Atec ATEC 212 SOLO ROTAX 912 UL manual Permitted Manoeuvres, Type of operation, Fuel

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2.6.Permitted Manoeuvres

Category of the aeroplane: Normal

Except of the normal flight manoeuvres, the sharp turns up to bank of 60o, level and climbing turns are permitted.

Acrobatics, intended spins and stalls are prohibited

2.7.Operational Load Factors

Maximum positive load factor in CG Maximum negative load factor in CG

………+6,0 g

………-4,0 g

2.8.Type of operation

Permitted day flights VFR only ( flights by unobstructed field of vision )

IFR flights ( instrument flights ) and flights by ice formation are prohibited

2.9. Crew

 

 

 

 

Number of seats ………………….

1

 

 

Minimum weight of crew

………….

65

kg

see Art. 9.4.

Maximum weight of crew

………….

90

kg

see Art. 9.4.

2.10. Fuel

Recommended motor fuel unleaded petrol with oil. Minimum octane number of petrol 95. Oil / Fuel mixture 1 : 50.

Fuel capacity

………………….

49 l

Not usable rest of fuel

………….

0,7 l

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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 aeroplane Do not exceed this speed in any case Do not exceed this speed by flaps deflectedCentre of Gravity CG Manoeuvre and Gust Envelope Type of operation Permitted ManoeuvresFuel Other limits WindPage Rescue system deployment Power-off flightAborted landing Emergency 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 Dismantling the Horizontal and Vertical Rudder AssemblyDismantling the wings Page Fuselage WingTail Surfaces Landing GearInstrument Equipment Fuel SystemSense 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 Maximum take-off weight Empty WeightOperation over this range is prohibited Centre of gravity determination Useful weight, weight table