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时间:2011-04-16 10:02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

21.  (13, 14, 15) BRACKET SPACER (6 LOCATIONS) 22.  23.  (113 LOCATIONS) WASHER  12.  (16, 17) BRACKET 
47.  (22, 23) BRACKET 
20.  (19, 20, 21) BRACKET  HOLE NO. 1 

HOLE NO. 30 
46.  (24, 25) BRACKET  HOLE NO. 90  16.  NUT (120 PLACES) 
(55)  HOLE NO. 60  FWD 
FLANGE B BRACKETS B 
____NOTE:  NUMBERS IN PARENTHESIS ARE THE BOLTHOLE LOCATIONS. Figure 402 (Sheet 2) Front Fan Case Installation  L-A2958 

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 72-33-01
 ALL  ú ú N02 Page 407 ú Jun 10/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES /MAINTENANCE MANUAL ////////////////////////
HOIST
PWA 85677 HANDLING BRACKET
FLANGE A 
L-A0555 MOUNTING PAD25. 
BOLT (2 LOCATIONS) 26.  FRONT FAN CASE 24. 
FLANGE A  C  FWD  L-A3500 
FLANGE A1  FRONT FAN CASE24. 
FLANGE B 
C  FWD  0987 L-A3777 
Figure 402 (Sheet 3) Front Fan Case Installation 

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 72-33-01
 ALL  ú ú N01 Page 408 ú Jun 10/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
S 014-003-N00
 (2)  
Remove the inlet cowl (AMM 71-11-01/401).

 S 014-004-N00

 (3)  
Remove the engine accelerometer (AMM 77-31-01/401).

 S 014-005-N00

 (4)  
Remove the electronic engine control (EEC) (AMM 73-21-04/401).

 S 014-040-N00

 (5)  
Remove the supplemental control unit (SCU) (AMM 73-21-15/401).

 S 014-008-N00

 (6)  
Remove the 1st-stage fan blades (AMM 72-31-02/401).


 S 014-009-N00
 CAUTION: MAKE SURE THE WIRE HARNESS DOES NOT TWIST OR BADLY BEND DURING
_______ THE REMOVAL OR THE INSTALLATION. THIS CAN CAUSE DAMAGE TO THE WIRE HARNESS.
 (7)  
Remove the fasteners that attach the wire bundle clamps to the brackets at Flanges A1, B, and B1 on the right side of the engine as follows (Fig. 401):

 (a)  
Remove the bolt (1) and nut (2) that attach the EEC wire bundle clamps to the split bracket (46) at the 2:30 o'clock position.

 (b)  
Remove the bolt (1) and nut (2) that attach the wire bundle
 clamp to the bracket (39) at the 2:30 o'clock position.


 (c)  
ENGINES POST-PW-SB 73-101; Remove the two bolts (1) that attach the wire bundle clamps to the bracket (47) at the 2:15 o'clock position.

 (d)  
Remove the screw (4), washer (5), and nut (6) that attach the wire bundle clamp to the bracket (27) at the 2:00 o'clock position.

 (e)  
Remove the screw (4), washer (5), and nuts (6) that attach the wire bundle clamps and the three ground wires to the split bracket (37) at the 1:45 o'clock position.

 (f)  
Remove the screw (4), washer (5), and nut (6) that attach the wire bundle clamps to the bracket (38) at the 1:45 o'clock position.

 (g)  
ENGINES PRE-PW-SB 72-332;
 Do the steps that follow:
 1) Remove the screws (4), washers (5), and nuts (6) that

 

 attach the wire bundle clamps to the lower holes in the split bracket (10) at the 1:30 o'clock position.
 2)  Remove the bolt (1) and nut (2) that attaches the wire bundle clamps to the upper hole in the split bracket (10) at the 1:30 o'clock position.
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 72-33-01
 ALL  ú ú N03 Page 409 ú Feb 15/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
(h)  ENGINES POST-PW-SB 72-332;
 Do the steps that follow:
 
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