|
To view this page ensure that Adobe Flash Player version 9.0.124 or greater is installed. Exhaust System 7-19 Carburetor And Priming System 7-19 Cooling System 7-20 Propeller 7-20 Fuel System 7-20 Brake System 7-23 Electrical System 7-23 Master Switch 7-25 Avionics Power Switch 7-25 7-1 TABLE OF CONTENTS (Continued) Page Ammeter 7-26 Over-Voltage Sensor And Warning Light 7-26 Circuit Breakers And Fuses 7-26 Ground Service Plug Receptacle 7-27 Lighting Systems 7-27 Exterior Lighting 7-27 Interior Lighting 7-28 Cabin Heating, Ventilating And Defrosting System 7-29 Pitot-Static System And Instruments 7-31 Airspeed Indicator 7-32 Rate-Of-Climb Indicator 7-32 Altimeter 7-32 Vacuum System Arid Instruments 7-32 Attitude Indicator 7-34 Directional Indicator 7-34 Suction Gage 7-34 Stall Warning System 7-34 Avionics Support Equipment 7-35 Audio Control Panel 7-35 Transmitter Selector Switch 7-35 Automatic Audio Selector Switch 7-35 Audio Selector Switches 7-37 Microphone - Headset 7-37 Static Dischargers 7-38 INTRODUCTION This section provides description and operation of the airplane and its systems. Some equipment described herein is optional and may not be installed in the airplane. Refer to Section 9, Supplements, for details of other optional systems and equipment. AIRFRAME The airplane is an all-metal, four-place, high-wing, single-engine airplane equipped with tricycle landing gear, and is designed for general utility purposes. 中国通航网 www.ga.cn 通航翻译 www.aviation.cn 本文链接地址：塞斯纳172飞行员操作手册 Cessna 172 PILOT'S OPERATING HANDBOOK(65) |
