• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-17 09:17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

 79-11-00
 ALL  ú ú N02 Page 1 ú Feb 10/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES /MAINTENANCE MANUAL ////////////////////////
OIL TANK SIGHT GAGE
SEE A
2
MAIN GEARBOX
FWD
OIL TANK SIGHT GAGE
SCUPPER DRAIN LINE
B
1 ENGINES WITHOUT PWSB 79-65
2 ENGINES WITH PWSB 79-65
HEAT SHIELD
A
ENGINE OIL TANK FILLER CAP
SEE B
1
A
SCUPPER
DRAIN
SCUPPER
ENGINE
DRAIN LINE
OIL TANK
OIL QUANTITY OIL TANK
TRANSMITTER MASTER MAGNETIC CHIP DETECTOR
A
OIL TANK SIGHT GAGE
1
ENGINE OIL TANK
FILLER CAP

SCUPPER
DRAIN
SCUPPER
DRAIN FILLER NECKLINE VALVE L-A0730
A-A
Oil Storage Component Location
Figure 1

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 79-11-00
 ALL  ú ú N02 Page 2 ú Jun 10/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
OIL TANK - REMOVAL/INSTALLATION
_______________________________
 1.  General
_______
 A.  This procedure removes and installs the oil tank.
 B.  The oil tank is installed on the aft face of the main gearbox at the 8 o'clock position.
 C.  You can get access to the oil tank through the left thrust reverser half.
 TASK 79-11-01-004-001-N00
 2.  Remove the Oil Tank (Fig. 401)
___________________
 A.  Standard Tools and Equipment
 (1)  
Container - 10 U.S. gallon (40 liter) capacity, use to collect the engine oil

 B.  
References

 (1)  
AMM 75-24-02/401, Turbine Vane Cooling Air Duct

 (2)  
AMM 79-21-10/401, Magnetic Chip Detector

 (3)  
AMM 79-31-01/401, Oil Quantity Transmitter

 (4)  
IPC 71-71-00 Fig. 1

 (5)  
IPC 72-61-00 Fig. 25

 (6)  
IPC 79-11-01 Fig. 10

 (7)  
IPC 79-11-01 Fig. 11

 (8)  
IPC 79-11-03 Fig. 1

 (9)  
IPC 79-21-51 Fig. 1

 C.  
Access

 (1)  
Location Zone 412 Engine 1 - Main Gearbox Aft Face 8 o'clock 422 Engine 2 - Main Gearbox Aft Face 8 o'clock 432 Engine 3 - Main Gearbox Aft Face 8 o'clock 442 Engine 4 - Main Gearbox Aft Face 8 o'clock

 (2)  
Access Panel
 415 Left Thrust Reverser Half - Engine 1
 425 Left Thrust Reverser Half - Engine 2
 435 Left Thrust Reverser Half - Engine 3
 445 Left Thrust Reverser Half - Engine 4


 D.  
Procedure


 S 864-002-N00
 (1)  
Open these circuit breakers on the overhead circuit breaker panel, P7, and attach the DO-NOT-CLOSE tags:

 (a)  
7F9 EIU L

 (b)  
7F10 EIU C

 (c)  
7F15 EIU R

 

 (2)  
Remove the No. 3 turbine vane cooling air duct (AMM 75-24-02/401).


 S 014-003-N00
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 79-11-01
 ALL  ú ú N01 Page 401 ú Feb 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES /MAINTENANCE MANUAL ////////////////////////
1. BOLT (10 LOCATIONS)
2. HEAT SHIELD
SEE A
41. BRACKET 1
36. COOLING AIR TUBE
1. BOLT
35. BRACKET
40. ELECTRICAL CONNECTOR
14. HEAT SHIELD34. GROUND STRAP (DT675) CLAMP
33. PACKING CHECK VALVE
SEE B
HOUSING (REF) 37. BOLT
38. CLAMP SLEEVE
15. OIL TANK
(REF) 16. TUBE SUPPORT
39. NUT
BRACKET
32. PACKING 17. NUT24. BRACKET
31. PACKING 18. HARNESS
BREATHER
25. BOLT  SUPPORT
TUBE BRACKET
26. PACKING
30. PACKING 1. BOLT
OIL TUBE 29. MAGNETIC CHIP
(REF) DETECTOR HOUSING 27. PACKING
19. NUT
20. BRACKET
23. ENGINE I.D.
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:747-400 AMM 飞机维护手册 滑油 OIL(14)