• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-28 13:46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

 L. 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 ∞∞27-93-00∞∞∞∞∞∞∞∞∞∞Page B283
 Aug 01/05R CES


 Loss of Channel 1/2 Yaw CTL from FAC 1/2 to ELAC 1/2
 1. Possible Causes
_______________
 - the DSI 15/18 output discret digital signal of the ELAC 1 and ELAC 2
 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
31-32-00-810-932 Failure of the Discrete Links AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning) ASM 27-92/37
 3. Fault Confirmation
__________________
 A. Test
 (1) Do the BITE test of the EFCS (ground scanning) (Ref. AMM TASK 27-96-00-740-001).
 4. Fault Isolation
_______________
 A. If the BITE test gives the maintenance message:
 ELAC1 OR WIRING FROM FAC1/2 or
 ELAC2 OR WIRING FROM FAC1/2

 - do the trouble shooting procedure (Ref. TASK 31-32-00-810-932) related to the DSI 15/18 output discret digital signal of the ELAC 1 and ELAC 2 (Ref. ASM 27-92/37).
 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 ∞∞27-93-00∞∞∞∞∞∞∞∞∞∞Page B284
 Aug 01/05R
 CES R False ELAC Warning due to Faulty Yellow Hydraulic Pressure Switch R


 1. Possible Causes
_______________
R
 - FWC-1 (1WW1)

 - PRESS SW-FLT CTL, Y (3151GN)

 - wiring from the FWC 1 to the pressure switch


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning) AMM 29-10-00-200-008 Check Nitrogen Charge Pressure on Hydraulic Power
 Accumulators AMM 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground
 Power Supply AMM 29-10-00-864-003 Depressurize the Blue Hydraulic System AMM 29-23-00-863-001 Pressurize the Green Hydraulic System from the Yellow
 Hydraulic System through the PTU with the Electric Pump AMM 29-23-00-864-001 Depressurize the Green and Yellow Hydraulic Systems after Operation of the PTU AMM 29-24-00-863-001 Pressurize the Yellow Hydraulic System with the
 Electric Pump AMM 29-24-00-864-001 Depressurize the Yellow Hydraulic System AMM 29-32-12-000-003 Removal of the System Pressure Switch (3151GN) AMM 29-32-12-400-003 Installation of the System Pressure Switch (3151GN) AMM 31-53-34-000-001 Removal of the Flight Warning Computer (FWC)
 (1WW1,1WW2) AMM 31-53-34-400-001 Installation of the Flight Warning Computer (FWC) (1WW1,1WW2) ASM 29-32/01
 3. Fault Confirmation
__________________
 A. Job Set-Up
 (1) Pressurize the aircraft hydraulic systems (Ref. AMM TASK 29-10-00-863-003), (Ref. AMM TASK 29-23-00-863-001) and (Ref. AMM TASK 29-24-00-863-001).
 「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 ∞∞27-93-00∞∞∞∞∞∞∞∞∞∞Page B285
 Aug 01/05 CES (2) On the center pedestal, on the ECAM control panel:


 Push the F/CTL key, the F/CTL page comes into view. R
 (3) For the ELAC1, on the overhead panel 24VU, release the FLT CTL/ELAC2 pushbutton switch (on this pushbutton switch, the OFF legend comes on).

 (4) For the ELAC2, on the overhead panel 23VU, release the FLT CTL/ELAC1 pushbutton switch (on this pushbutton switch, the OFF legend comes on).


R
R B. Put the aircraft back to its initial configuration.
 (1) Depressurize the aircraft hydraulic systems (Ref. AMM TASK 29-10-00-864-003), (Ref. AMM TASK 29-23-00-864-001) and (Ref. AMM TASK 29-24-00-864-001).

 (2) Push the FLT CTL/ELAC1 pushbutton switch or FLT CTL/ELAC2 pushbutton switch that you released before (on this pushbutton switch, the OFF legend goes off).


 4. Fault Isolation
_______________
R
R A. If the ELAC 1 FAULT or ELAC 2 FAULT warning goes out view when the R hydraulic systems are pressurized:
 - do the BITE test of the EFCS (ground scanning) (Ref. AMM TASK 27-96-00-740-001).
 (1) If the test gives a maintenance message related to the Yellow hydraulic pressure switch with a F/CTL maintenance status:
 
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 飞行操纵 3(87)