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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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 49VU ANTI ICE/RAIN/RPLNT/CAPT  1DB1 D01
 **ON A/C ALL
 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
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 -------------------------------------------------------------------------------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 71-51-43-010-066
 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.

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 4. Procedure
_________
 (Ref. Fig. 412/TASK 71-51-43-991-316)
 Subtask 71-51-43-020-063
 A. Removal of the ECU (Channel B) to Thrust Reverser Junction Box Harness (4214KS).
 NOTE : To open the flip-lock clamps and line blocks, turn the captive
____ screws or 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 4006VC-A from the harness junction box.

 CONFIG-1

 (2) Open the line block (10) that attaches the harness (5) to the bracket at station 167. If necessary remove the rubber support from the line block (10).

 CONFIG-2

 (3) Remove the bolt (20) that attaches the clamps (15) and (25) to the bracket at station 167. Remove the clamp (25) from the harness (5).

 (4) Leave the clamp (15) on the harness 4215KS and loosely install the bolt (20).

 END CONFIG-2

 (5) Open the line blocks (30) and (35) that attach the harness (5) to the brackets.

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


 (30) and (35).
 (7) Remove the harness (5) from the rubber supports. R R BEFORE SPIB NO. CFM02255MW1 R
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 INTENTIONALLY BLANK

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R ECU Channel B to Thrust Reverser Junction Box Harness R Figure 412/TASK 71-51-43-991-316- 12 (SHEET 1)
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R ECU Channel B to Thrust Reverser Junction Box Harness R Figure 412/TASK 71-51-43-991-316- 22 (SHEET 2)
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