Atec ATEC 212 SOLO ROTAX 912 UL guide

Chapter 8

8.Care and Maintenance

8.1.Maintenance Schedule

8.2.Aeroplane Repairs

8.3.Major Overhaul

8.4.Anchorage of the Aeroplane

8.5.Cleaning and Care

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Contents

Atec 212 Solo Type of aeroplane Atec 212 SoloPage Page Personal data of the owner Introduction Rescue System installed / not installed……… Specification DimensionsWeights Description of the Aeroplane Oil Temperature PowerTemperature of Engine Cylinders Operational Temperature Three-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 deflected Centre of Gravity CG Manoeuvre and Gust Envelope Fuel Permitted ManoeuvresType of operation Other limits WindPage Rescue system deployment Power-off flight Vibrations Emergency landingAborted landing Page Pre-Flight Inspection Procedures Before Entering the Cockpit Taxiing Warming up the EnginePre Take-Off Take Off and Climb Away Descent 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 Gear Sense of Motion of the Control Elements Fuel SystemInstrument Equipment Page Page Flap Control Safety BeltsCanopy Open / Close Flight Control Instruments Aeroplane 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

Atec ATEC 212 SOLO ROTAX 912 UL manual