Atec ATEC 212 SOLO ROTAX 912 UL manual Emergency landing, Aborted landing, Vibrations

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3.6.Emergency landing

1.Carried out in case of engine failure

2. Speed ……………………. 100 km/h ….. 54 kt

3.Adjust safety belts

4.Flaps according to situation

5.Announce the situation by the aeroplane radio station

6.Close the fuel valve

7.Turn off ignition

8.Turn off the main switch

In case of emergency landing onto a terrain and surfaces non-approved for light aircraft

landings an aircraft damage and crew injury may occur

3.7.Precautionary landing

Carry out in case of the loss of orientation, fuel exhaustion or for other reason if the aircraft is fully controllable.

1.Determine the wind direction

2.Choose a suitable landing area

3.Carry out a low pass into the wind along the right-hand side of landing area and inspect the area thoroughly.

4.Carry out a circuit flight

5.Calculate the landing plan

6.Land in the first third of the landing area using landing flaps

3.8.Aborted landing

Carry out in case of wrong calculation of landing manoeuvre or after jump out by landing in case of pilot’s consideration to abort landing manoeuvre and continue to fly.

1.Set up engine speed on maximum power

2.Set up take-off flaps position – I

3.

Get level speed 110 km/h

….. 59 kt

4.Draw up control stick slowly to get aircraft into climbing at speed 140 km/h ..... 75 kt

5.Retract flaps at an air speed 120 km/h ….. 76 kt

6.

Keep runway direction all the take off time using rudder

3.9.Vibrations

In case of unusual vibrations occurs.

1.Set the engine speed to where vibration is least

2.Carry out the safety landing checks for a possible emergency landing and head for the nearest airport

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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