(a)  
Apply the anti-seize compound to the threads of the barrel nut (19).

 (b)  
Install the barrel nut retainer (18), and the barrel nut (19) on the upper corner of the forward left side of the precooler.

 (c)  
Apply the thread lubricant to the O-ring (32) and the threads on the tee (30).

 (d)  
Install the tee (30), jamnut (31), bracket (34), and O-ring (32) on the boss on the forward left corner of the precooler.

 (e)  
Tighten the jamnut when the tee (30) is aligned with the pressure sense tube (6).

 (f)  
Apply the thread lubricant to the O-ring (32) and the threads of the tee (33).

 (g)  
Install the tee (33), jamnut (31), bracket (34), and O-ring (32) on the boss on the aft right corner of the precooler.

 (h)  
Tighten the jamnut (31) when the tee (33) is aligned with the tubes (25 and 26) and when the clamps (27) on the bracket (34) is aligned with the tubes (23 and 24).

 (i)  
Install the brackets (35 and 37) on the precooler-fan-air inlet.

 S 644-022
 (2)  Use anti-seize compound to lubricate the precooler mounting bolts (15 and 22), bushings (13 and 20), and nuts (10).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 36-12-01
 ALL  ú ú 01P Page 413 ú Oct 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 747-400 MAINTENANCE MANUAL
 S 434-023
 (3)  Put the seals (8) in the correct position on the precooler or on the duct flanges.
 S 424-024
 (4)  Put the precooler (1) in the installed position.
 S 434-025
 (5)  Engage the link (12) with the mount on the lower corner of the aft right side of the precooler (1) (Fig. 401, Sheet 3). (a) Install the bushing (13). (b) Put the washer (14) on the bolt (15) with the countersunk side of the washer adjacent to the bolt head. (c) Install the bolt (15), washer (11), and nut (10).
 S 434-026
 (6)  Install the bushing (20) in the mount on the upper corner of the forward left side of the precooler (1) (Fig. 401, Sheet 3). (a) Install the washer (21), with the countersunk side of the washer adjacent to the bolt head (22). (b) Install the bolt (22).
 S 434-027
 (7)  Engage the link (17) with the mount on the upper corner of the aft left side of the precooler (1) (Fig. 401, Sheet 3). (a) Install the bushing (13). (b) Put the washer (14) on the bolt (15) with the countersunk side of the washer adjacent to the bolthead. (c) Install the bolt (15), washer (11) and the nut (10).
 S 434-028
 (8)  Engage the link (16) with the mount on the lower corner of the aft left side of the precooler (1) (Fig. 401, Sheet 3). (a) Install the bushing (13). (b) Put the washer (14) on the bolt (15) with the countersunk side of the washer adjacent to the bolthead. (c) Install the bolt (15), washer (11), and the nut (10).
 S 434-029
 (9)  Do the steps that follow to install the couplings (7) on the ducts upstream and downstream of the precooler: (a) Tighten the couplings (7) to 115-125 pound-inches (13-14 N.m). (b) Lightly hit each coupling around its perimeter with a fiber hammer.
 (c) (d)  Continue the torque-hit procedure until three torque-hit cycles are completed.Tighten the couplings (7) to 115-125 pound-inches (13-14 N.m).

 S 944-030
 (10) Remove the protective mat from the fuel manifold.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 36-12-01
 ALL  ú ú 01P Page 414 ú Oct 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 434-031
 (11)
 Connect the bracket (5) to the precooler exhaust flange.

 S 644-047

 (12)
 Apply anti-seize compound to the threads of the pneumatic
 connectors.

 S 434-032

 (13)
 Connect the pressure sense hose (9) and the pressure sense tube (6) to the tee on the forward left corner of the precooler (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 氣動系統 PNEUMATIC SYSTEM(141)