. AMM TASK 73-25-34-710-040).

 (2) Do the operational test of the FADEC 2A and 2B on the ground (with engine non motoring) (Ref. AMM TASK 73-29-00-710-040).


 F 『 EEFF : ALL E ∞∞77-00-00∞∞∞∞∞∞∞∞∞∞Page 296
 E E Nov 01/04 ERE
ECES  4. Fault Isolation

 F  『
 E  C F M  E
 E  E
 E  56  E
 E  E


_______________
 A. If the fault symptom is identified by the upper ECAM warning ENG2 BLEED STATUS FAULT and the tests of the EIU and FADEC give no maintenance messages:
 - do a check for open or short to ground of the harness J3 between the EIU (1KS2) and the ECU (4000KS) pins AB/5A, 5C to pins J3/22, 23 (Ref. ASM 73-25/06).
 (1) If the wiring is not correct:

 - repair the above wiring.

 (2) If the wiring is correct:

 - replace the EIU-2 (1KS2) (Ref. AMM TASK 73-25-34-000-040) and (Ref. AMM TASK 73-25-34-400-040).

 (3) If the fault continues:

 - replace the CONT-ZONE TEMPERATURE (8HK) (Ref. AMM TASK 21-63-34-000-001) and (Ref. AMM TASK 21-63-34-400-001).

 (4) If the fault continues:


 - replace the ECU (4000KS) (Ref. AMM TASK 73-21-60-000-001) and (Ref. AMM TASK 73-21-60-400-001).
 F 『 EEFF : ALL E ∞∞77-00-00∞∞∞∞∞∞∞∞∞∞Page 297
 E E Nov 01/04 ERE
ECES

 F 『
 E C F M E
 E E
 E 56 E
 E E


 TASK 77-00-00-810-888
 Failure of the Starter Shutoff Valve on Engine 1
 1. Possible Causes
_______________
 - starter shutoff valve (SAV)

 - starter

 - harness J9

 - harness J10

 - ECU (4000KS)


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 73-21-50-000-008 Removal of the J9 Harness AMM 73-21-50-000-009 Removal of the J10 Harness AMM 73-21-50-400-008 Installation of the J9 Harness AMM 73-21-50-400-009 Installation of the J10 Harness AMM 73-21-60-000-001 Removal of the Electronic Control Unit (ECU)(4000KS) AMM 73-21-60-400-001 Installation of the Electronic Control Unit
 (ECU)(4000KS) AMM 73-29-00-710-040 Operational Test of the FADEC on the Ground (with
 Engine non Motoring)
 AMM 80-11-10-000-001 Removal of the Pneumatic Starter
 AMM 80-11-10-400-001 Installation of the Pneumatic Starter
 AMM 80-11-20-000-001 Removal of the Starter Shutoff Valve
 AMM 80-11-20-400-001 Installation of the Starter Shutoff Valve

 3. Fault Confirmation
__________________
 A. Test
 (1) Do the operational test of the FADEC 1A and 1B on the ground (with engine non motoring) (Ref. AMM TASK 73-29-00-710-040).
 4. Fault Isolation
_______________
 A. If the fault symptom is identified by the upper ECAM warning START AIR, SAV and the test of the FADEC 1A and 1B gives no CFDS maintenance message:
 - do a check for open or short to ground at pins J9/11, 12 or J10/11, 12 of the harness J9 or J10 between the ECU (4000KS) and the stater shutoff valve.
 (1) If the wiring is not correct:
 - repair the above wiring.
 F 『 EEFF : ALL E ∞∞77-00-00∞∞∞∞∞∞∞∞∞∞Page 298
 E E Nov 01/04 ERE ECES

 F 『 E C F M E E E E 56 E E E (2) If the wiring is correct:

 - disconnect the harness J9 or J10 from the ECU (4000KS) and do a check of the ECU resistance cable between: . pins 11 and 12 (10 to 60 ohms).
 (a) If the resistance values are in the specified limits:
 - do a check for low starter air duct pressure.
 1 If the starter air duct pressure is in the specified limits
_
 (11 PSI < P < 60 PSI):

 - replace the starter shutoff valve (SAV) (Ref. AMM TASK 80-11-20-000-001) (Ref. AMM TASK 80-11-20-400-001)

 - replace the starter (Ref. AMM TASK 80-11-10-000-001) (Ref. AMM TASK 80-11-10-400-001).
 
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 发动机指示(105)