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TO THE BALLSCREW ACTUATOR ASSEMBLY MAY OCCUR.
(b) Apply a 500 ±20 in-lb (56.5 ±2.3 Nm) clockwise torque to the upstop of the jackscrew and
hold.
NOTE: Make sure you do not put the torque on the safety rod nut.
1) While maintaining torque on the jackscrew, use a marker to make a line on the
jackscrew shield and the retainer - seal.
2) Release the torque.
(c) Measure the arc distance between the lines.
1) Make sure that the arc distance dimension is not more than 1.06 in. (26.9 mm) (36.0
degrees).
F. Put the Airplane Back to Its Usual Condition
SUBTASK 27-41-00-410-005
(1) Close this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
737-600/700/800/900
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SUBTASK 27-41-00-860-019
(2) Remove the safety tags and close these circuit breakers:
F/O Electrical System Panel, P6-2
Row Col Number Name
B 10 C00207 FLIGHT CONTROL STAB TRIM CONT
D 10 C00840 FLIGHT CONTROL STAB TRIM ACTUATOR
------------------------- END OF TASK ---------------------------
737-600/700/800/900
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Stabilizer Trim Secondary Brake System Test
Figure 505 (Sheet 1 of 3)/27-41-00-990-805
737-600/700/800/900
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Stabilizer Trim Secondary Brake System Test
Figure 505 (Sheet 2 of 3)/27-41-00-990-805
737-600/700/800/900
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Stabilizer Trim Secondary Brake System Test
Figure 505 (Sheet 3 of 3)/27-41-00-990-805
737-600/700/800/900
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TASK 27-41-00-700-809
11. Stabilizer Trim Cutout Test
A. General
(1) Use this procedure to make sure the stabilizer trim cutout switch operates correctly. It stops the
horizontal stabilizer when the control column command is opposite from the STAB TRIM
switches.
B. References
Reference Title
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-1680 Protractor - Assembly, Control Column
(Part #: 4MIT65B80307-1, Supplier: 81205, A/P Effectivity: 737-100,
-200, -200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800,
-900, -900ER, -BBJ)
(Part #: A27021-29, 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
330 Subzone - Left Horizontal Stabilizer and Elevator
340 Subzone - Right Horizontal Stabilizer and Elevator
E. Prepare for the Test
SUBTASK 27-41-00-860-020
(1) Do this task: Elevator Hydraulic System A and B - Pressurization, TASK 27-31-00-800-801.
SUBTASK 27-41-00-860-021
(2) Make sure that these circuit breakers are closed:
F/O Electrical System Panel, P6-2
Row Col Number Name
B 10 C00207 FLIGHT CONTROL STAB TRIM CONT
D 10 C00840 FLIGHT CONTROL STAB TRIM ACTUATOR
737-600/700/800/900
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F. Procedure
SUBTASK 27-41-00-710-012
WARNING: MAKE SURE THAT THE STABILIZER TRIM MOTOR HAS A MINIMUM 13 MINUTES OFF
FOR EVERY 2 MINUTES OPERATION. IF YOU DO NOT GIVE THE STABILIZER TRIM
MOTOR SUFFICIENT TIME OFF, DAMAGE TO THE STABILIZER TRIM MOTOR CAN
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737-600-700-800-900 AIRCRAFT MAINTENANCE MANUAL飛機維護手冊3(119)
