S 015-008
(5)
Remove access panel 3802 on the tail cone (AMM 12-31-41/201, Access Doors and Panels).
S 825-009
(6)
Set the horizontal stabilizer at 3 units of trim equal to the jackscrew "B" dimension of 41.57 +/- 0.05 inches (AMM 27-41-00/501, Horizontal Stabilizer Trim Control System).
NOTE: One person must be in the tail with a headset and the other
____
person in the control cabin.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
22-11-31
ALL ú ú 02 Page 502 ú Jul 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
(7) S 485-010Connect the power cable between the test set and the power outlet on the (D152) electronic equipment rack or an equivalent power outlet.
(8) S 485-001Connect the VTVM to the NSS FEEDBACK J7A and J8A on the test set.
(9) S 035-014Disconnect the sensor connectors D2205 (A system) or D2207 (B system).
S 485-004
(10)
Connect the -4 test cable (-111 cable on airplanes with a single A stablilizer position sensor) between the A system sensor and J-3 (A SENSOR) on the test set.
S 485-005
(11)
Connect the -111 test cable between the B system sensor and J-4 (B SENSOR).
S 865-015
(12)
Set the switches on the test set as follows:
(a)
LVDT FEEDBACK switches A to the ON position and B to the OFF position
(b)
LVDT EXCITATION switches A to the ON position and B to the OFF position
(c)
NSS EXCITATION switches A to the ON position and B to the OFF position.
(d)
NSS FEEDBACK switches A and B to the OFF position
(e)
All SOLENOID EXCITATION PISTON and ENGAGE switches to the OFF position
(f)
CURRENT SELECT switch to A T-VALVE
(g)
SOLENOID switches to the A NORM, OFF, and B NORM positions
(h)
ACTUATOR SELECT switch to A ONLY
(i)
POWER switch to the ON position.
NOTE: The power and NSS EXCITATION lights will be on.
____
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
22-11-31
ALL ú ú 01 Page 503 ú Nov 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
S 865-016
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 OR DAMAGE TO EQUIPMENT.
(13)
Put hydraulic system A and B switches to the ON position
(AMM 29-15-00/201, Hydraulic Systems).
S 865-017
(14)
Close the FLT CONT SYS circuit breaker on the P6 circuit breaker panel.
E. Sensor Adjustment
S 865-014
(1)
Quickly move the control column and make sure the right elevator trailing edge is in line with the tail cone index |0.06 inch.
S 035-022
(2)
Loosen the screw on the sensor clamp until the sensor can be turned.
S 825-023
(3)
Turn the A sensor housing slowly until you get a value less than
0.5 volts.
S 435-006
(4)
Tighten the clamp screw 8 to 12 pound-inches.
S 485-024
(5)
Remove the lockwire and turn the thumbnut on the microadjustment rod until you get the smallest voltage possible (less than 70mV).
S 825-007
(6)
Do steps 1-5 again, with the VTVM connected to J7B and J8B on the test set, to adjust the B system sensor.
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機(jī)維護(hù)手冊(cè) 自動(dòng)飛行 AUTOFLIGHT 2(32)
