(e)
Make sure all internal parts get a thick layer of the oil:
(f)
Move the FMU (6) at an angle.
(g)
Drain the oil from the FMU (6).
(h)
Install caps on the transfer tube ports.
S 024-111-N00
(8)
Install caps on the openings in the FMU (6) if it is not done.
S 024-112-N00
(9)
Install caps on the openings in the fuel pump (11).
TASK 73-11-01-404-033-N00
3. Fuel Pump Installation (Fig. 401)
______________________
A. Special Tools and Equipment
(1)
PWA 85862 Adapter - Torque, Pratt & Whitney,
Commercial Products Division,
400 Main Street,
East Hartford, CT 06108
(2)
PWA 85989 Fixture, Handling (Optional), Pratt & Whitney
(3)
PWA 86461 Adapter - Torque, Pratt & Whitney
B.
Consumable Materials
(1)
D00250 Petrolatum White, VV-P-236
(2)
D00390 Oil - Engine
(3)
G00964 Compound - Antigalling, Fel-Pro C-200
(4)
G01505 Lockwire - MS20995
(5)
G02332 Ferrule - P05-292 (Optional)
(6)
G02335 Cable - Safety - P05-291 (Optional)
C.
Parts
~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 401 | 6 | Fuel Metering Unit | 73-21-01 | 05 | 40 | | | 9 | Packing | 73-11-02 | 05 | 10 | | | 11 | Fuel Pump | 73-11-01 | 05 | 75 | | | 12 | Retainer | 73-11-06 | 35 | 35 | | | 13 | Packing | | | 40 | | | 21 | Gasket | 73-11-06 | 01 | 40 |
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
73-11-01
ALL ú ú N02 Page 414 ú Oct 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | | 31 | Packing | 71-71-01 | 01 | 565 | | | 35 | Packing | 73-11-01 | 05 | 65 | | | 37 | Packing | | | 70 | | | 38 | Packing | 73-21-01 | 05 | 35 | | | 41 | Packing | 73-11-06 | 20 | 25 | | | 42 | Packing | 73-11-01 | 05 | 55 | | | 46 | Packing | 73-21-09 | 01 | 10 | | | 49 | Packing | 73-34-01 | 05 | 20 | | | 53 | Packing | 73-21-01 | 05 | 25 | | | 58 | Packing | | | 55 | | | 59 | Packing | | | 60 | | | 61 | Packing | 73-11-01 | 05 | 15 | | | 74 | Packing | 73-21-09 | 01 | 55 | 2.....….........…...................................…..........…......…........1
D. References
(1)
AMM 70-23-00/201, Tightening Techniques and Torque Values
(2)
AMM 70-24-05/201, Electrical Harnesses
(3)
AMM 71-00-00/501, Power Plant
(4)
AMM 71-11-04/201, Fan Cowl Panels
(5)
AMM 71-11-06/201, Core Cowl Panels
(6)
AMM 73-11-07/401, Fuel Bypass Valve
(7)
AMM 73-21-01/401, Fuel Metering Unit
(8)
AMM 78-31-00/201, Thrust Reverser System
E.
Access
(1)
Location Zone 412 Engine 1 - Main Gearbox Fwd Face 5 o'clock 422 Engine 2 - Main Gearbox Fwd Face 5 o'clock 432 Engine 3 - Main Gearbox Fwd Face 5 o'clock 442 Engine 4 - Main Gearbox Fwd Face 5 o'clock
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
73-11-01
ALL ú ú N02 Page 415 ú Jun 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
(2)
Access Panel
415 and 416 Thrust Reverser Halves - Engine 1
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機維護手冊 發動機燃油和控制 1(23)
