Atec ATEC 212 SOLO ROTAX 912 UL manual Introduction, Personal data of the owner

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1.1.Introduction

The information provided by this manual is necessary for an effective and save operation of the ATEC 212 SOLO aircraft. Also included are information and documents of importance from the manufacturer.

1.2.Personal data of the owner

Owner of aircraft:

Address:

Telephone No:

Date from to:

Owner of aircraft:

Address:

Telephone No:

Date from to:

Owner of aircraft:

Address:

Telephone No:

Date from to:

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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 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 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 wings AssemblyDismantling the Horizontal and Vertical Rudder Page Fuselage WingTail Surfaces Landing GearSense of Motion of the Control Elements Fuel SystemInstrument Equipment Page Page Flap Control Safety BeltsCanopy Open / Close Flight Control InstrumentsAeroplane Repairs Cleaning and CareMajor Overhaul Anchorage of the AeroplanePage Operation over this range is prohibited Empty WeightMaximum take-off weight Centre of gravity determination Useful weight, weight table