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This task also includes steps to adjust the rudder forward quadrant and rudder pedals.
(4) Control Rod for Main Rudder Power Control Unit Adjustment - Use this task to adjust the control
rod for the main rudder power control unit.
(5) Control Rod for Standby Rudder Power Control Unit Adjustment - Use this test to adjust the
control rod for the standby rudder power control unit.
(6) Rudder Pedal Adjustment and Limit Travel Test - Use this test make sure the rudder pedals can
move through their full travel and the pedal adjustment crank operates correctly.
(7) Rudder Hinge Bearing and PCU Freeplay - Use this task to do a check of the freeplay of the
rudder control system.
(8) Rudder Centering Test - Use this test to make sure the rudder is in its center position.
(9) Rudder Pedal Forces Test - Use this test to make sure the rudder pedals operate with the correct
force.
(10) Rudder Travel Test - Use this test to make sure the rudder operates correctly.
(11) Standby Rudder Power Control Unit Deadband Test - Use this test to make sure the standby
rudder power control unit is in the correct rigged position.
(12) Rudder Trim System Test - Use this test to make sure the rudder system operates correctly.
(13) Wheel to Rudder Interconnect System Test - Use this test to make sure the wheel to rudder
function of the standby rudder power control unit operates correctly.
(14) Rudder Hinge Friction Test - Use this task to do a check of the rudder hinge for excessive friction.
(15) Main Rudder PCU Internal Hydraulic Leakage Test - Use this task to do a check for excessive
internal hydraulic leakage in the main rudder PCU.
(16) Rudder Override Operational Test - Use this task to verify that the override mechanisms on the
torque tube are operational.
(17) Rudder Main PCU Force Fight Monitor Test - Use this task to verify that the STBY RUD ON light
on the overhead panel P5-3 is functional.
TASK 27-21-00-820-806-002
2. Rudder Forward Quadrant Adjustment
(Figure 501)
A. General
(1) Use this test to make sure the rudder forward quadrant is adjusted correctly. After you adjust the
rudder forward quadrant, you must re-adjust the rudder pedals and control cables.
B. References
Reference Title
27-21-00-800-802 Remove Pressure from the Rudder Hydraulic Systems A, B, and
Standby (P/B 201)
27-21-00-840-802 Put the Rudder Systems A, B, and Standby Back to the Condition
Before the Pressure Removal (P/B 201)
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 006-099, 101-122; GUN 001-005, 155-157, 201-999
POST SB 737-27-1253
27-21-00
Config 2
Page 501
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(Continued)
Reference Title
32-51-00-820-802 Nose Wheel Steering System Adjustment (P/B 501)
C. 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)
D. Location Zones
Zone Area
112 Area Forward of Nose Landing Gear Wheel Well
211 Flight Compartment - Left
212 Flight Compartment - Right
311 Area Aft of Pressure Bulkhead - Left
312 Area Aft of Pressure Bulkhead - Right
E. Access Panels
Number Name/Location
112A Forward Access Door
113AW Forward Nose Wheel Well Panel
113BW Forward Nose Wheel Well Panel
114AW Forward Nose Wheel Well Panel
114BW Forward Nose Wheel Well Panel
317AL Tail Cone Access Door
F. Prepare for the Test
SUBTASK 27-21-00-860-070-002
(1) Do this task: Remove Pressure from the Rudder Hydraulic Systems A, B, and Standby,
TASK 27-21-00-800-802.
SUBTASK 27-21-00-010-017-002
(2) Open these access doors:
Number Name/Location
112A Forward Access Door
317AL Tail Cone Access Door
SUBTASK 27-21-00-010-018-002
(3) Open these access panels:
Number Name/Location
113AW Forward Nose Wheel Well Panel
113BW Forward Nose Wheel Well Panel
114AW Forward Nose Wheel Well Panel
114BW Forward Nose Wheel Well Panel
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 006-099, 101-122; GUN 001-005, 155-157, 201-999
POST SB 737-27-1253
27-21-00
Config 2
Page 502
Oct 10/2007
D633A101-GUN
　
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本文鏈接地址：737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL飛機維護手冊2(48)