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737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-35
Page 402
Feb 10/2005
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Elevator Tab Control Valve Installation
Figure 401 (Sheet 2 of 2)/27-31-35-990-801
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-35
Page 403
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TASK 27-31-35-400-801
3. Elevator Tab Control Valve - Installation
(Figure 401)
A. References
Reference Title
27-31-00-700-815 Elevator Tab Control System - Operational Test (P/B 501)
27-31-00-800-801 Elevator Hydraulic System A and B - Pressurization (P/B 201)
B. Consumable Materials
Reference Description Specification
D00153 Fluid - Hydraulic, Erosion Arresting, Fire Resistant BMS3-11, Type
IV
(interchange~
able&
intermixable
with Type V)
C. Expendables/Parts
AMM Item Description AIPC Reference AIPC Effectivity
9 Packing 27-31-31-02-075 GUN 001-028, 101-121,
155-157, 201-999
11 Control valve 27-31-31-02-015 GUN ALL
27-31-31-02-077 GUN 001-028, 101-121,
155-157, 201-999
D. Location Zones
Zone Area
318 Tail Cone Compartment - Right
E. Access Panels
Number Name/Location
318BR Tailcone Access Door
F. Control Valve Installation
SUBTASK 27-31-35-860-002
(1) Make sure hydraulic power is removed from the elevator hydraulic systems A and B. To remove
it, do this task: Elevator Hydraulic System A and B - Pressurization, TASK 27-31-00-800-801.
SUBTASK 27-31-35-420-001
(2) If the unions and packings are not installed in the control valve [11], then do these steps:
(a) Lubricate the unions and new packings with fluid, D00153.
(b) Install the new packings [9] and unions [8] to the control valve [11].
SUBTASK 27-31-35-420-002
(3) Install the control valve [11] to the airplane structure.
(a) Install the bolts [6] and washers [7] in the control valve [11].
(b) Remove the caps and plugs from the hydraulic [10] and electrical [5] lines.
(c) Connect the hydraulic lines [10] to the control valve [11].
(d) Connect the electrical line [5] to the control valve [11].
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Page 404
Oct 10/2007
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SUBTASK 27-31-35-730-001
(4) Do this task: Elevator Tab Control System - Operational Test, TASK 27-31-00-700-815.
G. Put the Airplane Back to Its Usual Condition
SUBTASK 27-31-35-410-001
(1) Install this access panel:
Number Name/Location
318BR Tailcone Access Door
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Page 405
Jun 10/2007
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ELEVATOR FEEL COMPUTER - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) A removal of the elevator feel computer
(2) An installation of the elevator feel computer.
TASK 27-31-37-000-801
2. Elevator Feel Computer - Removal
(Figure 401)
A. References
Reference Title
20-10-51-000-801 Flareless Tubing Assembly Removal (P/B 401)
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-1673 Pin - Safety, Elevator Feel Computer
(Part #: F80153-1, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
SPL-1677 Assembly - Trammel Bar, Stabilizer Trim Actuator
(Part #: F80055-1, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
C. Location Zones
Zone Area
311 Area Aft of Pressure Bulkhead - Left
312 Area Aft of Pressure Bulkhead - Right
D. Access Panels
Number Name/Location
311BL Stabilizer Trim Access Door
E. Prepare for the Removal
SUBTASK 27-31-37-010-001
(1) Open this access panel:
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737-600-700-800-900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册3(64)
