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时间:2011-04-17 09:17来源:蓝天飞行翻译 作者:航空
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 NOTE: You can use plain nuts with wire holes as an
____
 alternate method.

 (c)  Remove the filter cover (13). 1) Discard the packing (6). 2) Discard the four self-locking nuts (14).
 NOTE: Keep the nuts with the wire holes if they were used.
____
 (d)  
Remove the main oil filter (19) from the filter housing (1).

 (e)  
Remove the retaining ring (20) from the pressure relief valve (21).

 (f)  
Remove the pressure relief valve (21) from the cover (13).

 (g)  
Do a check of the studs installed in the main oil filter housing (Fig. 401, View I). 1) If the studs are not acceptable, remove and replace the


 main oil filter housing (AMM 72-61-11/401).
 S 034-033-N00
 (7) Install protective caps into the housing of the main oil filter.
 TASK 79-21-05-404-007-N00
 3. Main Oil Filter Element Installation (Fig. 401)
____________________________________
 A. Equipment
 (1)  M303, M305, or M307 Bergen Mechanical Crimper
 Bergen Cable Technologies Inc
 170 Gregg St

 P.O.
 Box 1300
 Lodi, NJ 07644-9982


 B.
Consumable Materials


 (1)  
D00390 Oil - Engine

 (2)  
G00964 Compound - Antigalling, Fel-Pro C-200

 (3)  
G02332 Ferrule, Safety Cable (P05-292)

 (4)  
G02334 Lockwire, (P05-289) 0.032 inch (0.813 mm) - AS3214-02

 (5)  
G02335 Cable, Safety (P05-291)

 C.
Parts


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 79-21-05
 ALL  ú ú N01 Page 410 ú Jun 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 401 | 1 | Main Oil Filter Housing | 72-61-11 | 01 | 55 | | | 2 | Filter Element | 79-21-05 | 05 | 75 | | | 11 | Bolt | | | 25 | | | 12 | Washer | | | 30 | | | 13 | Main Oil Strainer Cover | | | 35 | | | 14 | Nut | | | 45 | | | 15 | Screw | | | 57 | | | 16 | Spring Retainer | | | 67 | | | 17 | Washer | | | 62 | | | 18 | Main Oil Strainer Cover | | | 35 | | | 19 | Filter Element | | | 75 | | | 20 | Retaining Ring | 79-21-06 | 01 | 15 | | | 21 | Pressure Relief Valve | | | 30 | 2......…........…...................................…...........….....…........1
 D. References
 (1)
AMM 12-13-03/301, Engine - Servicing

 (2)
AMM 71-00-00/501, Power Plant

 (3)
AMM 71-11-04/201, Fan Cowl Panels

 (4)
AMM 71-11-06/201, Core Cowl Panels

 (5)
AMM 78-31-00/201, Thrust Reverser System

 E.
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 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


 F.
Install the main oil filter (Fig. 401).

 (1)
Remove protective cap from the housing of the main oil filter.

 (2)
Clean the housing of any unwanted material.


 S 434-034-N00
 S 144-061-N00
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 79-21-05
 ALL  ú ú N01 Page 411 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
S 424-062-N00

 CAUTION:_______ THE MAIN OIL FILTERS HAVE A REMOVABLE PLUG WHICH YOU MUST
 INSTALL BEFORE YOU INSTALL THE MAIN OIL FILTER INTO THE
 HOUSING.  IF YOU DO NOT INSTALL THE REMOVABLE PLUG, THE ENGINE
 
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