Atec ATEC 212 SOLO ROTAX 912 UL manual Atec 212 Solo

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Sole Manufacturer and Distributor in the Czech Republic:

ATEC v.o.s.

Location of factory: ATEC v.o.s., Opolanská 350, 289 07 Libice nad Cidlinou

Czech Republic

ATEC 212 SOLO

Libice nad Cidlinou January 2007

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Contents Atec 212 Solo Type of aeroplane Atec 212 SoloPage Page Personal data of the owner IntroductionRescue System installed / not installed……… Specification DimensionsWeights Description of the AeroplaneOil Temperature PowerTemperature of Engine Cylinders Operational TemperatureThree-View Sketch Page Air Speeds Never exceed the maximum take-off weight of the aeroplaneDo not exceed this speed in any case Do not exceed this speed by flaps deflectedCentre of Gravity CG Manoeuvre and Gust Envelope Type of operation Permitted ManoeuvresFuel Other limits WindPage Rescue system deployment Power-off flightAborted landing Emergency landingVibrations Page Pre-Flight Inspection Procedures Before Entering the CockpitTaxiing Warming up the EnginePre Take-Off Take Off and Climb AwayDescent and landing Cruising flightPage Take off Distance at 15 m / 50 feet height Stalling Speeds CASRate of Climb Cruising SpeedsPage Dismantling the Horizontal and Vertical Rudder AssemblyDismantling the wings Page Fuselage WingTail Surfaces Landing GearInstrument Equipment Fuel SystemSense of Motion of the Control Elements Page Page Flap Control Safety BeltsCanopy Open / Close Flight Control InstrumentsAeroplane Repairs Cleaning and CareMajor Overhaul Anchorage of the AeroplanePage Maximum take-off weight Empty WeightOperation over this range is prohibited Centre of gravity determination Useful weight, weight table