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greater than 0.210 inch (5.32 millimeters).
(g) Remove the tape.
(h) Set the FLT CONTROL A switch on the forward overhead panel, P5, to the ON position.
(i) Set the FLT CONTROL B switch on the forward overhead panel, P5, to the OFF position.
(j) Put a piece of tape over the left elevator index plate [1].
(k) Use a block, STD-1278 and force gauge, COM-1557 to apply a force of 15 +/- 1 pounds (67
+/- 4 newtons) to left 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).
1) Make a mark of the left 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.
(l) Use a block, STD-1278 and force gauge, COM-1557 to apply a force of 10 +/- 1 pounds (45
+/- 4 newtons) to left elevator trailing edge in the up direction.
NOTE: Apply the force approximately 0.5 inch (13 millimeters) forward of the elevator
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 left elevator position on the tape before you remove the force.
2) Slowly remove the force.
(m) Make sure the distance between the up and down position of the left elevator is not greater
than 0.210 inch (5.32 millimeters).
(n) Remove the tape.
(o) Set the FLT CONTROL B switch on the forward overhead panel, P5, to the ON position.
H. Put the Airplane Back to Its Usual Condition.
SUBTASK 27-31-32-860-024
(1) Do this task: Put the Elevator Hydraulic systems A and B Back to the Condition Before the
Pressurization, TASK 27-31-00-840-801.
SUBTASK 27-31-32-410-004
(2) Install this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-32
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D633A101-GUN
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Elevator Output Torque Tube Buss Linkage Freeplay Inspection
Figure 601 (Sheet 1 of 2)/27-31-32-990-804
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-32
Page 604
Feb 10/2006
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Elevator Output Torque Tube Buss Linkage Freeplay Inspection
Figure 601 (Sheet 2 of 2)/27-31-32-990-804
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-32
Page 605
Feb 10/2006
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
GUN 156, 201-204, 206 PRE SB 737-55A1080
TASK 27-31-32-200-801
3. Elevator Tab Freeplay - Check
(Figure 602)
A. General
(1) Use this test to do a check of the elevator tab trailing edge freeplay, the elevator tab hinge line
axial freeplay, and the elevator tab hinge line radial freeplay.
B. References
Reference Title
12-22-31-640-802 Elevator Tab Hinge Lubrication (P/B 301)
27-31-00-800-801 Elevator Hydraulic System A and B - Pressurization (P/B 201)
27-31-00-800-802 Remove Pressure from the Elevator Hydraulic Systems A and B
(P/B 201)
27-31-00-840-801 Put the Elevator Hydraulic systems A and B Back to the Condition
Before the Pressurization (P/B 201)
27-51-00-860-801 Trailing Edge Flap System Operation With Primary Control (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
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,
　
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