• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-28 13:42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 ground scanning gives the maintenance message: R B ELEV POS XDCR 34CE4 COM E1/S1 : USE STBY XDCR

 - refer to Para. Fault Isolation.

 (b) If the ground scanning gives at least two maintenance messages of the list below: L B ELEV POS XDCR 34CE3 COM E1/S1 : USE STBY XDCR R B ELEV POS XDCR 34CE4 COM E1/S1 : USE STBY XDCR THS ACTR XDCR2 9CE

 

 

 

 - do this trouble shooting procedure (Ref. TASK 27-90-00-810-819).
 4. Fault Isolation
_______________
 A. If the test gives the maintenance message:
 R B ELEV POS XDCR 34CE4 COM E1/S1 : USE STBY XDCR

 - deactivate the defective RVDT and connect the spare RVDT (Ref. AMM TASK 27-34-00-040-001) and (Ref. AMM TASK 27-34-00-440-001).
 (1) If the fault continues:

 - do the trouble shooting procedure (Ref. TASK 31-32-00-810-933) related to the ANI 2-X analog input signal of the ELAC COM and SEC COM (Ref. ASM 27-93/07) and (Ref. ASM 27-94/07).

 (2) If the fault continues:


 - replace the SERVO CTL-R ELEVATOR, OUTBD B (34CE4) (Ref. AMM TASK 27-34-51-000-001) and (Ref. AMM TASK 27-34-51-400-001).
 NOTE : The resistance of primary and secondary windings must be
____
 between 30 ohms and 500 ohms.

 (3) If the fault continues:
 (a) Do a check of the wiring of the POS XDCR COM SPLY signal from the servocontrol (34CE4) to the first terminal block (Ref. ASM 27-93/07):

 - if there is continuity, see Para. (b)

 - if there is no continuity, repair the above wiring.

 

 (b) Do a check and repair the wiring of the POS XDCR COM V1, V2 signals from the servocontrol (34CE4) to the first terminal block (Ref. ASM 27-93/07).


 B. Do the tests 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 ∞∞27-30-00∞∞∞∞∞∞∞∞∞∞Page 245
 Aug 01/00R
 CES  Loss of the Signal of the Right Blue Elevator-Servocontrol Position-Transducer by the SEC 1

 


 1. Possible Causes
_______________
 - SEC-1 (1CE1)

 - wiring of the POS XDCR COM (ANI 2-2) signal from the SEC 1 (1CE1) to the first terminal block


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-90-00-810-817 Loss of the ACS1 Signal of the SEC1 COM Side
 AMM 27-94-34-000-001 Removal of the SEC (1CE1,1CE2,1CE3)
 AMM 27-94-34-400-001 Installation of the SEC (1CE1,1CE2,1CE3)
 AMM 27-96-00-710-020 Operational Test of the Side Stick Assembly

 (Activation for the BITE Test)
 AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning)
 ASM 27-94/07

 3. Fault Confirmation
__________________
 A. Test
 (1) Do the operational test of the side stick assembly (Activation for the BITE test) (Ref. AMM TASK 27-96-00-710-020).
 NOTE : Before you start the operational test procedure, release the
____ FLT CTL/ELAC 1 pushbutton switch (on this pushbutton switch, the OFF legend comes on).
 (2) Do the BITE test of the EFCS (ground scanning) (Ref. AMM TASK 27-96-00-740-001).
 (a) If the ground scanning gives the maintenance message: SEC1 OR WIRING FROM R B ELEV POS XDCR 34CE4

 - refer to Para. Fault Isolation.

 (b) If the ground scanning gives at least two maintenance messages of the list below: SEC1 COM OR WIRING FROM THS ACTR XDCR2 9CE SEC1 OR WIRING FROM L B ELEV POS XDCR 34CE3 SEC1 OR WIRING FROM R B ELEV POS XDCR 34CE4


 - do this trouble shooting procedure (Ref. TASK 27-90-00-810-817).
 「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 ∞∞27-30-00∞∞∞∞∞∞∞∞∞∞Page 246
 Aug 01/00R CES


 4. Fault Isolation
_______________


 A. If the test gives the maintenance message: SEC1 OR WIRING FROM R B ELEV POS XDCR 34CE4
 - replace the SEC-1 (1CE1) (Ref. AMM TASK 27-94-34-000-001) and (Ref. AMM TASK 27-94-34-400-001).
 (1) If the fault continues:
 - do a check and repair the wiring of the POS XDCR COM (ANI 2-2) signal from the SEC 1 (1CE1) to the first terminal block (Ref. ASM 27-94/07).
 B. Do the tests 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 ∞∞27-30-00∞∞∞∞∞∞∞∞∞∞Page 247
 
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 1(53)