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Page 420
Jun 10/2004
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
SUBTASK 27-21-51-730-001
(6) Do this task: Rudder Trim System Test, TASK 27-21-00-700-819-001 or Rudder Trim System
Test, TASK 27-21-00-700-819-002.
SUBTASK 27-21-51-010-006
(7) Close this access panel:
Number Name/Location
324CL Vertical Fin, Access
SUBTASK 27-21-51-410-001
(8) Close this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
SUBTASK 27-21-51-410-002
(9) Close this access panel:
Number Name/Location
112A Forward Access Door
SUBTASK 27-21-51-010-007
(10) Install these access panels:
Number Name/Location
113AC Fwd Nose Wheel Well Upper Access Panel
114AC Fwd Nose Wheel Well Upper Access Panel
and .
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Page 421
Jun 10/2004
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RUDDER FORWARD QUADRANT - INSPECTION/CHECK
1. General
A. This procedure has this inspection task:
(1) Rudder Mechanical Control Path
TASK 27-21-51-210-801
2. Rudder Mechanical Control Path Inspection
(Figure 601)
A. Location Zones
Zone Area
112 Area Forward of Nose Landing Gear Wheel Well
B. Access Panels
Number Name/Location
112A Forward Access Door
C. Procedure
SUBTASK 27-21-51-010-009
(1) To get access to the rudder mechanical control path, do this task:
Open this access panel:
Number Name/Location
112A Forward Access Door
SUBTASK 27-21-51-210-001
(2) Do a general visual inspection of the rudder mechanical control path.
SUBTASK 27-21-51-010-010
(3) Close this access panel:
Number Name/Location
112A Forward Access Door
------------------------- END OF TASK ---------------------------
737-600/700/800/900
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EFFECTIVITY
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Page 601
Oct 10/2003
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Rudder and Rudder Trim Control System - Rudder Pedals and Forward Quadrants
Figure 601/27-21-51-990-804
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Page 602
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RUDDER AFT QUADRANT - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) A removal of the rudder aft quadrant
(2) An installation of the rudder aft quadrant.
B. The rudder aft quadrant includes the quadrant, quadrant shaft, and two bearing housings.
TASK 27-21-61-000-801
2. Rudder Aft Quadrant Removal
(Figure 401, Figure 402)
A. References
Reference Title
27-21-00-800-802 Remove Pressure from the Rudder Hydraulic Systems A, B, and
Standby (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
311 Area Aft of Pressure Bulkhead - Left
324 Vertical Fin - Rear Spar To Trailing Edge
D. Access Panels
Number Name/Location
112A Forward Access Door
113AC Fwd Nose Wheel Well Upper Access Panel
114AC Fwd Nose Wheel Well Upper Access Panel
311BL Stabilizer Trim Access Door
323FL Vertical Fin, Access
323GL Vertical Fin, Access
324CL Vertical Fin, Access
E. Prepare for the Removal
SUBTASK 27-21-61-860-003
(1) Do this task: Remove Pressure from the Rudder Hydraulic Systems A, B, and Standby,
TASK 27-21-00-800-802.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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SUBTASK 27-21-61-010-004
(2) Open this access panel:
Number Name/Location
112A Forward Access Door
SUBTASK 27-21-61-010-007
(3) Remove these access panels:
Number Name/Location
　
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