• 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

 (4) Remove the bolt (15) and the clamp (20) that attach the harness 4204KS to the bracket at station 233.

 (5) Remove the two bolts (15) and the two clamps (25) that attach the harness 4204KS to the brackets between stations 233 and 239.

 (6) Cut the lockwire and remove the screws (75) and the clamp (45) that attach the harness 4204KS to the fire detector element 4001WD1-A.

 (7) Remove the nut (55) that attaches the wire (50) to terminal C of the fire detector.

 (8) Remove the nut (60) that attaches the wire (65) to terminal A of the fire detector.

 (9) Remove the nut (95), the washers (90), the lockwasher (85), and the bolt (80) that attach the ground wire (70) to the bracket.


 (10) Remove the harness assembly 4204KS from the engine.

 (11) Put blanking caps on the electrical connectors.


 **ON A/C 156-156,
 Subtask 71-52-43-020-055-A
 A. Removal of the Channel A Fire Detector Harness Assembly (4204KS)
 (Ref. Fig. 401A/TASK 71-52-43-991-303-A)

 (1) Disconnect the electrical connector 452VC-A from the core junction box.

 (2) Remove the two bolts (5) and open the two clamps (10) that attach the harnesses to the pylon. Remove the harness 4204KS from the clamps. Install the bolt (5) and tighten it with your hand.

 (3) Remove the bolt (15) and open the clamp (40) that attaches the harness assemblies to the bracket at station 233. Remove harness 4204KS from the clamp. Install the bolt (15) and tighten it with your hand.


 F 『 EEFF : ALL E Page 40871-52-43
 E E May 01/05 ERE
ECES E E 56-5B E E E (4) Remove the bolt (15) and the clamp (20) that attach the harness 4204KS to the bracket at station 233.

 F  『
 E  C F M  E
 E  E

 

 (5) Remove the two bolts (15) and the two clamps (25) that attach the harness 4204KS to the brackets between stations 233 and 239.

 (6) Cut the lockwire and remove the screws (75) and the clamp (45) that attach the harness 4204KS to the fire detector element 4001WD1-A.

 (7) Remove the nut (55) that attaches the wire (50) to terminal C of the fire detector.

 (8) Remove the nut (60) that attaches the wire (65) to terminal A of the fire detector.

 (9) Remove the nut (95), the washers (90), the lockwasher (85), and the bolt (80) that attach the ground wire (70) to the bracket.


 (10) Cut the lacing tape that attaches the thermal blanket (30) and remove the harness from the thermal blanket (30).

 (11) If necessary, remove the thermal blanket (35).

 (12) Remove the harness assembly 4204KS from the engine.

 (13) Put blanking caps on the electrical connectors.


 F 『 EEFF : 156-156, E Page 40971-52-43
 E E May 01/05 ERE
ECES E F 『 E C F M E E E E 56-5B E

 

R Fire Detector Channel A Wire Harness Figure 401A/TASK 71-52-43-991-303-A12 (SHEET 1)
 F 『 EEFF : 156-156, E Page 41071-52-43
 E E Nov 01/03 E E ECES E F 『 E C F M E E E E 56-5B E

 

R Fire Detector Channel A Wire Harness Figure 401A/TASK 71-52-43-991-303-A22 (SHEET 2)
 F 『 EEFF : 156-156, E Page 41171-52-43
 E E Nov 01/03 E E ECES E

 F 『
 E C F M E
 E E
 E 56-5B E
 E E


 **ON A/C ALL
 TASK 71-52-43-400-042
 Installation of the Core Fire Detector Channel A Wire Harness (4204KS)
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific lint-free cloth
 No specific warning notice
 No specific access platform 1.5 m (4 ft. 11 in.)

R No specific Torque Wrench : range 5.00 to 35.00 lbf.in R (0.05 to 0.40 m.daN) R
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. CP1011 USA MIL-T-81533
 trichloroethane (Ref. 70-30-00)
 Material No. CP2208 USA 3M-361
 fiberglass adhesive tape (Ref. 70-30-00)
 Material No. CP8001 *
 lockwire 0.032 in. (0.8127 mm) (Ref. 70-30-00)
 Material No. CP8002 *
 lockwire 0.032 in. (0.8127 mm) (Ref. 70-30-00)
 Material No. CP8003 *
 lacing and tying tape (Ref. 70-30-00)


 
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(74)