27-09-11
ALL ú ú 01 Page 2 ú Jul 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
~.............................................................................. | Table 1 | ................................................................................ | CONTROL | | | | SYSTEM | CABLE CODE | CABLE FUNCTION | ................................................................................ | Spoilers | WSA1 | Wing Spoilers-Outboard spoilers up | | ................................................................. | | WSB1 | Wing Spoilers-Outboard spoilers down | | ................................................................. | | WSA2 | Wing Spoilers-Inboard spoilers up | | ................................................................. | | WSB2 | Wing Spoilers-Inboard spoilers down | ................................................................................ | Speed Brakes | SBA | Speed Brake Control-Speed Brake on | | ................................................................. | | SBB | Speed Brake Control-Speed Brake off | 2..............…............…..................................................1
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27-09-11
ALL ú ú 01 Page 3 ú Mar 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
FLIGHT CONTROL CABLES - MAINTENANCE PRACTICES
_____________________________________________
1. General_______
A. There are two tasks in this procedure. The first task is the identification and assembly specifications of the control cable. The second task is the rigging of the control cables.
TASK 27-09-14-862-007
2. Control Cables Identification and Assembly Specifications_________________________________________________________
A. General
_______
(1)
Refer to AMM 20-10-91/401 for the removal and installation of the control cables.
B.
References
(1)
AMM 20-10-91/401, Control Cables
C.
Access
(1)
Location Zone
208 Forward Cargo Compartment
218 Aft Cargo Compartment
216 Main Wheel Well, LH
217 Main Wheel Well, RH
D.
Identify and Make Control Cable Assemblies
S 862-002
(1)
Identify and make control cable assemblies for the flight control systems (Fig. 201 thru 208).
S 862-003
(2)
Swage control cables with dies for the next larger size AN standard terminals for all BACT14A terminals.
TASK 27-09-14-832-008
3. Control Cables Rigging______________________
A. General
(1)
It is necessary to test the cycle of the control cables of a system after the replacement of the cable. Refer to the applicable system for the rigging loads.
B.
References
(1)
AMM 27-11-00/501, Aileron and Aileron Trim Control System
(2)
AMM 27-21-00/501, Rudder and Rudder Trim Control System
(3)
AMM 27-31-00/501, Elevator and Tab Control System
(4)
AMM 27-41-00/501, Horizontal Stabilizer Trim Control System
(5)
AMM 27-51-00/501, Trailing Edge Flap System
(6)
AMM 27-61-00/501, Spoiler Control System
(7)
AMM 27-62-00/501, Speed Brake Control System
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27-09-14
ALL ú ú 01 Page 201 ú Nov 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
AILERON CONTROL
QUADRANTS
AILERON AILERON CONTROL
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