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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
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-1278 Block - Loading, 1/8 Inch Thick, 3 Inch by 3 Inch Wood or Fiberglass
Block with Pad to Prevent Damage to the Skin.
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
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BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
E. Access Panels
Number Name/Location
311BL Stabilizer Trim Access Door
F. Prepare for the Check
SUBTASK 27-31-32-860-019
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 27-31-32-860-020
(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 27-31-32-010-004
(3) Open this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
SUBTASK 27-31-32-860-021
(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 601).
SUBTASK 27-31-32-860-022
(5) Operate the elevator in the full travel 6 times.
SUBTASK 27-31-32-860-023
(6) Make sure the control column is in the neutral position.
G. Do a Check of the Buss Linkage of the Elevator Output Torque Tube
SUBTASK 27-31-32-220-010
CAUTION: DO NOT PUT A LOAD OF MORE THAN 65 POUNDS (290 NEWTONS) ON THE
ELEVATORS AT ONE TIME. IF THE LOAD IS TOO HEAVY, IT CAN CAUSE DAMAGE TO
THE ELEVATORS.
(1) Do a check of the elevator output torque tube:
(a) Set the FLT CONTROL A switch on the forward overhead panel, P5, to the OFF position.
(b) Make sure the FLT CONTROL B switch on the forward overhead panel, P5, is in the ON
position.
(c) Put a piece of tape over the right elevator index plate [1].
(d) Use a block, STD-1278 and force gauge, COM-1557 to apply a force of 15 +/- 1 pounds (67
+/- 4 newtons) to the right elevator trailing edge in the down direction and release slowly.
NOTE: Apply the force approximately 0.5 inch (13 millimeters) forward of the trailing
edge and 1 inch (25 millimeters) outboard of the inboard edge of the elevator (next
to the tailcone).
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Page 602
Oct 10/2007
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BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
1) Make a mark of the right elevator position on the tape after you remove the force.
NOTE: Mark the position of the elevator after the force is removed from the elevator.
(e) Use a block, STD-1278 and force gauge, COM-1557 to apply a force of 10 +/- 1 pounds (45
+/- 4 newtons) to right elevator trailing edge in the up direction.
NOTE: Apply the force approximately 0.5 inch (13 millimeters) forward of the trailing
edge and 1 inch (25 millimeters) outboard of the inboard edge of the elevator (next
to the tailcone).
1) Make a mark of the right elevator position on the tape before you remove the force.
2) Slowly remove the force.
(f) Make sure the distance between the up and down position of the right elevator is not
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737-600-700-800-900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册3(47)
