S 434-061-C01

 (26)
 Install the forward and aft cover tie straps (4 and 2).

 S 434-062-C01

 (27)
 Install the fire control module (15, Fig. 403) for the engine and the APU in the aft electronics control panel (AMM 26-21-51/401).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH NON-REINFORCED CONTROL ú

 76-11-01
 STANDS WITH A TIE ROD-AND-NUT THROUGH ú CONFIG 1 THE STABILIZER TRIM SHAFT ú C01 Page 416 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 434-063-C01
 (28)
 Install the left and right upper side doors (5).

 S 434-064-C01

 (29)
 Install the right control wheel (6) on the control wheel shaft (2).

 NOTE: Handles on control wheels must be 90 (|15)
____
 degrees apart when installed on the control stand.

 S 434-065-C01
 (30) Install the tie rod (8) and attach with the tie rod nut (7) at each end.
 NOTE: It is recommended that you discard the old tie rod nuts and
____
 replace with new tie rod nuts.

 (a)  Tighten the tie rod nuts to 60-70 inch-pounds
 (6.8-7.9 newton-meters).

 NOTE: Make sure at least two threads show on the tie rod
____
 after you tighten the tie rod nut.

 S 434-066-C01
 (31) Adjust the stabilizer trim chain as follows (Fig. 402):
 (a)  In the lower nose compartment, adjust the support links to the lower forward mechanism.
 NOTE: This will tighten the stabilizer trim chain.
____
 (b)  
Adjust the chain so that a 5 pound force will move the chain

 0.25 +0.07/-0.07 inch at a point 4.5 +1.0/-1.0 inches above the forward tangent of the forward mechanism sprocket.

 (c)  
Make sure that the dimension A of the forward and aft support links align within +0.06/-0.06 inch.

 (d)  
Make sure that the control wheels turn freely.

 S 864-067-C01
 (32)
 Make sure that the indicator position for stabilizer trim agrees with the position of the stabilizer.

 (a)  If necessary, adjust position indicator (AMM 27-41-00/501).

 (33)
 Adjust the flap control cables, WFA and WFB (AMM 27-51-00/501).

 S 434-069-C01

 (34)
 Connect the T( )A and T( )B cables (AMM 76-11-04/201 for turnbuckle location).

 S 824-068-C01
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH NON-REINFORCED CONTROL ú
 76-11-01 STANDS WITH A TIE ROD-AND-NUT THROUGH ú CONFIG 1 THE STABILIZER TRIM SHAFT ú C01 Page 417
 ú  Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 094-078-C01
 (35)
 Remove the clamps from the cables.

 S 834-070-C01

 (36)
 Adjust (rig) the forward loop on the thrust control cable (AMM 76-11-00/501).

 S 834-071-C01

 (37)
 Adjust (rig) the start control cables (AMM 76-11-00/501).

 S 834-072-C01

 (38)
 Adjust the control lever for the speed brake as follows (Fig. 401):

 (a)  
Put the control lever for the speed brake in the DOWN detent.

 (b)  
Make sure that the lever latch is in the detent on the control stand.

 (c)  
In the lower nose compartment, make sure that the rig pin can be freely installed through the speed brake forward drum into the structure. 1) If you cannot install the pin easily, do the steps as

 follows: a) Disconnect the upper end of the lower control rod from the idler link. b) Loosen the checknut and adjust the rod end until the rod end bolt fits freely with the rig pin installed. c) Install the rod end bolt with the washer below the
 bolthead. d) Put the washer and locknut on the bolt. e) Tighten the checknut on the rod end. f) Make sure that you can see the rod end in the
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 發動機控制 ENGINE CONTROLS(25)