• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-29 14:30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

______________________ R Not Applicable R 3. Fault Confirmation
__________________ R A. Not applicable, the Bleed Bias System is not installed. R 4. Fault Isolation
_______________
R A. On Channel 2B:
R Ignore the BLD SNSR, J15, ECU message. No maintenance action is required
R Ignore the BLD SNSR, J15, ECU* message. No maintenance action is
R required.

 F 『 EEFF : ALL E ∞∞75-30-00∞∞∞∞∞∞∞∞∞∞Page 252
 E E Aug 01/99 E E ECES
E

 F 『
 E C F M E
 E E
 E 56 E
 E E


R TASK 75-30-00-810-841
R Bleed Bias System on Engine 1
R 1. Possible Causes
_______________
R - Ignore the VTURI, BLD SNSR, ECU message. No maintenance action is required R - Ignore the VTURI, BLD SNSR, ECU* message. No maintenance action is R required
R 2. Job Set-up Information
______________________
R Not Applicable
R 3. Fault Confirmation
__________________
R A. Not applicable, the Bleed Bias System is not installed.
R 4. Fault Isolation
_______________
R A. On Channel 1B:
R Ignore the VTURI, BLD SNSR, ECU message. No maintenance action is
R required Ignore the VTURI, BLD SNSR, ECU* message. No maintenance action
R is required.

 F 『 EEFF : ALL E ∞∞75-30-00∞∞∞∞∞∞∞∞∞∞Page 253
 E E Aug 01/99 E E ECES
E

 F 『
 E C F M E
 E E
 E 56 E
 E E


R TASK 75-30-00-810-842
R Bleed Bias System on Engine 2
R 1. Possible Causes
_______________
R - Ignore the VTURI, BLD SNSR, ECU message. No maintenance action is required R - Ignore the VTURI, BLD SNSR, ECU* message. No maintenance action is R required
R 2. Job Set-up Information
______________________
R Not Applicable
R 3. Fault Confirmation
__________________
R A. Not applicable, the Bleed Bias System is not installed.
R 4. Fault Isolation
_______________
R A. On Channel 2B:
R Ignore the VTURI, BLD SNSR, ECU message. No maintenance action is
R required Ignore the VTURI, BLD SNSR, ECU* message. No maintenance action
R is required.

 F 『 EEFF : ALL E ∞∞75-30-00∞∞∞∞∞∞∞∞∞∞Page 254
 E E Aug 01/99 E E ECES
E

 F 『
 E C F M E
 E E
 E 56 E
 E E
 VARIABLE STATOR VANE SYSTEM (VSV) - FAULT ISOLATION PROCEDURES

______________________________________________________________
 TASK 75-32-00-810-801
 Failure of the VSV System on Engine 1
 1. Possible Causes
_______________
 - harness J7

 - Hydromechanical Unit (HMU)

 - ECU (4000KS)


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 73-21-10-000-002 Removal of the Hydromechanical Unit (HMU)
 AMM 73-21-10-400-002 Installation of the Hydromechanical Unit (HMU)
 AMM 73-21-50-000-040 Removal of the HJ7 Harness
 AMM 73-21-50-400-040 Installation of the HJ7 Harness

R 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 R (ECU)(4000KS) AMM 73-29-00-710-040 Operational Test of the FADEC on the ground (with Engine Motoring) ASM 73-25/18
 3. Fault Confirmation
__________________
 A. Test
 (1) Do the operational test of the FADEC 1A on the ground (with engine motoring) (Ref. AMM TASK 73-29-00-710-040).
 4. Fault Isolation
_______________
 A. If the test gives the maintenance message VSV ACT, HMU:
 - manually operate the VSV system and make sure that the system moves smoothly and freely.
 (1) If the fault continues:

 - do a check for line to line short circuit of the harness J7 between the ECU (4000KS) and the VSV torque-motor (Ref. ASM 73-25/18).

 (2) If the fault continues:


 - disconnect the cable J7 from the ECU and do a check of the ECU resistance between: . pins 25 and 26 (17 to 23 Ohms).
 F 『 EEFF : ALL E ∞∞75-32-00∞∞∞∞∞∞∞∞∞∞Page 201
 E E May 01/04 E E ECES
E E 56 E E E

 F  『
 E  C F M  E
 E  E
 
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 大气 AIR(71)