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EFFECTIVITY
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Page 602
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D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Elevator Balance Panel Wear Limits
Figure 601 (Sheet 1 of 2)/27-31-41-990-803
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Elevator Balance Panel Wear Limits
Figure 601 (Sheet 2 of 2)/27-31-41-990-803
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-41
Page 604
Feb 10/2006
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
CONTROL COLUMN - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) A removal of a control column
(2) An installation of a control column.
B. This procedure is applicable for the captain’s and first officer’s control column.
TASK 27-31-51-000-801
2. Control Column - Removal
(Figure 401)
A. References
Reference Title
27-31-00-800-802 Remove Pressure from the Elevator Hydraulic Systems A and B
(P/B 201)
B. Tools/Equipment
NOTE: When more than one tool part number is listed under the same "Reference" number, the
tools shown are alternates to each other within the same airplane series. Tool part numbers
that are replaced or non-procurable are preceded by "Opt:", which stands for Optional.
Reference Description
SPL-1585 Kit - Rigging Pins, All Systems
(Part #: F70207-109, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)
C. Location Zones
Zone Area
112 Area Forward of Nose Landing Gear Wheel Well
211 Flight Compartment - Left
212 Flight Compartment - Right
D. Access Panels
Number Name/Location
112A Forward Access Door
E. Prepare for the Removal
SUBTASK 27-31-51-860-001
(1) Do this task: Remove Pressure from the Elevator Hydraulic Systems A and B,
TASK 27-31-00-800-802.
SUBTASK 27-31-51-860-002
(2) Open these circuit breakers and install safety tags:
CAPT Electrical System Panel, P18-2
Row Col Number Name
E 7 C01208 STALL WARN ASYM MODE
F/O Electrical System Panel, P6-2
Row Col Number Name
B 10 C00207 FLIGHT CONTROL STAB TRIM CONT
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Page 401
Oct 10/2006
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Row Col Number Name
B 13 C00363 FLIGHT CONTROL SHUTOFF VALVES FLT CONT
C 13 C01074 FLIGHT CONTROL SHUTOFF VALVES FLT CONT
D 10 C00840 FLIGHT CONTROL STAB TRIM ACTUATOR
SUBTASK 27-31-51-010-001
(3) Open this access panel:
Number Name/Location
112A Forward Access Door
SUBTASK 27-31-51-480-001
(4) Install the rig pin E-1 from the rig pin kit, SPL-1585 in the left forward quadrant.
F. Control Column Removal
SUBTASK 27-31-51-020-001
(1) Disconnect the electrical wire [11] for the control column shaker [13] from the terminal strip in
the lower nose compartment.
SUBTASK 27-31-51-020-004
(2) Disconnect the electrical wire [5] to the control column [1] from the terminal strip in the lower
nose compartment.
SUBTASK 27-31-51-020-002
(3) Remove the ring assemblies and dust seals:
(a) Remove the screws [15] and washers [16] from the forward ring assembly [14] and aft ring
assembly [17].
(b) Remove the forward ring assembly [14] and aft ring assembly [17].
(c) Remove the aft dust seal [18] and forward dust seal [19].
SUBTASK 27-31-51-020-003
(4) Remove the control column [1]:
CAUTION: HOLD THE CONTROL COLUMN WHEN YOU REMOVE THE COUPLINGS. THE
CONTROL COLUMN CAN FALL AND CAUSE DAMAGE TO EQUIPMENT.
(a) Hold the control column while you remove the nuts [7], washers [8], and bolts [12] from the
outboard couplings [9].
(b) Remove the outboard couplings [9].
(c) Lift and remove the control column [1] from the forward quadrant assembly.
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Control Column Installation
Figure 401 (Sheet 1 of 6)/27-31-51-990-801
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Oct 10/2003
　
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