曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
that are replaced or non-procurable are preceded by "Opt:", which stands for Optional.
Reference Description
SPL-1748 Adapter - Torque Wrench, Manual, Stabilizer Trim Wheel
(Part #: C27064-1, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)
C. 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
D. Prepare for the Test
SUBTASK 27-41-00-860-002
(1) Set the main cutout switch, S272 on the control stand to the CUTOUT position.
SUBTASK 27-41-00-480-001
(2) Install the adapter, SPL-1748 on the captain’s control trim wheel.
E. Procedure
SUBTASK 27-41-00-710-003
WARNING: MAKE SURE THAT ALL PERSONS AND EQUIPMENT ARE CLEAR OF THE
HORIZONTAL STABILIZERS. THE HORIZONTAL STABILIZER WILL MOVE WHEN YOU
TURN THE CONTROL TRIM WHEELS. THIS CAN CAUSE INJURIES TO PERSONS AND
DAMAGE TO EQUIPMENT.
(1) Do the friction test of the horizontal stabilizer trim control:
(a) Turn the captain’s control trim wheel counterclockwise (full APL NOSE DOWN) until it
touches the stops.
(b) Turn the captain’s control trim wheel clockwise (full APL NOSE UP) until it touches the
stops.
1) Make sure the force necessary to operate the control trim wheel is not more than 62 inlb
(7.0 Nm) or not less than 22 in-lb (2.5 Nm).
2) Make sure the system operates smoothly.
(c) Turn the control trim wheel counterclockwise (full APL NOSE DOWN) until it touches the
stops.
1) Make sure the force necessary to operate the control trim wheel is not more than 62 inlb
(7.0 Nm) or not less than 22 in-lb (2.5 Nm).
2) Make sure the system operates smoothly.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-41-00
Page 521
Oct 10/2006
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
SUBTASK 27-41-00-080-001
(2) Remove the adapter, SPL-1748 from the captain’s control trim wheel.
------------------------- END OF TASK ---------------------------
TASK 27-41-00-700-803
5. Stabilizer Electric Trim System Test
A. General
(1) Use this test to make sure the horizontal stabilizer moves at the correct speed when it is
operated from the STAB TRIM switches.
B. References
Reference Title
24-22-00-860-811 Supply Electrical Power (P/B 201)
C. 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
D. Prepare for the Test
SUBTASK 27-41-00-860-003
(1) Do this task: Supply Electrical Power, TASK 24-22-00-860-811.
SUBTASK 27-41-00-860-004
(2) Make sure that these circuit breakers are closed:
CAPT Electrical System Panel, P18-1
Row Col Number Name
C 2 C00849 AFCS STABILIZER TRIM
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
SUBTASK 27-41-00-860-005
(3) Make sure that the main cutout switch, S272, on the P8 panel, is in the NORMAL position.
SUBTASK 27-41-00-860-006
(4) Make sure that the STAB TRIM switch on the stab trim and cabin door panel, P8-47 is in the
NORMAL position.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-41-00
Page 522
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
E. Procedure
SUBTASK 27-41-00-710-004
WARNING: MAKE SURE THAT ALL PERSONS AND EQUIPMENT ARE CLEAR OF THE
HORIZONTAL STABILIZERS. THE HORIZONTAL STABILIZERS WILL MOVE WHEN YOU
MOVE THE CONTROL WHEELS. THIS CAN CAUSE INJURIES TO PERSONS AND
DAMAGE TO EQUIPMENT.
(1) Do the test of the electrical trim system test:
(a) Set the flaps to any position from 1-40 units.
1) Push and hold the STAB TRIM switches on the captain’s control wheel to the NOSE
DOWN position.
a) Make sure the stabilizer leading edge moves up.
b) Release the STAB TRIM switches.
2) Push and hold the STAB TRIM switches on the captain’s control wheel to the NOSE UP
position.
a) Make sure the stabilizer leading edge moves down.
b) Release the STAB TRIM switches.
3) Push and hold the STAB TRIM switches on the first officer’s control wheel to the NOSE
DOWN position.
a) Make sure the stabilizer leading edge moves up.
b) Release the STAB TRIM switches.
4) Push and hold the STAB TRIM switches on the first officer’s control wheel to the NOSE
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737-600-700-800-900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册3(112)
