22-11-01
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 745-090
(2)
Push the LSK adjacent to STABILIZER> from the Rigging Tests Index.
S 745-091
(3)
During this test, follow the instructions and push the LSK adjacent to <CONTINUE as shown on the CDU display.
S 745-092
(4)
Make sure that the values for the A and B sides are in the limits shown on the CDU or in this section.
Test 54.01 STAB POS (VAC) Limits: -0.07 to 0.07
Measure the stabilizer B dimension with the trammel bar or steel measurement tape (Fig. 503).
Test 54.02 STAB POS (VAC) Limits: -1.93 to -1.43
When the STAB is stable, measure the stabilizer B dimension with the trammel bar or steel measurement tape (Fig. 503). The limits must be between 45.39 and 45.75 inches.
Test 54.03 STAB POS (VAC) Limits: 6.30 to 7.60
When the STAB is stable, measure the stabilizer B dimension with the trammel bar or steel measurement tape (Fig. 503). The limits must be between 25.65 to 25.85 inches.
S 745-093
(5) Push the LSK adjacent to <CONTINUE to go back to the Rigging Tests Index.
I. Pitch Control Wheel Steering Rigging Test
S 865-032
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
_______ SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. AILERONS, RUDDER, ELEVATORS, FLAPS, SLATS, SPOILERS, LANDING GEAR, AND THRUST REVERSERS CAN MOVE QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
(1) Supply hydraulic power (AMM 29-15-00/201).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
SEE A
UPPER STOP
LOWER STOP
"B" ACTUATOR DIMENSION TRAMMEL BAR
1
FWD
A
1THE "B" DIMENSION IS MEASURED BETWEEN THE CENTER OF THE UPPER AND LOWER GIMBAL PINS
Stabilizer Trim "B" Dimension Location Figure 503
E84055
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
(2) S 745-099Push the LSK adjacent to <CWS from the Rigging Tests Index.
(3) S 745-173Push the LSK adjacent to <PITCH CWS.
(4) S 745-142During this test, follow the instructions and push the LSK adjacent to <CONTINUE as shown on the CDU display.
(5) S 745-177Make sure that the values for the A and B sides are in the limits shown on the CDU or in this section.
NOTE:____ Do not apply force to column for the Tests 55.01 thru 55.03.
Test 55.01 PCWS SENSORS RIGGING (VAC) Limits: -0.20 to 0.20
Test 55.02 PCWS SENSOR (VAC) Limits: -0.20 to 0.20
Test 55.03 PCWS SENSOR (VAC) Limits: -0.20 to 0.20
NOTE:____ Apply force at the center of the control wheel hub, perpendicular to the axis of the control column. Apply force to the NOM value as shown on the CDU display.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 自動飛行 AUTOFLIGHT 1(144)
