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时间:2011-04-16 10:04来源:蓝天飞行翻译 作者:航空
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 TASK 72-61-11-004-001-N00
 2.  Remove the Main Oil Filter Housing
__________________________________
 A.  Standard Tools and Equipment
 (1)
Container - 5 gallon (20 liter) capacity, suitable to collect oil

 B.  
References

 (1)  
AMM 71-11-04/201, Fan Cowl Panels

 (2)  
AMM 71-11-06/201, Core cowl Panels

 (3)  
AMM 78-31-00/201, Thrust Reverser System

 (4)  
AMM 79-35-01/401, Oil Filter Differential Pressure Switch

 (5)  
AIPC 26-21-55, Fig. 3, AIPC 36-11-61, Fig. 1, AIPC 71-00-50, Fig. 1, AIPC 71-71-01, Fig. 1, AIPC 72-61-00, Fig. 1, AIPC 72-61-11, Fig. 1, AIPC 79-21-01, Fig. 15, AIPC 79-21-05, Fig. 5, AIPC 79-21-06, Fig. 1, AIPC 79-21-51, Fig. 5, AIPC 79-35-01, Fig. 1

 C.  
Access

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

 (2)  
Access Panel 415 and 416 Thrust Reverser Halves - Engine 1 425 and 426 Thrust Reverser Halves - Engine 2 435 and 436 Thrust Reverser Halves - Engine 3 445 and 446 Thrust Reverser Halves - Engine 4

 D.  
Procedure (Fig. 401 and 402)

 (1)  
Open the fan cowl panels (AMM 71-11-04/201).


 S 014-026-N00
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 72-61-11
 ALL  ú ú N01 Page 401 ú Jun 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES /MAINTENANCE MANUAL ////////////////////////
SEE A
PNEUMATIC 
FIRE EXTINGUISHING  TUBE NUTS 
TUBE NUT 

1. MAIN OIL HOUSING FILTER  GEARBOX MAIN  SEE  B  OIL TANK  FWD 

Figure 401 (Sheet 1) Pneumatic Tubes Installation 

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 72-61-11
 ALL  ú ú N01 Page 402 ú Oct 10/88
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
SCREW3.  SCREW5.  WASHER6. 
(2 LOCATIONS)  WASHER6.  FIRE7. 
COOLER FUEL/OIL  2. WASHER  SCREW5.  SCREW5.  EXTINGUISHING TUBE ASSEMBLY 
(2 LOCATIONS)  WASHER6. 
4.NUT 
14.SPACER 

(2 LOCATIONS)
4.NUT 4.NUT
13.DRAIN TUBE SEE C
8.SCREW
9.WASHER
BRACKET
12. BRACKET 10.NUT
SEE D
11.CLAMP  PNEUMATIC TUBE10. NUT
BLOCK  NUT (ATTACHED
(2 LOCATIONS)  MAIN GEARBOX
SEE F ASSEMBLY  TO THE DIFFUSER CASE)SEE E
FWD B
8.SCREW (3 LOCATIONS)
9.WASHER
8.SCREW (3 LOCATIONS) (4 LOCATIONS)
19. PNEUMATIC TUBE
9. WASHER (4 LOCATIONS)
18.PNEUMATIC TUBE ASSEMBLY
17. PNEUMATIC TUBE
10.NUT 16.PNEUMATIC
(3 LOCATIONS) TUBE
15. PNEUMATIC 10.NUT
TUBE  D
C
(4 LOCATIONS)
Pneumatic Tubes Installation
Figure 401 (Sheet 2)

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 72-61-11
 ALL  ú ú N01 Page 403 ú Feb 10/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES /MAINTENANCE MANUAL ////////////////////////
21. OIL SYSTEM PRESSURE RELIEF 10. NUT VALVE
9. WASHER
SEE G
20. OIL FILTER OUTLET 4. NUTPRESSURE TUBE (2 PLACES)
10. NUT 9. WASHER
(2 PLACES) (2 PLACES)
28. CLAMP BLOCK
22. CLAMP ASSEMBLY
8.
SCREW (2 PLACES)

9.
WASHER


23. BOLT
22. CLAMP (2 PLACES)
18. PNEUMATIC
27. SPACER 
(2 PLACES)  TUBE 
SEE  H  HIGH PRESSURE 
2. WASHER  CONTROLLER 
(2 PLACES)  17. PNEUMATIC TUBE 
 
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