(c)  
Remove the union (3) and the O-ring (4). 1) Discard the O-ring.

 (d)  
Remove the band clamp from the valve actuator.

 NOTE: Keep the band clamp for the installation.
____
 TASK 36-11-19-404-037
 3. Install the PRV (Fig. 401)
_______________
 A. Consumable Materials
 (1)  
D01062, Never-Seize, Pure Nickel Special, NSBT-8N
 (High temperature anti-seize compound)

 (2)  
G00095 Detector - Leak, Leak-Tek (160X)

 (3)  
D00062 Lubricant - Pneumatic System Thread, FS 1292 (Fluor-Silicone) MIL-G-4343

 (4)  
G00145 Tape - Permacel 421

 B.
References

 (1)  
24-22-00/201, Manual Control

 (2)  
AMM 20-11-28/401, Lockwire

 (3)  
36-00-00/201, Pneumatic System

 (4)  
AMM 36-11-01/401, Pneumatic Manifold

 (5)  
71-00-00/201, Power Plant

 (6)  
71-11-04/201, Fan Cowl Panels

 (7)  
71-11-06/201, Core Cowl Panels

 (8)  
78-31-00/201, Thrust Reverser System

 C.
Access

 (1)  
Location Zone
 412 Engine 1 - HPC Case 10:00 o'clock
 422 Engine 2 - HPC Case 10:00 o'clock
 432 Engine 3 - HPC Case 10:00 o'clock
 442 Engine 4 - HPC Case 10:00 o'clock

 (2)  
Access Panel
 415 Left Thrust Reverser Half - Engine 1
 425 Left Thrust Reverser Half - Engine 2
 435 Left Thrust Reverser Half - Engine 3
 445 Left Thrust Reverser Half - Engine 4

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 36-11-19
 ALL  ú ú 02P Page 407 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 D. Install the PRV
 S 424-068
 (1) Do these steps to install the band clamp on the valve actuator:
 NOTE: The PRV may need to be changed using the Hamilton Sundstrand
____ Service Bulletin HS-SB 36-183. The Hamilton Sundstrand service bulletin changes the insulation cover and the heat shield because of the new wire routing.
 (a)  
Put the band clamp in its position on the actuator.

 (b)  
Tighten the band clamp 30 to 40 inch-pounds

 (3.39 to 4.52 newton meters).

 (c)  
Install a lockwire on the band clamp (AMM 20-11-28/401).

 S 644-055
 (2)  
Apply lubricant to the O-ring (4).

 S 434-041

 (3)  
Install the O-ring (4) on the union (3).

 S 644-056

 (4)  
Apply anti-seize compound to the threads of the union (3) and the elbow (2).

 S 434-042

 (5)  
Install the union (3) in the PRV (1).

 S 434-043

 (6)  
Install the elbow (2) on the union (3).

 S 434-015

 (7)  
Remove the protective covers from the open ducts.

 S 434-016

 (8)  
Install the seals (8) in the duct flanges.

 S 424-017

 (9)  
Put the PRV (1) between the duct.

 (a)  
If you cannot easily install the PRV because it is too tight, loosen one of the duct sections on either side of the PRV (AMM 36-11-01/401).

 (10)
 Loosely install the couplings (7).

 (11)
 Connect the actuator pressure tube to the elbow (2) on the PRV.

 S 434-044
 S 434-018
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 36-11-19
 ALL  ú ú 02P Page 408 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 S 214-053
 (12)
 Make sure there is a clearance of 0.37-0.87 inches between the valve actuator and the high pressure duct.

 S 434-020

 (13)
 Tighten the couplings (7) to 115-125 pound-inches (13-14 N.m).

 NOTE: Make sure you align the joints of the duct and the HPSOV
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機維護手冊 氣動系統 PNEUMATIC SYSTEM(120)