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1) Install the bolts [19], washers [20] (under the bolt), washers [21] (under the nut), and
nuts [22].
2) Install the bolts [14], washers [15] (under the bolt), washers [16] (under the nut), and
nuts [17].
(d) Install the bolts [4], washers [5], and nuts [6] to attach the upper bearing housing [2] and
plate [3] to the airplane structure.
SUBTASK 27-21-82-210-001
(3) Examine the feel output rod [9] for damage.
NOTE: The feel output rod has two load paths.
SUBTASK 27-21-82-420-002
(4) Connect the feel and centering unit crank [8] to the rudder feel output rod [8]:
(a) Install the bolt assembly [28], bushing [29], washer [30], washer [31], and nut [32].
1) Tighten the nut [32] to 45-60 pound-inches (5.1-6.8 newton-meters).
CAUTION: DO NOT TRY TO TIGHTEN THE NUT [32] AGAIN AFTER YOU TIGHTEN THE NUT
[33], YOU CAN CAUSE DAMAGE TO EQUIPMENT.
(b) Install the nut [33].
1) Tighten the nut [33] to 12-15 pound-inches (1.3-1.7 newton-meters).
SUBTASK 27-21-82-480-002
(5) Install the rig pin R-5 of the rig pin kit, SPL-1585 from the rudder feel and centering unit [7].
SUBTASK 27-21-82-420-003
(6) Connect the rudder trim actuator [1] to the rudder feel and centering unit [7]:
(a) Install the bolt assembly [23], washer [24], and nut [25].
1) Tighten the nut [25] to 85-100 pound-inches (9.6-11.3 newton-meters).
CAUTION: DO NOT TRY TO TIGHTEN THE NUT [25] AGAIN AFTER YOU TIGHTEN THE NUT
[27], YOU CAN CAUSE DAMAGE TO EQUIPMENT.
(b) Install the washer [26] and nut [27].
(c) Tighten the nut [27] to 30-35 pound-inches (3.9-4.0 newton-meters).
SUBTASK 27-21-82-080-001
(7) Remove the rig pins R-3 or R-4 of the rig pin kit, SPL-1585 from the rudder forward quadrants.
SUBTASK 27-21-82-080-002
(8) Remove the rig pin R-5 of the rig pin kit, SPL-1585 from the rudder feel and centering unit.
F. Rudder Feel and Centering Unit Test
SUBTASK 27-21-82-020-002
(1) Disconnect the steering for the nose landing gear from the rudder system
NOTE: It is not necessary to disconnect the steering if the airplane is on jacks and the nose
landing gear is fully extended.
SUBTASK 27-21-82-860-004
(2) Do this task: Rudder Hydraulic System A, B, or Standby Pressurization,
TASK 27-21-00-800-801.
SUBTASK 27-21-82-700-001
(3) Test the Feel and Centering System:
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(a) Operate the rudder pedals through their full travel range three times.
(b) Make sure the rudder trim indicator shows zero units of trim.
(c) Push the captain’s left rudder pedal forward approximately 0.5 inch and release it.
1) Make sure each side of the rudder trailing edge aligns with the tab on the rudder index
plate.
(d) Push the captain’s right rudder pedal forward approximately 0.5 inch and release it.
1) Make sure each side of the rudder trailing edge aligns with the tab on the rudder index
plate.
SUBTASK 27-21-82-420-004
(4) Connect the steering for the nose landing gear to the rudder system if it disconnects.
SUBTASK 27-21-82-730-002
(5) Do this task: Rudder Pedal Forces Test, TASK 27-21-00-700-816-001 or Rudder Pedal Forces
Test, TASK 27-21-00-700-816-002.
SUBTASK 27-21-82-730-001
(6) Do this task: Rudder Travel Test, TASK 27-21-00-700-817-001 or Rudder Travel Test,
TASK 27-21-00-700-817-002.
G. Put the Airplane Back to Its Usual Condition
SUBTASK 27-21-82-860-005
(1) Do this task: Put the Rudder Systems A, B, and Standby Back to the Condition Before the
Pressure Removal, TASK 27-21-00-840-802.
SUBTASK 27-21-82-410-004
(2) Install this access panel:
Number Name/Location
324DR Vertical Fin, Trailing Edge Access
SUBTASK 27-21-82-410-003
(3) Install this access panel:
Number Name/Location
324DL Trailing Edge Access
SUBTASK 27-21-82-410-001
(4) Install this access panel:
Number Name/Location
324BL Vertical Fin, Trailing Edge Access
SUBTASK 27-21-82-010-004
(5) Install these access panels:
Number Name/Location
113AC Fwd Nose Wheel Well Upper Access Panel
114AC Fwd Nose Wheel Well Upper Access Panel
and .
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SUBTASK 27-21-82-410-002
(6) Close this access panel:
Number Name/Location
112A Forward Access Door
------------------------- END OF TASK ---------------------------
　
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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(107)