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point, adjust the tab rod end until a minimum travel of 0.040 inch (1.02 millimeters) is
achieved.
a) If it was necessary to adjust the tab rods, make sure you torque the check nuts to
the proper torque and do a check of the rod end rotation from contact point to
contact point.
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
SUBTASK 27-31-00-420-010
(12) Install lockwire on the checknuts [103] and checknuts [105] (Figure 510).
GUN ALL
H. Put the Airplane Back to Its Usual Condition
SUBTASK 27-31-00-410-005
(1) Install these access panels:
Number Name/Location
334PT Horizontal Stabilizer, Tab Control Rod Fairing
344PT Horizontal Stabilizer, Tab Control Rod Fairing,
Elevator Sta 34.0
SUBTASK 27-31-00-940-006
(2) Close this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
SUBTASK 27-31-00-860-039
(3) Do this task: Put the Elevator Systems A and B Back to the Condition Before the Pressure
Removal, TASK 27-31-00-840-802.
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-00
Page 547
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Elevator Tab Pushrods Adjustment
Figure 508/27-31-00-990-821
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 156, 201-204, 206 PRE SB 737-55A1080 27-31-00
Page 548
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Elevator Tab Pushrods Adjustment
Figure 509/27-31-00-990-839
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 156, 201-204, 206 PRE SB 737-55A1080 27-31-00
Page 549
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Elevator Tab Pushrods Adjustment
Figure 510/27-31-00-990-810
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
27-31-00
Page 550
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Elevator Tab Pushrods Adjustment
Figure 511/27-31-00-990-827
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
27-31-00
Page 551
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Elevator Tab Fixture Bar Installation
Figure 512 (Sheet 1 of 2)/27-31-00-990-811
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN 156, 201-204, 206 PRE SB 737-55A1080; AIRPLANES
WITH FOUR ELEVATOR TAB HINGES
27-31-00
Page 552
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Elevator Tab Fixture Bar Installation
Figure 512 (Sheet 2 of 2)/27-31-00-990-811
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; AIRPLANES WITH SIX
HINGE ELEVATOR TABS
27-31-00
Page 553
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
TASK 27-31-00-820-806
11. Input Rod of the Elevator Feel Computer - Adjustment
(Figure 502, Figure 513)
A. General
(1) Use this test to adjust the input rod (stabilizer pushrod) of the elevator feel computer.
B. References
Reference Title
22-11-31-710-801 Stabilizer Position Sensor Test (P/B 501)
27-31-00-700-801 Null Procedure - Mach Trim Actuator (P/B 201)
27-31-00-800-802 Remove Pressure from the Elevator Hydraulic Systems A and B
(P/B 201)
27-31-00-840-802 Put the Elevator Systems A and B Back to the Condition Before the
Pressure Removal (P/B 201)
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,
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737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册2(146)
