Atec ATEC 212 SOLO ROTAX 912 UL manual Warming up the Engine, Taxiing, Pre Take-Off

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5.Throttle to idle run

6.Open the choke if the engine is cold

7.Pull up the control stick

8.Main switch on

9.Ignition on

10.Brakes on

11.Start the engine

12.Turn off the choke

13.Warm up the engine until the operating temperature

4.3.Warming up the Engine

Start to warm up the engine at 2000 rpm, hold approx. 2 minutes, continue until 2500 rpm till the oil temperature reaches 50oC. Check both ignition circuits according to Art. 4.5.

4.4.Taxiing

Recommended speed of taxiing is 15 km/h ….. 8 kt max, direction is controlled by the tail

wheel using pedals. Hand brake control is on the control stick. Control stick pulled up.

4.5.Pre Take-Off

Compulsory procedures prior take-off:

1.

Brakes

checked

2.

Foot-operated controls

checked

3.

Hand operated controls

checked

4.

Flap position I set and

checked

5.

Choke turned off

checked

6.

Fuel master switch on and

checked

7.

Fuel gauge indicator

checked

8.

Instruments on and within limits

checked

9.

Safety belts secure

checked

10.

Cockpit secure and locked

checked

4.6.Take – Off and Climb Away

By accelerating until the maximum position of the throttle is reached, make the aeroplane move. Fly off the tail wheel pushing control stick and then get control back to neutral position. Keep the aeroplane running on the main wheels at a normal flight position in the axis of the runway using rudder and elevator control. At speed of 75 km/h … 40 kt you make the aeroplane fly off the earth by a light pull of the stick and continue the flight until 110 km/h … 59 kt Then by gradual pull you make the aeroplane start climbing at the optimum speed of 120 - 140 km/h … 65 – 75 kt. Retract flaps after the height of 50 m … 150 feet and a speed of 120 km/h … 65 kt is reached. The marginal engine values must not be exceeded during the take-off.

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Contents Atec 212 Solo Atec 212 Solo Type of aeroplanePage Page Introduction Personal data of the ownerSpecification Dimensions Rescue System installed / not installed………Weights Description of the AeroplanePower Oil TemperatureTemperature of Engine Cylinders Operational TemperatureThree-View Sketch Page Never exceed the maximum take-off weight of the aeroplane Air SpeedsDo 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 Wind Other limitsPage Power-off flight Rescue system deploymentVibrations Emergency landingAborted landing Page Procedures Before Entering the Cockpit Pre-Flight InspectionWarming up the Engine TaxiingPre Take-Off Take Off and Climb AwayCruising flight Descent and landingPage Stalling Speeds CAS Take off Distance at 15 m / 50 feet heightRate of Climb Cruising SpeedsPage Dismantling the wings AssemblyDismantling the Horizontal and Vertical Rudder Page Wing FuselageTail Surfaces Landing GearSense of Motion of the Control Elements Fuel SystemInstrument Equipment Page Page Safety Belts Flap ControlCanopy Open / Close Flight Control InstrumentsCleaning and Care Aeroplane RepairsMajor Overhaul Anchorage of the AeroplanePage Operation over this range is prohibited Empty WeightMaximum take-off weight Useful weight, weight table Centre of gravity determination