S 486-020-N00

 (2)  
Install the strainer and adapter to the fuel distribution valve.

 (a)  
Lubricate the packings with petrolatum.

 (b)  
Install the packings in the grooves on the ends of the strainer.

 (c)  
Put the strainer into the housing of the fuel distribution valve.

 (d)  
Put the adapter on the four hole flange on the fuel
 distribution valve.

 (e)  
Align the offset bolt hole.

 (f)  
Install the adapter with the bolts.

 S 796-016-N00
 (3)  
Do the leak check of the fuel distribution tubes and connections.

 (a)  
Pressurize the fuel manifold and the fuel distribution valve at the adapter with air to 95-105 psi (655-725 kPa).

 (b)  
Apply the leak check to the fuel distribution tubes between the fuel distribution valve and the fuel injectors.

 (c)  
Apply the leak check to the connections between the fuel distribution valve and the fuel injectors.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 73-11-00
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
(d)  
Let the leak check stay for a minimum of five minutes.

 (e)  
Make sure that you can see no leakage from the surfaces, joints or connections.

 (f)  
If you find any leakage, repair or replace the applicable components and do the leak inspection for those components again.

 (g)  
Disconnect the air supply.

 S 086-015-N00
 (4)  
Remove the adapter from the fuel distribution valve.

 (a)  
Keep the bolts with the adapter.

 S 416-014-N00
 (5)  
Install the strainer in the fuel distribution valve
 (AMM 73-11-04/401).

 H.
Return the aircraft to its usual condition

 S 416-035-N00
 WARNING: OBEY THE INSTRUCTIONS IN AMM 78-31-00/201 WHEN YOU CLOSE THE
_______ THRUST REVERSERS. IF YOU DO NOT OBEY THE INSTRUCTIONS, INJURIES TO PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR.
 (1)  
Close the thrust reversers (AMM 78-31-00/201).

 S 416-036-N00

 (2)  
Close the core cowl panels (AMM 71-11-06/201).

 S 416-037-N00

 (3)  
Close the fan cowl panels (AMM 71-11-04/201).

 S 446-038-N00

 (4)  
Do the activation procedure for the thrust reversers
 (AMM 78-31-00/201).

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 ALL  ú ú N01 Page 607 ú Feb 10/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
FUEL PUMP - REMOVAL/INSTALLATION
________________________________
 1.  General
_______
 A.  This procedure gives the tasks for the removal and the installation of the fuel pump. You can remove and install the fuel pump with the fuel metering unit (FMU) as one unit (this is referred to as the fuel pump unit). You can also remove and install the fuel pump after the removal of the FMU. This procedure gives the steps to remove and to install the fuel pump with and without the FMU.
 B.  The fuel pump is installed on the forward face of the main gearbox at the 5 o'clock position.
 C.  You can get the access to the fuel pump when you open the left and right half of the thrust reverser.
 TASK 73-11-01-004-001-N00
 2.  Fuel Pump Removal (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, Commercial Products Division, 400 Main Street, East Hartford, CT 06108

 B.  
Standard Tools and Equipment

 (1)
Container - 5 gallon (20 liter) capacity, used to collect fuel
　
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