(e)
Remove the filter element (56a) from the main oil filter housing (1). 1) Discard the filter element (56a).
(f)
Remove the retaining ring (78) from the pressure relief valve (79).
(g)
Remove the pressure relief valve (79) from the cover (29).
(h)
Remove the oil system pressure relief valve (21). 1) Remove the bolts (60) that attach the bracket and pressure relief valve (21) to the main oil filter housing (1). 2) Remove the bracket (30), and the pressure relief valve
(21). 3) Discard the packings (62 and 63).
TASK 72-61-11-404-013-N00
3. Install the Main Oil Filter Housing___________________________________
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)
G02334 Lockwire, (P05-289) 0.032 inch (0.813 mm) AS3214-02
(3)
G02335 Cable, Safety (P05-291)
(4)
G02332 Ferrule, Safety Cable (P05-292)
(5)
G00964 Compound - Antigalling, Fel-Pro C-200
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
72-61-11
ALL ú ú N01 Page 425 ú Oct 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
C. Parts
~.............................................................................. | AMM | | AIPC | ................. ............................. | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 401 | 1 | Main Oil Filter Housing | 72-61-11 | 01 | 55 | | | 2 | Washer | 36-11-61 | 01 | 60 | | | 3 | Screw | | | 55 | | | 4 | Nut | | | 40 | | | 5 | Screw | 26-21-55 | 03 | 5 | | | 6 | Washer | | | 10 | | | 7 | Fire Extinguishing Tube Assy | | | -| | | | Tube Assy | | | 35 | | | | Tube Assy | | | 40 | | | 8 | Screw | 36-11-61 | 01 | 30 | | | 9 | Washer | | | 35 | | | 10 | Nut | | | 70 | | | 11 | Clamp Block Assy | | | -| | | | Block Half | | | 80 | | | | Channel | | | 75 | | | 12 | Bracket | 71-00-50 | 01 | 535 | | | 13 | Drain Tube | 71-71-01 | 01 | 260 | | | 14 | Spacer | 36-11-61 | 01 | 65 | | | 15 | Pneumatic Tube | | | 185 | | | 16 | Pneumatic Tube | | | 140 | | | 17 | Pneumatic Tube | | | 190 | | | 18 | Pneumatic Tube Assy | | | -| | | | Tube Assy | | | 130 | | | | Tube Assy | | | 180 | | | 19 | Pneumatic Tube | | | 210 | | | 20 | Oil Filter Outlet Pressure Tube | 79-35-01 | 01 | 10 | | | 21 | Oil System Pressure Relief Valve | 79-21-06 | 01 | 95 | | | 22 | Clamp | 36-11-61 | 01 | 120 | | | 23 | Bolt | 71-00-50 | 01 | 510 | | | 24 | Nut | 72-61-00 | 01 | 25 | | | 25 | Bolt | | | 20 | | | 26 | Screw | 36-11-61 | 01 | 85 | | | 27 | Spacer | | | 95 | | | 28 | Clamp Block Assy | | | -| | | | Block | | | 110 | | | | Channel | | | 105 | | | | Block | | | 115 | | | 29 | Cover | 79-21-05 | 01 | 35 |
2.....….........…..................................…...........…......…........1
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
72-61-11
ALL ú ú N01 Page 426 ú Jun 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
~.............................................................................. | AMM | | AIPC | ................. ............................. | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | | 30 | Bracket | 71-00-50 | 01 | 533 | | | 31 | Oil Filter Inlet Pressure Tube | 79-35-01 | 01 | 5 | | | 32 | Screw | 36-11-61 | 01 | 30 | | | 33 | Support Bar | 71-00-50 | 01 | 520 | | | 34 | Air/Oil Heat Exchanger Inlet Tube| 79-21-01 | 15 | 60 | | | 34a | Bolt | | | 15 | | | 34b | Packing | | | 40 | | | 35 | Main Filter Oil Tube | 72-61-11 | 05 | 65 | | | 36 | Oil Trim Pressure Tube | 79-21-01 | 15 | 75 | | | 37 | Fuel/Oil Cooler Bypass Valve Tube| 79-21-51 | 05 | 150 | | | 38 | Retainer | | | 100 | | | 39 | Packing | | | 95 | | | 40 | Packing | | | 90 | | | 41 | Bolt | | | 30 | | | 42 | Packing | 79-21-01 | 15 | 55 | | | 43 | Bolt | | | 10 | | | 44 | Bolt | 72-61-11 | 05 | 5 | | | 45 | Packing | | | 67 | | | 46 | Bolt | | | 15 | | | 47 | Nut | | | 25 | | | 48 | Bolt | | | 10 | | | 49 | Reducer (PRE-PW-SB 79-70) | 72-51-11 | 01 | 15 | | | 49 | Reducer (POST-PW-SB 79-70) | 72-35-01 | 15 | 45 | | | 50 | Packing (PRE-PW-SB 79-70) | 72-51-11 | 01 | 20 | | | 51 | Insert | | | 25 | | | 52 | Packing (PRE-PW-SB 79-70) | | | 30 | | | 52 | Packing (POST-PW-SB 79-70) | 72-35-01 | 15 | 50 | | | 53 | Packing | 72-51-11 | 01 | 45 | | | 54 | Transfer Tube | | | 50 | | | 55A | Transfer Tube | | | 40 | | | 55B | Transfer Tube (PRE-PW-SB 79-43) | | | 42 | | | 55C | Transfer Tube (or Anti-Siphon | | | 43 | | | | Tube Assembly)(POST-PW-SB 79-43)| | | |
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 发动机 ENGINE 2(151)
