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Reference Description
COM-1557 Gauge - Force
(Part #: DG-200, Supplier: 92456, A/P Effectivity: 737-ALL)
(Part #: DPP-500G, Supplier: 92456, A/P Effectivity: 737-ALL)
(Part #: DPPH-150, Supplier: 92456, A/P Effectivity: 737-ALL)
(Part #: DPPH-50, Supplier: 92456, A/P Effectivity: 737-ALL)
(Part #: FDIX 100, Supplier: 0BFD9, A/P Effectivity: 737-ALL)
(Part #: FDIX 50, Supplier: 0BFD9, A/P Effectivity: 737-ALL)
(Part #: FDV 50, Supplier: 0BFD9, A/P Effectivity: 737-ALL)
(Opt Part #: FDI 100, Supplier: 0BFD9, A/P Effectivity: 737-ALL)
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)
STD-1107 Gauge - Feeler, 0.0 - 0.5 Inch, Readable to 1/1000th
STD-1238 Indicator - Dial
STD-1303 Caliper - Dial
D. Location Zones
Zone Area
211 Flight Compartment - Left
212 Flight Compartment - Right
311 Area Aft of Pressure Bulkhead - Left
312 Area Aft of Pressure Bulkhead - Right
334 Left Horizontal Stabilizer - Elevator
344 Right Horizontal Stabilizer - Elevator
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-32
Page 617
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
GUN 001-099, 101-122, 155, 157, 205, 207-999; GUN 156, 201-204, 206 POST SB 737-55A1080 (Continued)
E. Access Panels
Number Name/Location
311BL Stabilizer Trim Access Door
F. Prepare for the Check
SUBTASK 27-31-32-860-007
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. AILERONS, RUDDERS,
ELEVATORS, FLAPS, SPOILERS, SLATS, AND THRUST REVERSERS CAN MOVE
QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE INJURY TO
PERSONS AND DAMAGE TO EQUIPMENT.
(1) Pressurize the elevator hydraulic systems A and B. To pressurize them, do this task: Elevator
Hydraulic System A and B - Pressurization, TASK 27-31-00-800-801.
SUBTASK 27-31-32-860-008
(2) Make sure the flaps are in the full up position, do this task: Trailing Edge Flap System
Operation With Primary Control, TASK 27-51-00-860-801.
SUBTASK 27-31-32-010-002
(3) Open this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
SUBTASK 27-31-32-860-009
(4) Use the bar, SPL-1677 to set the "B" dimension at 39.89 +/- 0.01 inches (1013.2 +/- 0.3
millimeters) or 4 units of trim (Figure 603).
SUBTASK 27-31-32-860-010
(5) Operate the elevator in the full travel 6 times.
SUBTASK 27-31-32-860-011
(6) Make sure the control column is in the neutral position.
G. Do a Check of the Elevator Tab Trailing Edge Freeplay
SUBTASK 27-31-32-220-004
(1) Do a check of the elevator tab trailing edge freeplay (Figure 603):
(a) Remove pressure from the elevator hydraulic systems A and B. To remove the pressure,
do this task: Remove Pressure from the Elevator Hydraulic Systems A and B,
TASK 27-31-00-800-802.
(b) Make sure that the flaps are retracted to the full up position.
(c) Make sure the stabilizer is set to 4.0 +/- 0.5 units of trim.
CAUTION: BE VERY CAREFUL WHEN YOU INSTALL THE WOODEN BLOCK. IF YOU USE
MORE THAN HAND PRESSURE TO INSTALL THE WOODEN BLOCK, YOU CAN
CAUSE DAMAGE TO THE ELEVATOR OR TAIL CONE.
(d) Keep the elevator from moving by installing a wooden block between the inboard edge of
the elevator and the tail cone (Figure 603).
NOTE: Be sure to cover the wooden block with duct tape or equivalent so that you do not
damage the paint of the elevator or tail cone.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-32
Page 618
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
GUN 001-099, 101-122, 155, 157, 205, 207-999; GUN 156, 201-204, 206 POST SB 737-55A1080 (Continued)
CAUTION: BE VERY CAREFUL WHEN YOU INSTALL THE MOUNTING PLATE. THE ELEVATOR
IS MADE OF COMPOSITE MATERIALS. THE MOUNTING PLATE CAN CAUSE
DAMAGE TO THE ELEVATOR IF YOU ARE NOT CAREFUL. DO NOT MOVE THE
CONTROL COLUMNS. ANY MOVEMENT OF THE CONTROL COLUMNS CAN
CAUSE DAMAGE TO THE ELEVATOR OR INJURY TO PERSONS WORKING NEAR
THE ELEVATOR.
(e) Attach a mounting plate to the elevator trailing edge forward of hinge 2 of the elevator tab.
1) Put the dial indicator, STD-1238 plunger on the top of the elevator tab, approximately 0.1
inch (3 millimeters) forward of the trailing edge of the elevator tab and within 0.5 inch
(13 mm) of the inboard side of the hinge 2 centerline.
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737-600-700-800-900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册3(52)
