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时间:2011-03-27 12:57来源:蓝天飞行翻译 作者:航空
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 (3) Make sure that the access platform is in position.


 Subtask 71-51-43-010-073
 B. Get Access
 (1) Make sure that the fan cowl doors are open: (Ref. TASK 71-13-00-010-040) FOR 1000EM1 437AL, 438AR FOR 1000EM2 447AL, 448AR
 Subtask 71-51-43-865-078
 C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU ENGINE/1 AND 2/IGN/SYS A 1JH A03 49VU ANTI ICE/PROBES/AOA/1 4DA1 D04 49VU ANTI ICE/PROBES/PITOT/1 3DA1 D02 49VU COM/CVR/SPLY 2RK E14 49VU COM/CVR/CTL 4RK E13
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,
 49VU ANTI ICE/RAIN/RPLNT/CAPT 1DB1 D01
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 121VU RCDR/DFDR 7TU K16 121VU HYDRAULIC/HYD POWER/Y 3803GX N30 122VU ANTI ICE/WINDOWS/R 4DG2 W14 122VU ANTI ICE/WINDOWS/L 4DG1 X14 122VU ANTI ICE/PROBES/2/PITOT 3DA2 Y14 122VU ANTI ICE/PROBES/2/AOA 4DA2 Y13 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
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
 **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 2WE1 Q44 121VU ENGINE/ENG1 AND 2 FIRE EXTIG/BTL1/SQUIB/A 1WE1 Q43 121VU ENGINE/ENG1/FIRE DET/LOOP B 8WD1 Q38 121VU ENGINE/ENG1/FADEC B/AND EIU 1 4KS1 R41 122VU ELEC/GCU/1 2XU1 T26
 FOR 1000EM2 49VU ENGINE/2/FIRE DET/LOOP B 8WD2 A07 49VU ENGINE/2/FADEC A/AND EIU 2 2KS2 A05
 121VU ENGINE/IGN/ENG2/SYS B 3JH2 P42 121VU ENGINE/IGN/ENG2/SYS A BAT 2JH2 P40 121VU ENGINE/ENG1 AND 2 FIRE EXTIG/BTL2/SQUIB/B 2WE2 Q42 121VU ENGINE/ENG1 AND 2 FIRE EXTIG/BTL2/SQUIB/A 1WE2 Q41 121VU ENGINE/ENG2/FADEC B 4KS2 Q40
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 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU ENGINE/ENG2/FIRE DET/LOOP A 7WD2 Q39 122VU ELEC/GCU/2 2XU2 T27
 4. Procedure
_________
 (Ref. Fig. 411/TASK 71-51-43-991-306) Subtask 71-51-43-420-059
 A. Installation of the ECU (Channel A) to Thrust Reverser Junction Box
 Harness (4213KS)

 NOTE : For the recommended procedure for the installation of the wire
____
 harness (Ref. TASK 70-60-00-910-041).

 NOTE : To tighten the flip-lock clamps and line blocks, turn the captive
____ screws or bolts 1/4 turn clockwise to engage the cam nuts.
 (1) Remove the protective covers from the electrical connectors.

 (2) Put the electrical harness (5) in position on the engine.

 (3) Connect the electrical connector 4007VC-A to the harness junction box.

 (4) Put the harness (5) into the rubber supports of the line blocks (10),

 (15) and (20).

 (5) If removed, put the rubber supports in the line blocks (10), (15) and (20).

 (6) Connect the electrical connector 4000KS-J5 to the ECU. NOTE : The wire harness for connectors 4000KS-J1 and 4000KS-J5 may

____
 touch as shown on
 (Ref. Fig. 411/TASK 71-51-43-991-306)


 (7) Make sure that the harness (5) is correctly installed on the engine. BEFORE SPIB NO. CFM02255MW1


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 (8) Close the line blocks (10), (15) and (20) and tighten the captive
 
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