• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-27 12:57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

 **ON A/C ALL
 122VU ELEC/GCU/2 2XU2 T27 122VU ELEC/GCU/1 2XU1 T26 122VU ANTI ICE/WINDOWS/R 4DG2 W14 122VU ANTI ICE/WINDOWS/L 4DG1 X14 122VU ANTI ICE/PROBES/PHC/3 2DA3 Y16 122VU ANTI ICE/PROBES/2/TAT 1DA2 Y15 122VU ANTI ICE/PROBES/2/PITOT 3DA2 Y14 122VU ANTI ICE/PROBES/2/AOA 4DA2 Y13 122VU ANTI ICE/PROBES/2/PHC 2DA2 Y12 122VU ANTI ICE/PROBES/2/STATIC 5DA2 Y11 122VU ANTI ICE/PROBES/3/PITOT 3DA3 Z16 122VU ANTI ICE/PROBES/3/AOA 4DA3 Z15 122VU ANTI ICE/PROBES/3/STATIC 5DA3 Z14 122VU ANTI ICE/PROBES/1/STATIC 5DA1 Z13 122VU ANTI ICE/PROBES/1/TAT 1DA1 Z12
R  **ON A/C 001-049, 051-052, 054-056, 058-059, 061-099, 101-101, 103-149,
R  151-199, 201-299, 301-399, 401-499, Post SB 30-1037 For A/C 001-049,051-052,054-056,
 122VU ANTI ICE/RAIN/RPLNT/F/O  1DB2 W11
 F 『 EEFF : ALL E Page 46771-52-43
 E E Aug 01/05 E E ECES E

 F 『
 E C F M E
 E E
 E 56-5B E
 E E


 **ON A/C ALL
 4. Procedure
_________
R **ON A/C 001-049, 051-099, 101-149, 151-155, 157-199, 201-299, 301-399, R 401-499,
 Subtask 71-52-43-420-057
 A. Installation of the Vibration Sensor Harness Assembly (4206KS) (Ref. Fig. 403/TASK 71-52-43-991-306)
 NOTE : When using fiberglass clamps on the engine core harnesses, do as
____ follows: Wrap fiberglass adhesive tape (Material No. CP2208) around the harness(es) to make sure that the clamps do not move when they are installed. Wrap only the locations where the clamps are being installed.
 NOTE : Before you tighten the clamps, adjust the wire harness to get
____ maximum clearance between the harness and the other structures on the engine. Make sure that the harness will not touch other structures.
 (1) Remove the blanking caps from the electrical connectors.

 (2) Put the harness 4206KS in position on the engine.

 (3) Connect the electrical connector 457VC-A to the core junction box.

 (4) Put the two clamps (10) on the harness 4206KS. Attach the clamps to the pylon with the bolts (5).

 (5) Put the harness into the clamp (20) attached to the bracket at station 233. Make sure the reference marker is correctly aligned. Install the bolt (15).


 NOTE : The Installation Reference Markers are fiberglass tape on the
____
 harnesses.

 (6) Put the harness into the clamp (35) and install the bolt (15).

 (7) Put the harness into the clamp (40) attached to the bracket at station 233. Install the bolt (15).

 (8) Connect the electrical connector 4003EV-A to the TRF Vibration Sensor (4003EV).


 F 『 EEFF : ALL E Page 46871-52-43
 E E Aug 01/05 E E ECES E

 F  『
 E  C F M  E
 E  E
 E  56-5B  E
 E  E


 (9) Make sure that the harness 4206KS is correctly installed on the engine.
 (10) TORQUE the bolts (15) to between 20 and 25 lbf.in (0.22 and 0.28 m.daN).
 **ON A/C 156-156,
 Subtask 71-52-43-420-057-A
 A. Installation of the Vibration Sensor Harness Assembly (4206KS)
 (Ref. Fig. 403A/TASK 71-52-43-991-306-A)

 NOTE : When using fiberglass clamps on the engine core harnesses, do as
____ follows: Wrap fiberglass adhesive tape (Material No. CP2208) around the harness(es) to make sure that the clamps do not move when they are installed. Wrap only the locations where the clamps are being installed.
 NOTE : Before you tighten the clamps, adjust the wire harness to get
____ maximum clearance between the harness and the other structures on the engine. Make sure that the harness will not touch other structures.
 (1) Remove the blanking caps from the electrical connectors.

 (2) Put the harness 4206KS in position on the engine.

 (3) Connect the electrical connector 457VC-A to the core junction box.

 (4) Put the two clamps (10) on the harness 4206KS. Attach the clamps to the pylon with the bolts (5).

 (5) Put the harness 4206KS into the thermal blanket (30) and (35), as required.

 (6) Use a new piece of lacing and tying tape (Material No. CP8003) at each eyelet set. Tie the lacing and tying tape (Material No. CP8003) in a square knot.


 NOTE : Do not tighten the lacing and tying tape (Material No. CP8003)
____ too much. There must be a clearance between the thermal blanket flaps.
 F 『R EEFF : ALL E Page 46971-52-43
 E E May 01/05 E E ECES E

 F 『
 E C F M E
 E E
 E 56-5B E
 E E
 (7) Put the harness into the clamp (20) attached to the bracket at station 233. Make sure the reference marker is correctly aligned. Install the bolt (15).
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:A320飞机维护手册 AMM 动力装置 POWER PLANT 2(90)