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1) Make sure the difference is between 0.60 and 0.90 inches (15.2 - 22.9 mm).
(as) Do this task: Retract the Trailing Edge Flaps, TASK 27-51-00-860-804.
H. Put the Airplane Back to Its Usual Condition
SUBTASK 27-31-00-860-070
(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 27-31-00-410-012
(2) Close this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
------------------------- END OF TASK ---------------------------
TASK 27-31-00-700-807
17. Manual Mode - Test
(Figure 502)
A. General
(1) Use this test to make sure the control columns and control wheels operate freely.
B. References
Reference Title
27-31-00-800-802 Remove Pressure from the Elevator Hydraulic Systems A and B
(P/B 201)
27-31-00-840-802 Put the Elevator Systems A and B Back to the Condition Before the
Pressure Removal (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)
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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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
F. Prepare for the Test
SUBTASK 27-31-00-860-071
(1) Do this task: Remove Pressure from the Elevator Hydraulic Systems A and B,
TASK 27-31-00-800-802.
SUBTASK 27-31-00-040-001
(2) Do the following to isolate the spoilers to keep them from moving when you turn the control
wheel:
(a) Turn the A and B Spoiler Shutoff Switches on the P5-3 panel to the OFF position.
SUBTASK 27-31-00-010-014
(3) Open this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
SUBTASK 27-31-00-860-073
(4) Use the bar, SPL-1677 to set the "B" dimension at 4 units of trim (39.89 +/- 0.01 inches or 1013.2
+/- 0.3 mm) (Figure 502).
G. Manual Mode Test
SUBTASK 27-31-00-730-006
(1) Do the manual mode test:
(a) Make sure the control columns and control wheels move freely:
1) Move the control column in a longitudinal direction (forward and aft), and while moving
the control column forward and aft, rotate the control wheel between the left and right
stops.
a) Repeat this step nine more times.
2) Rotate and hold the control wheel against the left stop and move the control column in a
longitudinal direction (forward and aft) between the stops.
3) Rotate and hold the control wheel against the right stop and move the control column in
a longitudinal direction (forward and aft) between the stops.
4) Hold the control column full forward and rotate the control wheel left and right between
the stops.
5) Hold the control column full aft and rotate the control wheel left and right between the
stops.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-00
Page 575
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
H. Put the Airplane Back to Its Usual Condition
SUBTASK 27-31-00-860-074
(1) Do this task: Put the Elevator Systems A and B Back to the Condition Before the Pressure
Removal, TASK 27-31-00-840-802.
SUBTASK 27-31-00-040-002
(2) If necessary, turn the A and B Spoiler Shutoff Switches on the P5-3 panel to the ON position.
SUBTASK 27-31-00-410-013
(3) Close this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
------------------------- END OF TASK ---------------------------
TASK 27-31-00-700-808
18. Control Column Travel and Centering - Test
(Figure 502, Figure 505, Figure 514, Figure 523)
A. General
(1) Use this test to make sure the control columns can move through their full travel. This also
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737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册2(156)
