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塞斯纳172飞行员操作手册 Cessna 172 PILOT'S OPERATING HANDBOOK(68)

时间:2011-12-29 11:03来源:蓝天飞行翻译 作者:航空 点击:

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Figure 7-2. Instrument Panel (Sheet 1 of 2) Figure 7-2. Instrument Panel (Sheet 2 of 2)
 
The horizontal stabilizer is constructed of a forward and aft spar, ribs and stiffeners, center, left, and right wrap-around skin panels, and formed leading edge skins. The horizontal stabilizer also contains the elevator trim tab actuator. Construction of the elevator consists of formed leading edge skins, a forward spar, aft channel, ribs, torque tube and bellcrank, left upper and lower "V" type corrugated skins, and right upper and lower "V" type corrugated skins incorporating a trailing edge cut-out for the trim tab. The elevator trim tab consists of a spar, rib, and upper and lower "V" type corrugated skins. The leading edge of both left and right elevator tips incorporate extensions which contain balance weights.
FLIGHT CONTROLS
The airplane's flight control system (see figure 7-1) consists of conventional aileron, rudder, and elevator control surfaces. The control surfaces are manually operated through mechanical linkage using a control wheel for the ailerons and elevator, and rudder/ brake pedals for the rudder.
 
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