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 2) Lubricate a new packing (4) with the petrolatum. 3) Install the packing (4) on the drain plug (5). 4) Lubricate the threads of the drain plug (5) with engine
 oil.
 5)  Install the drain plug (5) in the FP3 port of the fuel pump. a) Tighten the drain plug (5) to 45-55 pound-inches
 (5.1-6.2 newton-meters). 6) Install the lockwire on the drain plug (5).
 (c)  Remove the fuel supply tube (11): 1) Disconnect the tube nut (10) from the adapter (9) for the
 fuel bypass valve. 2) Disconnect the tube nut (12) from the fuel metering unit. 3) Disconnect the tube nut (17) from the tee for the fuel
 supply manifold. 4) Remove the fuel supply tube (11) from the engine. 5) Install caps on the openings in the adapter (7), fuel
 metering unit and the tee for the fuel supply manifold.
 (d)  Remove the fuel bypass valve (7) from the engine: 1) Remove the bolts (3) which install the fuel tube (2) for the oil cooler inlet to the fuel bypass valve (7).
 2)  Remove the bolts (13) and the washers (14) which attach the fuel bypass valve (7) to the fuel pump.
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
3) Remove the fuel bypass valve (7) from the engine.
 a) Discard the packings (6 and 15).
 4) Discard the packing (16) from the fuel tube (2) flange.
 5) Install caps on the fuel tube and the openings in the fuel
 bypass valve (7) and the fuel pump .
 S 024-058-N00
 (2)  
If it is necessary to replace the fuel bypass valve (7), do the steps that follow:

 (a)  
Remove the adapter (9) from the fuel bypass valve.

 (b)  
Discard the packing (8).

 TASK 73-11-07-404-020-N00
 3. Fuel Bypass Valve Installation (Fig. 401)
______________________________
 A. Consumable Materials
 (1)  
D00250 Petrolatum White, VV-P-236

 (2)  
D00390 Oil - Engine

 (3)  
G01505 Lockwire - MS20995

 (4)  
G02332 Ferrule - P05-292 (Optional)

 (5)  
G02335 Cable - Safety - P05-291 (Optional)

 B.
Parts

 ~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 401 | 4 | Packing | 73-11-02 | 05 | 10 | | | 6 | Packing | 73-11-07 | 02 | 25 | | | 7 | Bypass Fuel Return Valve (Fuel | | | 35 | | | | Bypass Valve) | | | | | | 8 | Packing | | | 10 | | | 15 | Packing | | | 30 | | | 16 | Packing | 73-11-06 | 20 | 25 | 2.....….........…...................................…..........…......…........1
 C. References
 (1)  AMM 71-00-00/501, Power Plant
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
(2)  
AMM 71-11-04/201, Fan Cowl Panels

 (3)  
AMM 71-11-06/201, Core Cowl Panels

 (4)  
AMM 78-31-00/201, Thrust Reverser System

 D.  
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

 (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

 E.  
Procedure

 S 424-060-N00
 (1)  
If it is necessary to install a new fuel bypass valve (7), do the steps that follow:

　
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