S 865-135
(7)
If you will do no more tests, then do this task:
"Put the Airplane to its Usual Condition."
TASK 31-24-02-735-474
10. Control Wheel Position Signals Test___________________________________
A. Special Tools and Equipment
(1) Universal Protractor 11MIT5-74110-51
B. Reference
(1) AMM 27-11-00/201, Aileron and Aileron Trim Control System
C. Access
(1) Location Zones
101 Control Cabin - Left
102 Control Cabin - Right
D. Procedure
S 865-715
(1)
Make sure you did the Prepare For Input Parameter Test task.
S 735-716
(2)
Do this test of the position signals from the control wheel:
(a)
Attach the universal protractor 11MIT5-74110-51 to the control wheel.
(b)
Set the portable tester to SUBFRAME 0, WORD 28.
(c)
Move the control wheel to the zero degree position.
(d)
Install a rig pin in the captain's control wheel.
(e)
Make sure the portable tester display is 7771 to 0007 (nominal 0000).
(f)
Remove the rig pin from the captain's control wheel.
(g)
Turn the control wheel to the positions shown in the table.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
BEJ 101-112, 114-999; ú 31-24-02
ú ú 14 Page 519 ú Mar 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
(h) Make sure the portable tester display agrees with the values in the table.
~...................................................... | CONTROL WHEEL POSITION | PORTABLE TESTER READOUT | ........................................................ | 50° CW | 1172 to 1256 (nominal 1224) | | 50° CCW | 6522 to 6606 (nominal 6554) | 2........................….............................1
S 865-460
(3)
Remove the universal protractor from the control wheel.
S 865-717
(4)
If you will do no more tests, then do this task:
"Put the Airplane to its Usual Condition."
TASK 31-24-02-735-121
11. Elevator Position Signals Test______________________________
A. References
(1)
AMM 27-31-00/201, Elevator and Tab Control
(2)
AMM 27-31-00/501, Elevator and Tab Control
(3)
AMM 29-00-00/201, Hydraulic Power
(4)
AMM 31-24-51/401, Elevator Position Sensor
B. Access
(1) Location Zones
101 Control Cabin - Left
102 Control Cabin - Right
C. Procedure
S 865-702
(1) Make sure you did the Prepare For Input Parameter Test task.
S 865-123
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
_______ SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. AILERONS, RUDDERS, ELEVATORS, FLAPS, SPOILERS, LANDING GEAR, AND THRUST REVERSERS CAN MOVE QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(2) Supply power to the elevator system (AMM 27-31-00/201).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
BEJ 101-112, 114-999; ú 31-24-02
ú ú 11 Page 520 ú Mar 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
(3) S 865-703Set the B dimension on the stabilizer jackscrew to 41.57 |0.05 inches (AMM 27-31-00/501).
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