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GUN 156, 201-204, 206 PRE SB 737-55A1080
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 ALL
(a) Make sure the end of the bushing [104] covers the inspection hole on each tab pushrod
[110].
(b) Make sure the inspection hole of each tab pushrod end bearing is not shown.
(c) If the thread engagement is not correct, you must do the coarse adjustment again.
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 001-099, 101-122, 155, 157, 205, 207-999; GUN 156, 201-204, 206 POST SB 737-55A1080
SUBTASK 27-31-00-430-001
(17) Install lockwire on the checknuts [103] and checknuts [105] Figure 511.
GUN ALL
------------------------- END OF TASK ---------------------------
737-600/700/800/900
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Elevator Full Travel Measurements
Figure 523/27-31-00-990-826
737-600/700/800/900
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ELEVATOR - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) A removal of the elevator
(2) An installation of the elevator
(3) A removal of the elevator control pushrod
(4) An installation of the elevator control pushrod.
B. When it is necessary to balance the elevator, make sure you do a check of the elevator and the
elevator tab part numbers. Refer to Chapter 51 of the Structural Repair Manual when you balance the
elevator-elevator tab combination after the structural repairs or after you put on new paint.
C. If you install a tab on the elevator during the elevator installation, make sure the number of the
elevator control tab adjust weights agree with the tab data plate.
TASK 27-31-11-000-801
2. Elevator - Removal
(Figure 401, Figure 402, Figure 403, Figure 406)
GUN 156, 201-204, 206 PRE SB 737-55A1080; AIRPLANES WITH FOUR ELEVATOR TAB HINGES
NOTE: Also see Figure 404.
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 405.
GUN ALL
A. References
Reference Title
27-31-00-800-802 Remove Pressure from the Elevator Hydraulic Systems A and B
(P/B 201)
27-31-32-200-801 Elevator Tab Freeplay - Check (P/B 601)
27-31-32-200-802 Elevator Tab Freeplay - Check (P/B 601)
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)
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-2034 Sling - Elevator Hoisting
(Part #: C27034-1, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)
737-600/700/800/900
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C. Location Zones
Zone Area
311 Area Aft of Pressure Bulkhead - Left
318 Tail Cone Compartment - Right
334 Left Horizontal Stabilizer - Elevator
335 Left Horizontal Stabilizer - Tip
344 Right Horizontal Stabilizer - Elevator
345 Right Horizontal Stabilizer - Tip
D. Access Panels
Number Name/Location
311BL Stabilizer Trim Access Door
318BR Tailcone Access Door
333BB Horizontal Stabilizer, Access Panel, Trailing Edge
334GB Horizontal Stabilizer, Elevator Hinge Cover
334HB Horizontal Stabilizer, Elevator Hinge Cover
334JB Horizontal Stabilizer, Elevator Hinge Cover
334KB Horizontal Stabilizer, Elevator Hinge Cover
334LB Horizontal Stabilizer, Elevator Hinge Cover
　
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