Atec ATEC 212 SOLO ROTAX 912 UL manual

Models: ATEC 212 SOLO ROTAX 912 UL

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Chapter 7

7.Description of the Aeroplane and Its Systems

7.1.Wing

7.2.Fuselage

7.3.Tail Surfaces

7.4.The Landing Gear

7.5.Control

7.6.The Driving Unit

7.7.Fuel System

7.8.Instrument Equipment

7.9.The Sense of Motion of the Control Elements

Image 26

Contents

Atec 212 Solo Atec 212 Solo Type of aeroplanePage Page Introduction Personal data of the ownerWeights Specification DimensionsRescue System installed / not installed……… Description of the AeroplaneTemperature of Engine Cylinders PowerOil Temperature Operational TemperatureThree-View Sketch Page Do not exceed this speed in any case Never exceed the maximum take-off weight of the aeroplaneAir Speeds Do not exceed this speed by flaps deflectedCentre of Gravity CG Manoeuvre and Gust Envelope Fuel Permitted ManoeuvresType of operation Wind Other limitsPage Power-off flight Rescue system deploymentVibrations Emergency landingAborted landing Page Procedures Before Entering the Cockpit Pre-Flight InspectionPre Take-Off Warming up the EngineTaxiing Take Off and Climb AwayCruising flight Descent and landingPage Rate of Climb Stalling Speeds CASTake off Distance at 15 m / 50 feet height Cruising SpeedsPage Dismantling the wings AssemblyDismantling the Horizontal and Vertical Rudder Page Tail Surfaces WingFuselage Landing GearSense of Motion of the Control Elements Fuel SystemInstrument Equipment Page Page Canopy Open / Close Safety BeltsFlap Control Flight Control InstrumentsMajor Overhaul Cleaning and CareAeroplane Repairs Anchorage of the AeroplanePage Operation over this range is prohibited Empty WeightMaximum take-off weight Useful weight, weight table Centre of gravity determination