(a)
Limit Switch and Position Transmitter Module and Travel Limit Mechanism 1) The limit switch and position transmitter modules are
adjusted correctly if: a) The tensions in cables SL and SP are 50 | 5 lbs (222 +/- 22 newtons).
b) AIRPLANES WITH STAB TRIM LEVERS ON THE CONTROL STAND; rig pins E/ST1, E/ST3, E/ST4, and E/ST5 can be put in freely when Dimension B on the stabilizer ballscrew actuator is 19.07 |0.01 inches
(484.4 +/- 0.25 mm).
c) AIRPLANES WITH ALTERNATE STAB TRIM SWITCHES ON THE CONTROL STAND; rig pins E/ST3, E/ST4, and E/ST5 can be put in freely when Dimension B on the stabilizer ballscrew actuator is 19.07 |0.01 inches (484.4 +/- 0.25 mm).
2) AIRPLANES WITH STAB TRIM LEVERS ON THE CONTROL STAND; the travel limit mechanism is correctly adjusted if the condition that follows is correct: a) Cables SLA and SLB are adjusted such that the stop lugs
on the lower end of ballnuts are between 0.16 to 0.60 of a turn away from the stop lugs on the upper flange of the gearbox.
(2) For correct adjustment of the stabilizer trim indicating system, Dimension B on the stabilizer trim ballscrew actuator must be set to
19.07 | 0.01 inches (484.4 +/- 0.25 mm) (stabilizer is at 0 degree position) (Fig. 502).
B. Equipment
(1)
Gage Assembly - B27039-2 (Part of Elevator and Stabilizer Rigging Equipment, B27039-1)
(2)
Rig Pins from Set B20003-XX (AMM 20-10-24/201):
(a)
E/ST1 - P/N B20003-21
(b)
E/ST3 - P/N B20003-21
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D.
E.
F.
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757
MAINTENANCE MANUAL
(c)
E/ST4 - P/N B20003-21
(d)
E/ST5 - P/N B20003-21Consumable Materials
(1)
C00308 Compound - Corrosion Preventive MIL-C-11796References
(1)
AMM 06-42-00/201, Empennage Access Doors and Panels
(2)
AMM 20-10-24/201, Rig Pins
(3)
AMM 24-22-00/201, Electrical Power - Control
(4)
AMM 29-11-00/201, Main (Left, Right, Center) Hydraulic SystemsAccess
(1)
Location Zone 311 Area Aft of the Pressure Bulkhead to BS 1787.45 (Left)
(2)
Access Panel 311AL Forward Stabilizer Compartment Access Door
Prepare for Adjustment
S 865-041
(1) Supply electrical power (AMM 24-22-00/201).
S 865-042
WARNING: KEEP PERSONS AND EQUIPMENT AWAY FROM ALL CONTROL SURFACES
_______ WHEN HYDRAULIC POWER IS SUPPLIED. AILERONS, ELEVATORS, RUDDER, FLAPS, SLATS, SPOILERS, AND STABILIZER ARE FULLY POWERED SURFACES. INJURY TO PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR WHEN HYDRAULIC POWER IS SUPPLIED.
(2)
Pressurize the right and center hydraulic systems (AMM 29-11-00/201).
S 865-043
(3)
Move the horizontal stabilizer such that Dimension B on the stabilizer trim ballscrew actuator is 19.07 | 0.01 inches
(484.4 +/- 0.25 mm).
S 865-044
(4)
Remove the power from the right and center hydraulic systems (Ref 29-11-00).
S 865-045
(5)
Put the RIGHT and CENTER STAB TRIM SHUTOFF valve switches on the control stand panel, P10, to CUTOUT.
S 865-046
(6)
Open these circuit breakers on the overhead panel, P11, and attach DO-NOT-CLOSE tags:
(a)
11B19, STAB TRIM ALT (IF INSTALLED)
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757 MAINTENANCE MANUAL 中國航空網 m.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：757 AMM 飛機維護手冊 飛行操縱 FLIGHT CONTROLS 4(94)
