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时间:2011-04-16 10:09来源:蓝天飞行翻译 作者:航空
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SEEJ
SEE K

W3 HARNESS 
W5 HARNESS 
W3 HARNESS 
CLAMP 
CLAMP  W3 HARNESS 
CLAMP 
BOLT  W3 HARNESS  CLAMP 
BOLT 
BOLT 
W5 HARNESS 
W5 HARNESS  CLAMP  CLAMP 
BOLT 
BOLT 
CLAMP 
BOLT 
W3 HARNESS  J 
BOLT 

LA9297 (0000) 
EEC Wiring Harness W3 Installation 
Figure 401 (Sheet 5) 

E44581
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 73-21-07
 ALL  ú ú N01A Page 407 ú Oct 10/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES /MAINTENANCE MANUAL ////////////////////////
W3P5 W5P5
W3P1 
W5P6 
SEE  M  L 
NUTS 
W3 HARNESS  W5 HARNESS 
BOLT  CLAMP  BOLT  M CLAMP  FWD  TUBE HARNESS SUPPORT EEC WIRING 
LA9298 (0000) 
Figure 401 (Sheet 6) EEC Wiring Harness W3 Installation 

E44583
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 73-21-07
 ALL  ú ú N01A Page 408 ú Oct 10/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
SEE  P 
W3P1 
W5P6 
MAIN 
GEARBOX 
W3P18  BRACKET 
SEE  O 
N  W3,W5 
HARNESS 
MAIN GEARBOX 
OIL PRESSURE 
TUBE 
CLAMP 
BOLT 
FWD 
BOLTS 
NUT 
BOLT 
NUTS 

GROUND STRAP 
W3,W5 
HARNESS 

LA9299 (0000) 
EEC Wiring Harness W3 Installation 
Figure 401 (Sheet 7) 

E44585
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 73-21-07
 ALL  ú ú N01A Page 409 ú Oct 10/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
D. Procedure
 S 864-041-N00
 (1)  
For the applicable engine, open this circuit breaker and install the DO-NOT-CLOSE tag:

 (a)  
P6 Main Power Distribution Panel
 1) 6F15 ENG 1 PERF SOL PWR A
 2) 6F16 ENG 1 PERF SOL PWR B
 3) 6G15 SCU ALT PWR ENG 1
 4) 6G23 ENG SCU 1
 5) 6E15 ENG 2 PERF SOL PWR A
 6) 6E16 ENG 2 PERF SOL PWR B
 7) 6G16 SCU ALT PWR ENG 2
 8) 6G24 ENG SCU 2
 9) 6D15 ENG 3 PERF SOL PWR A
 10) 6D16 ENG 3 PERF SOL PWR B
 11) 6G17 SCU ALT PWR ENG 3
 12) 6G25 ENG SCU 3
 13) 6C15 ENG 4 PERF SOL PWR A
 14) 6C16 ENG 4 PERF SOL PWR B

 

 15) 6G18 SCU ALT PWR ENG 4
 16) 6G26 ENG SCU 4

 S 014-040-N00
 (2)  Open the left fan cowl panel (AMM 71-11-04/201).
 S 044-039-N00
 WARNING: DO THE THRUST REVERSER DEACTIVATION PROCEDURE TO PREVENT THE
_______
 OPERATION OF THE THRUST REVERSER. THE ACCIDENTAL OPERATION OF
 THE THRUST REVERSER CAN CAUSE INJURIES TO PERSONS OR DAMAGE TO
 EQUIPMENT.

 (3)  
Do this procedure: Thrust Deactivation for Ground Maintenance
 (AMM 78-31-00/201).


 (4)  
Open the left core cowl panel (AMM 71-11-06/201).


 S 014-038-N00
 S 014-037-N00
 WARNING: OBEY THE INSTRUCTIONS IN AMM 78-31-00/201 WHEN YOU OPEN THE
_______
 THRUST REVERSERS. IF YOU DO NOT OBEY THE INSTRUCTIONS,
 INJURIES TO PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR.

 (5)  Open the left thrust reverser (AMM 78-31-00/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 
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