Atec ATEC 212 SOLO ROTAX 912 UL manual Centre of Gravity CG

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2.4. Centre of Gravity ( CG )
CG of the empty aeroplane …………………	% MAC
Flight range of CG …………………………	28 – 36% MAC

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Contents Atec 212 Solo Type of aeroplane Atec 212 SoloPage Page Personal data of the owner IntroductionDescription of the Aeroplane Specification DimensionsRescue System installed / not installed……… WeightsOperational Temperature PowerOil Temperature Temperature of Engine CylindersThree-View Sketch Page Do not exceed this speed by flaps deflected Never exceed the maximum take-off weight of the aeroplaneAir Speeds Do not exceed this speed in any caseCentre of Gravity CG Manoeuvre and Gust Envelope Fuel Permitted ManoeuvresType of operation Other limits WindPage Rescue system deployment Power-off flightVibrations Emergency landingAborted landing Page Pre-Flight Inspection Procedures Before Entering the CockpitTake Off and Climb Away Warming up the EngineTaxiing Pre Take-OffDescent and landing Cruising flightPage Cruising Speeds Stalling Speeds CASTake off Distance at 15 m / 50 feet height Rate of ClimbPage Dismantling the wings AssemblyDismantling the Horizontal and Vertical Rudder Page Landing Gear WingFuselage Tail SurfacesSense of Motion of the Control Elements Fuel SystemInstrument Equipment Page Page Flight Control Instruments Safety BeltsFlap Control Canopy Open / CloseAnchorage of the Aeroplane Cleaning and CareAeroplane Repairs Major OverhaulPage Operation over this range is prohibited Empty WeightMaximum take-off weight Centre of gravity determination Useful weight, weight table