Atec ATEC 212 SOLO ROTAX 912 UL manual Rescue system deployment, Power-off flight

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3.1.Engine Failure on Take-Off

1.Push stick forward aircraft into gliding attitude and maintain airspeed of 100 km/h (54 kt).

2.Determine the wind direction, adjust flaps for suitable position, turn off fuel valve,

switch-off ignition, adjust safety belts and switch-off the master switch just before landing.

A.At a height up to 50 m get the aircraft into landing configuration and carry out a landing with respect for obstructions in take-off direction.

B.At a height above 50 m choose a suitable area for emergency landing.

3.2.Engine Failure in Flight

1.Get the aircraft into gliding attitude and maintain airspeed of 100 km/h (54 kt).

2.Check a fuel level, switch on and make sure ignition is switched on.

3.If no problem found, try restarting the engine once more using additional fuel system.

4.If restarting impossible, use the instructions 3.1.

3.3.Rescue system deployment

In distress by final loss of flight control do activate the rescue system

1.Switch off ignition

2.Adjust safety belts

3.Activate the rescue system

In case of landing on a limited area when collision is inevitable, use the rescue system for a braking devise.

The aircraft can be damaged or the crew may be injured due to using a rescue system

3.4.Fire in flight

1.Close the fuel valve

2.Open the throttle

3.Switch off the main switch and ignition

4.Do emergency landing

5.Get off the aircraft

3.5.Power-off flight

1. Speed …………………… 100 km/h ….. 54 kt

3.Flaps retracted

4.Normal flight conditions

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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 Type of operation Permitted ManoeuvresFuel Wind Other limitsPage Power-off flight Rescue system deploymentAborted landing Emergency landingVibrations 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 Horizontal and Vertical Rudder AssemblyDismantling the wings Page Wing FuselageTail Surfaces Landing GearInstrument Equipment Fuel SystemSense of Motion of the Control Elements Page Page Safety Belts Flap ControlCanopy Open / Close Flight Control InstrumentsCleaning and Care Aeroplane RepairsMajor Overhaul Anchorage of the AeroplanePage Maximum take-off weight Empty WeightOperation over this range is prohibited Useful weight, weight table Centre of gravity determination