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NOTE: See Figure 508 or Figure 509.
GUN 001-099, 101-122, 155, 157, 205, 207-999; GUN 156, 201-204, 206 POST SB 737-55A1080
NOTE: See Figure 511.
GUN 101-122
NOTE: See Figure 517.
GUN 156, 201-204, 206 PRE SB 737-55A1080
NOTE: See Figure 518.
GUN 001-099, 155, 157, 205, 207-999; GUN 156, 201-204, 206 POST SB 737-55A1080
NOTE: See Figure 519.
GUN ALL
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-00
Page 598.28
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
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-1677 Assembly - Trammel Bar, Stabilizer Trim Actuator
(Part #: F80055-1, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
SPL-1686 Fixture - Bar, Elevator Tab
(Part #: C27028-21, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
(Opt Part #: C27028-1, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
(Opt Part #: F80248-8, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500)
C. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
334 Left Horizontal Stabilizer - Elevator
344 Right Horizontal Stabilizer - Elevator
D. Access Panels
Number Name/Location
311BL Stabilizer Trim Access Door
334PT Horizontal Stabilizer, Tab Control Rod Fairing
344PT Horizontal Stabilizer, Tab Control Rod Fairing, Elevator Sta 34.0
E. Elevator Tab Pushrod Adjustment.
SUBTASK 27-31-00-970-001
(1) Get the number and direction (airplane nose up or airplane nose down) of stabilizer wheel turns
necessary to trim the airplane during the power-off flight test.
SUBTASK 27-31-00-970-004
(2) Get the record of the Center of Gravity that was made during the power-off flight test.
SUBTASK 27-31-00-010-027
(3) Open this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
SUBTASK 27-31-00-010-028
(4) For the left elevator tab pushrods, remove this access panel:
Number Name/Location
334PT Horizontal Stabilizer, Tab Control Rod Fairing
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-00
Page 598.29
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
SUBTASK 27-31-00-010-029
(5) For the right elevator tab pushrods, remove this access panel:
Number Name/Location
344PT Horizontal Stabilizer, Tab Control Rod Fairing,
Elevator Sta 34.0
SUBTASK 27-31-00-480-011
(6) Use the bar, SPL-1677 to set the "B" dimension to 39.89 +/-0.01 inches (1013.2 +/- 0.3 mm)
(Figure 502).
SUBTASK 27-31-00-980-001
(7) Push the elevator trailing edge full up by hand.
SUBTASK 27-31-00-820-012
(8) Then, while you move the elevator down from the trailing edge up position, align the elevator
with the index mark in +/- 0.04 inches (+/- 1.0 mm), or less (Figure 505).
NOTE: Keep the elevators at this position while you adjust the tab pushrods. If the elevator
position is changed, you must put the elevator trailing edge at full up position and do
this step again before you continue.
SUBTASK 27-31-00-480-012
(9) Install the fixture, SPL-1686 (Figure 512):
GUN 156, 201-204, 206 PRE SB 737-55A1080; AIRPLANES WITH FOUR ELEVATOR TAB HINGES
(a) Install the fixture, SPL-1686 below the elevator and elevator tab at the inboard side of the
second elevator tab hinge.
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
(b) Install the fixture, SPL-1686 below the elevator and elevator tab at the inboard side of the
third elevator tab hinge.
GUN ALL
(c) Make sure the cross bar on the fixture, SPL-1686 touches the lower surface of the elevator
trailing edge.
GUN 156, 201-204, 206 PRE SB 737-55A1080; AIRPLANES WITH FOUR ELEVATOR TAB HINGES
SUBTASK 27-31-00-820-013
(10) Adjust the elevator tab pushrods [110] using the Elevator Tab Rig Adjustment Chart:
GUN 156, 201-204, 206 PRE SB 737-55A1080
　
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