Atec ATEC 212 SOLO ROTAX 912 UL manual

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Chapter 4

4.Standard Procedures

4.1Pre-Flight Inspection

4.1.1Procedures Before Entering the Cockpit

4.1.2Procedures After Entering the Cockpit

4.2Procedures Before Starting the Engine and Starting the Engine

4.3Warming up the Engine, Engine Check

4.4Taxiing

4.5Pre Take-Off

4.6Take-Off and Climb Away

4.7Cruising Flight

4.8Descend and Landing

4.9Flight in the Rain

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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 Permitted Manoeuvres Type of operationFuel Wind Other limitsPage Power-off flight Rescue system deploymentEmergency landing Aborted 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 Assembly Dismantling the Horizontal and Vertical RudderDismantling the wings Page Tail Surfaces WingFuselage Landing GearFuel System Instrument EquipmentSense 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 Empty Weight Maximum take-off weightOperation over this range is prohibited Useful weight, weight table Centre of gravity determination