(2)  
AMM 71-00-00/501, Power Plant

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

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 73-21-01
 ALL  ú ú N03 Page 408 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
(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 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

 F.
Procedure

 S 424-079-N00
 (1)  
Remove the caps from the fuel metering unit (FMU) (5) and the fuel pump.

 S 424-080-N00

 (2)  
If you will install a new FMU (5), install these parts on the FMU:

 (a)  
Lubricate a new packing (26) with the petrolatum.

 (b)  
Install a new packing (26) on the adapter (27).

 (c)  
Put the adapter (27) on the FMU (5).

 (d)  
Lubricate the threads of inboard bolts (28) with engine oil.

 (e)  
Install the adapter (27) to the FMU with two inboard bolts (28).

 NOTE: Only tighten the bolts with your hand at this time.
____
 (f)  
Lubricate a new packing (23) with the petrolatum.

 (g)  
Install new packing (23) on the adapter (22).

 (h)  
Install the adapter (22) in the FMU (5).

 (i)  
Tighten the adapter to 200-225 pound-inches (22.6-25.4 newton-meters).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 73-21-01
 ALL  ú ú N02 Page 409 ú Jun 10/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
S 424-081-N00
 (3)  
Install the FMU:

 (a)  
Install the FMU M3108 (5) on the fuel pump:

 1)  Lubricate the packings (13, 14, 32, and 33) with the petrolatum.
 2)  Install the transfer tubes (34) to the fuel pump as follows: a) Install one packing (32 and 33) to both of the transfer
 tubes (34). b) Install the transfer tubes (34), packing side inward, to the fuel pump ports. c) Install the retainers (35) to hold the transfer tubes (34) in position in the fuel pump. d) Install the remaining packings (13 and 14) to the
 transfer tubes (34) on the fuel pump. 3) Lubricate the studs on the FMU (5) with engine oil. 4) Install the FMU (5) on the fuel pump.
 NOTE: Make sure the supply tubes on the fuel pump align
____
 with the ports on the FMU.

 5) Install the FMU (5) to the fuel pump with the washers (15) and the nuts (16). 6) Tighten the nuts (16) to 270-300 pound-inches (22.6-33.9 newton-meters).
 (b)  Install the bracket (30) on the adapter (27): 1) Lubricate the threads of two bolts (28 and 29) with engine
 oil. 2) Put the bracket (30) on the adapter (27). 3) Install the bracket (30) with the bolts (28 and 29).
 NOTE: Install the bolt (29) at the bottom hole of the
____
 bracket.

 4)  Tighten all four bolts to 65-85 pound-inches (7.3-9.6 newton-meters).
 (c)  Connect the supply tube (2) for the fuel distribution valve: 1) Remove the caps from the supply tube (2). 2) Lubricate the packings (8) with the petrolatum. 3) Install the packings (8) and the retainers (7) on the ends
 of the supply tube (2). 4) Lubricate the threads of the adapter for the fuel flow transmitter and of the FMU adapter (27) with engine oil. 5) Connect the tube nuts (1) to the adapter for the fuel flow transmitter and to the FMU adapter (27). 6) Tighten the tube nuts (1) to 100-110 pound-inches
　
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 2(9)