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时间:2011-04-14 10:00来源:蓝天飞行翻译 作者:航空
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 49-14-00
 ALL  ú ú 02 Page 401 ú Oct 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 ~................................................................... | TABLE I | ..................................................................... | Electrical | Mating | | | Connector | Component | Approximate Location | ..................................................................... | í P12 | Serial Number | Lower Aft Left Side of the Inlet | | | I.D. Unit | Plenum | | í P15 | N2 Speed | Left Side of the Accessory Gearbox | | | Sensor | | | í P17 | IGV Actuator | Left Side of the Engine Between the | | | | Inlet Plenum and the Compressor | | | | Scroll | | í P18 | N1 Speed | Upper Left Side of the Load Gearbox | | | Sensor | | | í P19 | Oil Quantity | Bottom Right Side of the Load Gearbox| | | Sensor | | | í P20 | T13 Air Temp. | Upper Forward Side of the APU on the | | | Sensor | ECS Pneumatic Duct | | í P21 | Diverter Valve| Upper Right Side of the Compressor | | | Control Unit| Scroll | | t P22 | J22 Harness | Bottom of the APU on Lower Bracket | | | Connector | | | | | | | í P23 | T12 Air Temp. | Lower Forward Side of the Inlet | | | Sensor | Plenum | 2............…...............…......................................1
 TASK 49-14-00-004-122
 2.  APU WITH A WIRE HARNESS JUMPER (PRE-PWC-SB 16142); APU Front Wire Harness Removal (Fig. 401)______________________________
 A.  References
 (1)
WDM 49-11-16, 49-11-17, 49-11-18

 (2)
SSM 49-11-01

 (3)
IPC 49-14-00 Fig. 1


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 49-14-00
 ALL  ú ú 02 Page 402 ú Oct 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

2.
 P22 CONNECTOR

3.
 CLAMP


1. J22 CONNECTOR 4. P20 CONNECTOR
14. NUT
21. NUT
14. NUT
T13 AIR 
20. CLAMP  5. BOLT  TEMPERATURE 
SEE  A  SEE  B  6. BOLT  SENSOR 
14. NUT  DIVERTER 
17. NUT  VALVE CONTROL 
7. P21 CONNECTOR 

6. BOLT
8. CLAMP
8.
 CLAMP


9.
 BOLT

19. WIRE HARNESS LACING TAPE
JUMPER
17. NUT  9. BOLT 9A. CLAMP
10. BOLT 8. CLAMP OIL LEVEL
SENSOR17. NUT 11. P19 CONNECTOR
18. CLAMP
12. BOLT
17. NUT
15. NUT
T12 AIR TEMPERATURE SENSOR 13. CLAMP
16. P23 CONNECTOR
15. NUT
12.
 BOLT

13.
 CLAMP FWD


1  SEE SHEET 2
14. NUT
VIEW ON RIGHT SIDE OF ENGINE - FRONT WIRE HARNESS
A
APU Front Wire Harness Installation Figure 401 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 49-14-00
 ALL  ú ú 02 Page 403 ú Oct 10/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

22.
 NUT

23.
 CLAMP


22. NUT
24.
 NUT

25.
 CLAMP


24. NUT 
41. P18  25. CLAMP 
CONNECTOR 
N1 SPEED 
SENSOR  26. BOLT 
24. NUT 
26. BOLT 
40. BOLT  26. BOLT  IGV ACTUATOR 
39. BOLT 
27. P17 CONNECTOR 
1  FROM  14. NUT 
SHEET 1 
28. CLAMP 
14. NUT 
38. BOLT  29. P15 CONNECTOR 
37. CLAMP  N2 SPEED 
SENSOR 

36. BOLT
30.
 CLAMP

31.
 SPACER


14. NUT
35. BOLT
32. CLAMP
FWD HARNESS SUPPORT BRACKET
34. SCREW (4 LOCATIONS)
33. J2 CONNECTOR 6. BOLT
 
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