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+/- 0.3 millimeter) by doing the "Check" steps in this procedure: Elevator Balance Panel -
Installation, TASK 27-31-41-400-801.
SUBTASK 27-31-00-200-007
(2) Move each elevator (left and right side) by hand through the full travel to make sure that the
elevator moves smoothly and freely.
(a) Visually verify that each of the bulb seals do not bind as the elevator moves through the full
travel.
SUBTASK 27-31-00-420-009
(3) Install the access panels that were removed for this procedure.
SUBTASK 27-31-00-700-004
(4) Do this task: Manual Mode - Test, TASK 27-31-00-700-807.
G. Put the Airplane Back to Its Usual Condition
SUBTASK 27-31-00-860-055
(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 27-31-00-410-025
(2) Close this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
------------------------- END OF TASK ---------------------------
TASK 27-31-00-700-804
14. Elevator Travel Limit - Test
(Figure 502, Figure 523)
A. General
(1) Use this test to make sure the elevator operates correctly through the full travel.
B. References
Reference Title
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)
27-31-00-800-802 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)
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(Continued)
Reference Title
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)
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 27-31-00-860-056
(1) Do this task: Remove Pressure from the Elevator Hydraulic Systems A and B,
TASK 27-31-00-800-802.
SUBTASK 27-31-00-860-057
(2) Do this task: Null Procedure - Mach Trim Actuator, TASK 27-31-00-700-801.
SUBTASK 27-31-00-010-011
(3) Open this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
SUBTASK 27-31-00-860-058
(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 millimeters) (Figure 502).
G. Elevator Travel Limit Test
SUBTASK 27-31-00-730-003
CAUTION: DO NOT PUT A LOAD OF MORE THAN 65 POUNDS (289 NEWTONS) ON THE
ELEVATORS AT ONE TIME. IF THE LOAD IS TOO HEAVY, IT CAN CAUSE DAMAGE TO
THE ELEVATORS.
(1) Do the elevator travel limit test with hydraulics off:
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(a) Check for binding at the left and right elevators:
1) Use your hand to move the right elevator through the full travel.
a) Make sure that there is no binding through the full travel.
2) Use your hand to move the left elevator through the full travel.
a) Make sure that there is no binding through the full travel.
(b) Move and hold the captain’s control column aft until it touches the stops.
1) Make sure the right elevator moves 13.16 - 14.87 inches (334.3 - 377.7 mm) up from the
index mark (Figure 523).
(c) Move and hold the captain’s control column forward until it touches the stops.
1) Make sure the right elevator moves 9.90 - 11.08 inches (251.5 - 281.4 mm) down from
the index mark.
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737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册2(150)
