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(e) Make marks of the right elevator positions on the masking tape (from the two tables below).
(f) Move the captain’s control column slowly aft with the force gauge, COM-1557.
1) Hold the captain’s control column at these elevator positions (that have been marked
on the masking tape of the right elevator) and make sure the forces to move the control
column are in these limits:
NOTE: Put a straight edge on the top of the trailing edge surface of the elevator
surface to measure the elevator position at the surface of the tailcone.
NOTE: The "breakout" is when the elevator starts to move.
Table 502/27-31-00-993-825
RIGHT ELEVATOR POSITION (T.E. UP) REQUIRED COLUMN FORCE (AFT)
BREAKOUT 3.0 - 7.0 pounds (13.3 - 31.1 newtons)
1.90 - 2.00 inches (48.3 - 50.8 mm) 14.5 - 21.5 pounds (64.5 - 95.6 newtons)
5.05 - 5.15 inches (128.3 - 130.8 mm) 21.0 - 27.0 pounds (93.4 - 120.1 newtons)
9.40 - 9.50 inches (238.8 - 241.3 mm) 29.5 - 36.5 pounds (131.2 - 162.4 newtons)
(g) Move the captain’s control column slowly forward with the force gauge, COM-1557.
1) Hold the captain’s control column at these elevator positions and make sure the forces
to move the control column are in these limits:
NOTE: The "breakout" is when the elevator starts to move.
Table 503/27-31-00-993-826
RIGHT ELEVATOR POSITION
(T.E. DOWN)
REQUIRED COLUMN FORCE
(FORWARD)
BREAKOUT 3.5 - 7.5 pounds (15.6 - 33.4 newtons)
1.90 - 2.00 inches (48.3 - 50.8 mm) 17.5 - 21.5 pounds (77.8 - 95.6 newtons)
5.05 - 5.15 inches (128.3 - 130.8 mm) 28.5 - 35.5 pounds (126.8 - 157.9 newtons)
9.40 - 9.50 inches (238.8 - 241.3 mm) 34.8 - 42.8 pounds (154.7 - 190.4 newtons)
H. Put the Airplane Back to Its Usual Condition
SUBTASK 27-31-00-080-006
(1) Remove the adapter, SPL-1674 and control column assembly protractor, SPL-1680 from the
captain’s control column.
SUBTASK 27-31-00-860-082
(2) Do this task: Put the Elevator Hydraulic systems A and B Back to the Condition Before the
Pressurization, TASK 27-31-00-840-801.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-00
Page 583
Oct 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
SUBTASK 27-31-00-410-015
(3) Close this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
------------------------- END OF TASK ---------------------------
TASK 27-31-00-700-810
20. Neutral Shift - Test
(Figure 502, Figure 505, Figure 523)
A. General
(1) Use this test to make sure the elevator neutral shift mechanism moves the elevator when the
stabilizer moves. When the stabilizer moves, it gives a mechanical input to the elevator PCUs.
B. References
Reference Title
24-22-00-860-811 Supply Electrical Power (P/B 201)
27-31-00-700-801 Null Procedure - Mach Trim Actuator (P/B 201)
27-31-00-800-801 Elevator Hydraulic System A and B - Pressurization (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)
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
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)
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
E. Access Panels
Number Name/Location
311BL Stabilizer Trim Access Door

　
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