bolt in the landing gear torsion link. 5) Make sure you can see the threads of the lower rod end adapter through the inspection hole in the lower rod end.
NOTE: The threads of the lower rod end adapter must cover
____ at least 50% of the inspection hole.
6) Install the bolt, the radius fillers and the nut to attach
the lower rod end to the landing gear torsion link. 7) Install the cotter pin. 8) Make sure the two rod ends align correctly. 9) Tighten the checknut on the lower rod end. 10) Make sure you can easily move the rig pin S/B-3.
S 085-006
(4)
Remove the rig pin S/B-3.
S 215-029
(5)
Make sure the cable end is between the inspection holes in the lower rod end adapter.
(a)
If the cable end is not between the inspection holes, adjust the lower telescoping assembly: 1) Remove the lower telescoping assembly from the cable and
the bracket. 2) Install the washers between the adapter and the bracket. 3) Install the lower telescoping assembly and the cable on the
bracket. 4) Make sure the cable end is between the inspection holes in the lower rod end adapter. 5) Hold the guide tube and torque the lower rod end adapter to 25-40 inch pounds.
S 215-007
(6)
Make sure you can see the swivel tube through the inspection hole in the guide tube.
(a)
If the swivel tube is not visible through the inspection hole in the guide tube, adjust the upper rod end: 1) Adjust the upper rod end. 2) Remove the lower rod end from the landing gear torsion
link. 3) Manually retract and extend the cable to verify that the cable and valve lever move freely and do not bind. 4) Make sure you can see the threads of the upper rod end adapter through the inspection hole in the upper rod end.
NOTE: The threads of the upper rod end adapter must cover
____ at least 50% of the inspection hole.
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27-62-51
ALL ú ú 02 Page 504 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
5) Install the bolt, the radius fillers and the nut to attach
the lower rod end to the landing gear torsion link. 6) Install the cotter pin. 7) Tighten the checknut on the lower rod end. 8) Tighten the checknut on the upper rod end. 9) Make sure that you can easily install the rig pin S/B-3
through the valve lever. 10) Install the lockwire.
S 415-008
(7)
Attach the protective boot to the spacer:
(a)
Install the clamp with the worm screw forward and the thumb flats inboard.
S 725-009
(8)
Do the functional test of the interlock valve cable.
S 585-010
(9)
Lower the airplane and remove the jacks (AMM 07-11-11/201).
TASK 27-62-51-725-011
3. Ground Spoiler Interlock Valve Cable Functional Test
____________________________________________________
A. References
(1)
AMM 07-11-11/201, Jack Airplane
(2)
AMM 07-11-31/201, Jack Airplane Axles
(3)
AMM 12-15-31/301, Main Landing Gear Shock Strut
(4)
AMM 24-22-00/201, Manual Control
(5)
AMM 27-62-00/201, Speed Brake Control System
B.
Access
(1)
Location Zone
217 Right Main Wheel Well
C.
Prepare for the Functional Test
S 585-012
(1)
Lift the airplane with the jacks until the right main gear shock strut is fully extended (AMM 07-11-11/201).
(2)
Supply the electrical power (AMM 24-22-00/201).
S 865-014
(3)
Supply the system A hydraulic power (AMM 27-62-00/201).
D.
Do the Functional Test
S 865-013
S 865-015
(1)
Move the speed brake lever to the UP position.
(a)
Make sure the ground spoilers do not move.
S 865-016
(2) Release the air pressure in the shock strut for the right main landing gear.
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本文链接地址：737-300 400 500 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 5(132)
