Atec ATEC 212 SOLO ROTAX 912 UL manual

Models: ATEC 212 SOLO ROTAX 912 UL

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Chapter 9

9.Weight, Centre of Gravity

9.1.Introduction

9.2.Empty Weight

9.3.Maximum Take-Off Weight

9.4.CG Range

9.5.CG Determination

9.6.Useful Load, Weight Table

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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 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 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 Assembly Dismantling the Horizontal and Vertical RudderDismantling the wings Page Fuselage WingTail Surfaces Landing GearFuel System Instrument EquipmentSense 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 Empty Weight Maximum take-off weightOperation over this range is prohibited Centre of gravity determination Useful weight, weight table