曝光台 注意防骗
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C. Location Zones
Zone Area
318 Tail Cone Compartment - Right
333 Left Horizontal Stabilizer - Rear Spar to Trailing Edge
334 Left Horizontal Stabilizer - Elevator
343 Right Horizontal Stabilizer - Rear Spar to Trailing Edge
344 Right Horizontal Stabilizer - Elevator
D. Access Panels
Number Name/Location
318BR Tailcone Access Door
333BB Horizontal Stabilizer, Access Panel, Trailing Edge
343BB Horizontal Stabilizer, Access Panel - T.E. Area
E. Tab Mechanism Installation
SUBTASK 27-31-34-860-008
(1) Make sure hydraulic power is removed from the elevator hydraulic systems A and B. To remove
it, do this task: Remove Pressure from the Elevator Hydraulic Systems A and B,
TASK 27-31-00-800-802.
SUBTASK 27-31-34-420-007
(2) Install the elevator tab lock actuator [78]:
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(a) Install the bolt [71] and washer [72], bushing [73], washer [74], and nut [75].
(b) Install the bolt [76], bushings [77], washer [79], and nut [80].
NOTE: The bolt [76] is installed with the head pointing inboard on both the left and right
actuator mechanisms. This will allow the full removal of the bolt from the actuator
mechanism without it contacting adjacent structure.
SUBTASK 27-31-34-420-008
(3) Connect the hydraulic line.
(a) Remove the caps and plugs from the hydraulic and electrical lines.
(b) Connect hydraulic line [31] from the crank assembly [32].
SUBTASK 27-31-34-080-004
(4) Remove rig pin E-5 of the rig pin kit, SPL-1585 from the aft control quadrant (Figure 401).
SUBTASK 27-31-34-730-013
(5) Do this task: Elevator Tab Control System - Operational Test, TASK 27-31-00-700-815.
F. Put the Airplane Back to Its Usual Condition
SUBTASK 27-31-34-410-013
(1) For the left elevator, install this access panel:
Number Name/Location
333BB Horizontal Stabilizer, Access Panel, Trailing Edge
SUBTASK 27-31-34-410-014
(2) For the right elevator, install this access panel:
Number Name/Location
343BB Horizontal Stabilizer, Access Panel - T.E. Area
SUBTASK 27-31-34-410-015
(3) Install this access panel:
Number Name/Location
318BR Tailcone Access Door
------------------------- END OF TASK ---------------------------
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ELEVATOR TAB CONTROL MECHANISM - INSPECTION/CHECK
1. General
A. This procedure has these inspection tasks:
(1) Elevator Balance Weight Installation and Elevator Tab Control Mechanism General Visual
Inspection
TASK 27-31-34-210-801
2. Elevator Balance Weight Installation and Elevator Tab Control Mechanism - General Visual Inspection
A. Location Zones
Zone Area
334 Left Horizontal Stabilizer - Elevator
344 Right Horizontal Stabilizer - Elevator
B. Access Panels
Number Name/Location
333BB Horizontal Stabilizer, Access Panel, Trailing Edge
333CB Horizontal Stabilizer, Access Panel, Trailing Edge
333DB Horizontal Stabilizer, Access Panel, Trailing Edge
334PT Horizontal Stabilizer, Tab Control Rod Fairing
343BB Horizontal Stabilizer, Access Panel - T.E. Area
343CB Horizontal Stabilizer, Access Panel - T.E. Area
343DB Horizontal Stabilizer, Access Panel - T.E. Area
344PT Horizontal Stabilizer, Tab Control Rod Fairing, Elevator Sta 34.0
C. Procedure
SUBTASK 27-31-34-010-014
(1) Remove these access panels to get access to the left Elevator Tab Control Mechanism:
Number Name/Location
333BB Horizontal Stabilizer, Access Panel, Trailing Edge
333CB Horizontal Stabilizer, Access Panel, Trailing Edge
333DB Horizontal Stabilizer, Access Panel, Trailing Edge
334PT Horizontal Stabilizer, Tab Control Rod Fairing
SUBTASK 27-31-34-010-010
(2) Remove these access panels to get access to the right Elevator Tab Control Mechanism:
Number Name/Location
343BB Horizontal Stabilizer, Access Panel - T.E. Area
343CB Horizontal Stabilizer, Access Panel - T.E. Area
343DB Horizontal Stabilizer, Access Panel - T.E. Area
344PT Horizontal Stabilizer, Tab Control Rod Fairing,
Elevator Sta 34.0
SUBTASK 27-31-34-210-001
(3) Do a general visual inspection of the left and right elevator balance weight installations and
elevator tab control mechanisms (Figure 601 or Figure 602 Figure 601 or Figure 602).
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
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737-600-700-800-900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册3(62)
