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[29] and elevator tab [22]. Discard the pin [53].
GUN 156, 201-204, 206 PRE SB 737-55A1080; AIRPLANES WITH FOUR ELEVATOR TAB HINGES
(c) Remove the nut [47], washer [46], and bolt [41] from the elevator tab control mechanism
[32] and tab pushrod [29].
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
(d) Remove the nut [47], washer [46], spacer [53], and the bolt [41] from the elevator tab control
mechanism [32] and tab pushrod [29].
GUN ALL
(e) Disconnect the tab pushrod [29] from the elevator tab control mechanism [32].
(f) Remove the tab pushrod [29] from the airplane.
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-34
Page 417
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
TASK 27-31-34-400-803
5. Elevator Tab Pushrod - Installation
(Figure 401)
GUN 156, 201-204, 206 PRE SB 737-55A1080
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
NOTE: Also see Figure 403, Figure 405 and Figure 408.
GUN ALL
A. References
Reference Title
27-31-00-700-804 Elevator Travel Limit - Test (P/B 501)
27-31-00-700-806 Elevator Tab Linkage - Test (P/B 501)
27-31-00-700-809 Control Column Power Force - Test (P/B 501)
27-31-00-710-803 Elevator Power-Off Flight - Test (P/B 501)
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)
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
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
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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E. Tab Pushrod Installation
SUBTASK 27-31-34-860-006
(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 27-31-34-420-004
(2) Install the tab pushrods [29]:
(a) Put the tab pushrods [29] in its position.
NOTE: If you loosened or removed the nuts [47] or nuts [25], they need to be replaced
with new nuts. Using new nuts will ensure that they have the required run-on
torque.
GUN 156, 201-204, 206 PRE SB 737-55A1080; AIRPLANES WITH FOUR ELEVATOR TAB HINGES
(b) Install the bolts [41], washers [46], and new nuts [47] to connect the tab pushrods [29] to the
elevator tab control mechanism [32].
NOTE: The inboard bolt is installed with the head inboard and the outboard bolt is
installed with the head outboard.
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
(c) Install the spacers [53], bolts [41], washers [46], and new nuts [47] to connect the tab
pushrods [29] to the elevator tab control mechanism [32].
NOTE: The inboard bolt is installed with the head inboard and the outboard bolt is
installed with the head outboard.
GUN 156, 201-204, 206 PRE SB 737-55A1080
CAUTION: IF THE NEW NUTS [47] ARE NOT TIGHTENED CORRECTLY, THEN THE PUSHRODS
CAN BECOME DISCONNECTED AND CAUSE DAMAGE TO THE ELEVATOR AND
STABILIZER.
(d) Tighten the new nuts [47] to 50 - 80 pound-inches (5.7 - 9.0 newton-meters).
GUN 001-099, 101-122, 155, 157, 205, 207-999; GUN 156, 201-204, 206 POST SB 737-55A1080
CAUTION: IF THE NEW NUTS [47] ARE NOT TIGHTENED CORRECTLY, THEN THE PUSHRODS
　
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