76-11-01
STANDS WITH A STABLIZER TRIM SHAFT WITH ú CONFIG 3 A SELF-LOCKING INSERT-AND-BOLT ú C02 Page 424 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 824-081-C03
(4)
Make sure that the dimension A of the forward and aft stabilizer trim chain support links match within +0.06/-0.06 inch.
S 824-082-C03
(5)
Adjust the flap control cables, WFA and WFB (AMM 27-51-00/501).
S 824-083-C03
(6)
Adjust (rig) the forward loop of the thrust control cable (AMM 76-11-00/501).
S 824-084-C03
(7)
Adjust (rig) the engine start control cables (AMM 76-11-00/501).
S 824-092-C03
(8)
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
inspection hole in the control rod. g) Remove the rig pin.
S 414-085-C03
(9)
Close the forward nose compartment.
(10)
Close the electronic equipment access door No. 1201.
(11)
Supply hydraulic power (AMM 29-15-00/201).
S 714-090-C03
(12)
With the reverse thrust levers in their stowed position (forward and down), move each forward thrust lever through its full travel.
S 414-086-C03
S 864-087-C03
(a) Make sure the levers move smoothly and freely without
interference, binding, or scraping.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS-REINFORCED CONTROL ú
76-11-01
STANDS WITH A STABLIZER TRIM SHAFT WITH ú CONFIG 3 A SELF-LOCKING INSERT-AND-BOLT ú C01 Page 425 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 714-088-C03
(13) Do the Normal Operations Procedure to make sure the reverse thrust levers are correctly installed (AMM 78-31-00/501).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS-REINFORCED CONTROL ú
76-11-01 STANDS WITH A STABLIZER TRIM SHAFT WITH ú CONFIG 3 A SELF-LOCKING INSERT-AND-BOLT ú C01 Page 426
ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
START LEVERS - REMOVAL/INSTALLATION
___________________________________
1. General
_______
A. This procedure has two tasks. The first task is the removal of the start lever, the second is the installation of the start lever.
TASK 76-11-02-004-001-C01
2. Remove the Start Lever
______________________
A. Equipment
(1) Dowel Set - Thrust Lever, Control Stand,
F80195-1
B. References
(1)
AMM 26-21-51/401, Engine and APU Fire Control Module
(2)
AMM 27-09-14/201, Flight Control Cables
(3)
AMM 29-15-00/201, Hydraulic Systems A, B, and Standby
(4)
AMM 76-11-04/201, Engine Control Cables
C. Access
(1)
中國航空網 www.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(36)
