• 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
 123VU Y HYD/ELEC/PUMP  3802GX  AB06
 123VU Y HYD/ELEC/ELEC PUMP/NORM  3801GX  AB03
 FOR 1000EM1
 49VU ENGINE/1/FIRE DET/LOOP A  7WD1  A06
 49VU ENGINE/1/FADEC A/AND EIU 1  2KS1  A04
 121VU ENGINE/IGN/ENG1/SYS B  3JH1  P41
 121VU ENGINE/IGN/ENG1/SYS A BAT  2JH1  P39

 121VU ENGINE/ENG1 AND 2 FIRE EXTIG/BTL1/SQUIB/B 121VU ENGINE/ENG1 AND 2 FIRE EXTIG/BTL1/SQUIB/A 121VU ENGINE/ENG1/FIRE DET/LOOP B 121VU ENGINE/ENG1/FADEC B/AND EIU 1 122VU ELEC/GCU/1 FOR 1000EM2 49VU ENGINE/2/FIRE DET/LOOP B 49VU ENGINE/2/FADEC A/AND EIU 2 121VU ENGINE/IGN/ENG2/SYS B 121VU ENGINE/IGN/ENG2/SYS A BAT 121VU ENGINE/ENG1 AND 2 FIRE EXTIG/BTL2/SQUIB/B 121VU ENGINE/ENG1 AND 2 FIRE EXTIG/BTL2/SQUIB/A 121VU ENGINE/ENG2/FADEC B 121VU ENGINE/ENG2/FIRE DET/LOOP A 122VU ELEC/GCU/2  2WE1 1WE1 8WD1 4KS1 2XU1 8WD2 2KS2 3JH2 2JH2 2WE2 1WE2 4KS2 7WD2 2XU2  Q44Q43Q38R41T26A07A05P42P40Q42Q41Q40Q39T27
 Subtask 71-51-43-010-063
 C. Get Access
 (1) Open the fan cowls: (Ref. TASK 71-13-00-010-040) FOR 1000EM1 437AL, 438AR FOR 1000EM2 447AL, 448AR
 (2) Put the access platform in position.

 F 『 EEFF : ALL E Page A44271-51-43
 E E May 01/05 ERE
ECES E

 F 『
 E C F M E
 E E
 E 56-5B E
 E E


 4. Procedure
_________
 (Ref. Fig. 413/TASK 71-51-43-991-307, 414/TASK 71-51-43-991-308, 415/TASK 71-51-43-991-309)
 Subtask 71-51-43-020-060
 A. Removal of the Left Side Harness
 NOTE : To open the flip-lock clamps and line blocks, turn the captive
____ screws or captive bolts 1/4 turn counterclockwise to disengage the cam nuts.
R  NOTE : Loosely attach the clamp(s), anti-rotation lug(s) if applicable,____
R  and bolt(s) to the brackets from which they were removed to make
R  it easier for installation.
 (1) Disconnect the electrical connector 447VC-A from the pylon junction box. (Ref. Fig. 413/TASK 71-51-43-991-307)

 (2) Disconnect the electrical connector 4005VC from the electrical connector 4005VC-A.

 (3) Open the line blocks (10) that attach the harness (5) to the brackets at station 167.

 (4) If necessary, remove the rubber supports from the line blocks (10).

 (5) Remove the harness (5) from the rubber supports.

 (6) Open the line block (10) that attaches the harness to the bracket at station 174, at the top left side of the engine. (Ref. Fig. 414/TASK 71-51-43-991-308)


R R BEFORE SPIB NO. CFM02255MW1. R
 (7) Open the line block (15) that attaches the harness (5) to the bracket at station 176.

 (8) Open the line block (20) that attaches the harness (5) to the brackets at station 185.


 F 『 EEFF : ALL E Page A44371-51-43
 E E Feb 01/04 E E ECES E F 『 E C F M E E E E 56-5B E

 

 Upper Right Fan Zone Electrical Harness Figure 413/TASK 71-51-43-991-307
 F EEFF : E ER ECES  ALL  『E 71-51-43EE E Page A444 Feb 01/04


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


 INTENTIONALLY BLANK

 F 『R E E Page A44571-51-43
 E E Feb 01/04 E E ECES E F 『 E C F M E E E E 56-5B E F 『 E C F M E E E E 56-5B E F 『 E C F M E E E E 56-5B E F 『 E C F M E E E E 56-5B E F 『 E C F M E E E E 56-5B E F 『 E C F M E E E E 56-5B E (9) If necessary, remove the rubber supports from the line blocks (10),

 

R R  Upper Left Fan Zone Electrical Harness Figure 414/TASK 71-51-43-991-308- 14 (SHEET 1)
 F EEFF : E E ECES  ALL  『E 71-51-43EEE Page A446 Feb 01/04

 


R R  Upper Left Fan Zone Electrical Harness Figure 414/TASK 71-51-43-991-308- 24 (SHEET 2)
 F EEFF : E E ECES  ALL  『E 71-51-43EEE Page A447 Feb 01/04

 


R R  Upper Left Fan Zone Electrical Harness Figure 414/TASK 71-51-43-991-308- 34 (SHEET 3)
 F EEFF : E E ECES  ALL  『E 71-51-43EEE Page A448 Feb 01/04

 


R R  Upper Left Fan Zone Electrical Harness Figure 414/TASK 71-51-43-991-308- 44 (SHEET 4)
 F EEFF : E E ECES  ALL  『E 71-51-43EEE Page A449 Feb 01/04

 


R R  Lower Left Fan Zone Electrical Harness Figure 415/TASK 71-51-43-991-309- 12 (SHEET 1)
 F EEFF : E E ECES  ALL  『E 71-51-43EEE Page A450 Feb 01/04

 


R R  Lower Left Fan Zone Electrical Harness Figure 415/TASK 71-51-43-991-309- 22 (SHEET 2)
 
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(53)