Atec ATEC 212 SOLO ROTAX 912 UL manual

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Chapter 3

3.Emergency Instructions

3.1.Engine Failure Taking-Off

3.2.Engine Failure in Flight

3.3.Rescue System Application

3.4.Fire in Flight

3.5.Power-Off Flight

3.6.Emergency Landing

3.7.Safety Landing

3.8.Aborted landing

3.9.Vibration

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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 Permitted Manoeuvres Type of operationFuel Other limits WindPage Rescue system deployment Power-off flightEmergency landing Aborted landingVibrations 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 Assembly Dismantling the Horizontal and Vertical RudderDismantling the wings Page Landing Gear WingFuselage Tail SurfacesFuel System Instrument EquipmentSense of Motion of the Control Elements Page Page Flight Control Instruments Safety BeltsFlap Control Canopy Open / CloseAnchorage of the Aeroplane Cleaning and CareAeroplane Repairs Major OverhaulPage Empty Weight Maximum take-off weightOperation over this range is prohibited Centre of gravity determination Useful weight, weight table