F 『
E C F M E
E E
E 56-5B E
E E
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
**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 71-51-43-010-058
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 44071-51-43
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. 404/TASK 71-51-43-991-303, 405/TASK 71-51-43-991-304)
Subtask 71-51-43-020-055
A. Removal of the IDG Control and Anti-Ice 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 connectors 401VC-A, 404VC-A and 405VC-A from the pylon junction box. (Ref. Fig. 404/TASK 71-51-43-991-303)
(2) Disconnect the electrical connector 4005VC-A from the connector on
the left harness at station 174. R R BEFORE SPIB NO. CFM02255MW1 R
(3) Open the flip-lock clamps (10), (20), (25) and (55) that attach the harness (5) to the engine brackets.
(4) Open the line blocks (15), (30), and (35) attached to the brackets at station 158.
CONFIG-1
(5) Open the line block (40) that attaches the harness (5) to the bracket at station 167.
CONFIG-2
(Ref. Fig. 404/TASK 71-51-43-991-303)
(Detail B)
(6) Remove the bolt (45) that attaches the clamps (50) and (75) to the bracket at station 167.
F 『 EEFF : ALL E Page 44171-51-43
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
R R Upper Right Fan Zone Electrical Harnesses Figure 404/TASK 71-51-43-991-303- 13 (SHEET 1)
F EEFF : E E ECES ALL 『E 71-51-43EEE Page 442 Feb 01/04
R R Upper Right Fan Zone Electrical Harnesses Figure 404/TASK 71-51-43-991-303- 23 (SHEET 2)
F EEFF : E E ECES ALL 『E 71-51-43EEE Page 443 Feb 01/04
R R Upper Right Fan Zone Electrical Harnesses Figure 404/TASK 71-51-43-991-303- 33 (SHEET 3)
F EEFF : E E ECES ALL 『E 71-51-43EEE Page 444 Feb 01/04
F 『
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(26)
