Atec ATEC 212 SOLO ROTAX 912 UL manual

Models: ATEC 212 SOLO ROTAX 912 UL

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Chapter 5

5.Performances

5.1.Introduction

5.2.Stalling Speeds

5.3.Take off Distance at 15 m / 50 ft Height

5.4.Rate of Climb

5.5.Cruising Speeds

5.6.Range of Flight

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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 Type of operation Permitted ManoeuvresFuel Wind Other limitsPage Power-off flight Rescue system deploymentAborted landing Emergency landingVibrations 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 Horizontal and Vertical Rudder AssemblyDismantling the wings Page Tail Surfaces WingFuselage Landing GearInstrument Equipment Fuel SystemSense of Motion of the Control Elements Page Page Canopy Open / Close Safety BeltsFlap Control Flight Control InstrumentsMajor Overhaul Cleaning and CareAeroplane Repairs Anchorage of the AeroplanePage Maximum take-off weight Empty WeightOperation over this range is prohibited Useful weight, weight table Centre of gravity determination