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Figure 406 (Sheet 1 of 2)/27-31-34-990-808
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-34
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Elevator Tab Control Mechanism Installation
Figure 406 (Sheet 2 of 2)/27-31-34-990-808
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-34
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Elevator Tab Control Mechanism Installation
Figure 407/27-31-34-990-813
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 156, 201-204, 206 PRE SB 737-55A1080 27-31-34
Page 414
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Elevator Tab Control Mechanism Installation
Figure 408/27-31-34-990-814
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 001-099, 101-122, 155, 157, 205, 207-999; GUN 156, 201-
204, 206 POST SB 737-55A1080
27-31-34
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TASK 27-31-34-000-803
4. Elevator Tab Pushrod - Removal
(Figure 401)
GUN 156, 201-204, 206 PRE SB 737-55A1080; AIRPLANES WITH FOUR ELEVATOR TAB HINGES
NOTE: Also see Figure 402, Figure 404 and Figure 407.
GUN 001-099, 101-122, 155, 157, 205, 207-999; GUN 156, 201-204, 206 POST SB 737-55A1080; AIRPLANES
WITH THE SIX HINGE ELEVATOR TAB WITH RECTANGULAR HEAD BOLTS
NOTE: Also see Figure 403, Figure 405 and Figure 408.
GUN ALL
A. General
(1) This task is applicable for two left elevator tab and two right elevator tab pushrods.
B. References
Reference Title
27-31-00-800-802 Remove Pressure from the Elevator Hydraulic Systems A and B
(P/B 201)
27-31-00-820-805 Elevator Tab Pushrods - 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
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
E. Access Panels
Number Name/Location
318BR Tailcone Access Door
333BB Horizontal Stabilizer, Access Panel, Trailing Edge
343BB Horizontal Stabilizer, Access Panel - T.E. Area
F. Prepare for the Removal
SUBTASK 27-31-34-860-005
(1) Remove pressure 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.
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EFFECTIVITY
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SUBTASK 27-31-34-010-007
(2) To get access to the aft control quadrant, do this task:
Remove this access panel:
Number Name/Location
318BR Tailcone Access Door
SUBTASK 27-31-34-010-008
(3) For the left elevator, remove this access panel:
Number Name/Location
333BB Horizontal Stabilizer, Access Panel, Trailing Edge
SUBTASK 27-31-34-010-009
(4) For the right elevator, remove this access panel:
Number Name/Location
343BB Horizontal Stabilizer, Access Panel - T.E. Area
SUBTASK 27-31-34-480-003
(5) Install the rig pin E-5 from rig pin kit, SPL-1585 in the aft control quadrant (Figure 401).
SUBTASK 27-31-34-220-002
(6) Measure the elevator tab position. To measure it, do this task: Elevator Tab Pushrods -
Adjustment, TASK 27-31-00-820-805.
(a) Keep a record of the elevator tab position.
G. Tab Pushrod Removal
SUBTASK 27-31-34-020-008
(1) Remove the bolts [24] that attach the access panel [23] to the elevator [21].
SUBTASK 27-31-34-020-009
(2) Remove the tab pushrod [29]:
(a) Remove the screws [48] from the pin retainer [49].
(b) Remove the pin [53], nut [25], washer [26], bushing [27], and bolt [28] from the tab pushrod
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737-600-700-800-900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册3(58)
