Atec ATEC 212 SOLO ROTAX 912 UL Pre-Flight Inspection, Procedures Before Entering the Cockpit

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4.1.Pre-Flight Inspection

It is important to carry out a proper pre-flight inspection failure to do so or perform an incomplete inspection could be the cause of an accident. The manufacturer recommends using the following procedure:

4.1.1. Procedures Before Entering the Cockpit

1.Check ignition - turned off.

2.Check main switch – turned off

3.Check the wings, wing surfaces ailerons and flaps, clearances, hinges and connections of the controls, security of the wing pins, Pitot tube.

4.Check the tail surfaces, elevator and rudder for secure connections, clearances and free movement.

5.Check the fuselage, the surface and state.

6.Check the landing gear, laminate springs, security of main and front wheels, their covers, screws and nuts, proper tire pressure, break function.

7.Engine – the state of fastening of the engine covers, the state of the engine bed, intact fuel, oil and cooling system hoses, the fuel system drain.

8.Propeller – the surface state, if it is intact, the state and fastening of the propeller cone.

9.Canopy – control of fastening and proper locking of the canopy, correct functioning and condition of the electrical installation of instruments, the state of the flight instruments, control of the fuel level, proper functioning of controls.

Before entering the cockpit step on the marked foot-path on the wing only. Stepping outside the marked area especially on the flap may damage the airframe seriously

4.1.2Procedures After Entering the Cockpit

1.Check foot-operated controls

2.Check brakes – brakes on

3.Check hand - operated controls

4.Check flaps

5.Check engine controls

6.Check fuel valve

7.Check fuel level indicator

8.Check main switch – turned off

9.Check ignition – turned off

10.Check instruments – state, zero positions, adjust altimeter

4.2.Procedures Before Starting the Engine and Starting the Engine

1.Rescue system - unlock

2.Safety belts - fasten

3.Close the canopy and secure

4.Turn on the fuel valve

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Contents Atec 212 Solo Type of aeroplane Atec 212 SoloPage Page Personal data of the owner IntroductionDescription of the Aeroplane Specification DimensionsRescue System installed / not installed……… WeightsOperational Temperature PowerOil Temperature Temperature of Engine CylindersThree-View Sketch Page Do not exceed this speed by flaps deflected Never exceed the maximum take-off weight of the aeroplaneAir Speeds Do not exceed this speed in any caseCentre 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 CockpitTake Off and Climb Away Warming up the EngineTaxiing Pre Take-OffDescent and landing Cruising flightPage Cruising Speeds Stalling Speeds CASTake off Distance at 15 m / 50 feet height Rate of ClimbPage Dismantling the Horizontal and Vertical Rudder AssemblyDismantling the wings Page Landing Gear WingFuselage Tail SurfacesInstrument Equipment Fuel SystemSense of Motion of the Control Elements Page Page Flight Control Instruments Safety BeltsFlap Control Canopy Open / CloseAnchorage of the Aeroplane Cleaning and CareAeroplane Repairs Major OverhaulPage Maximum take-off weight Empty WeightOperation over this range is prohibited Centre of gravity determination Useful weight, weight table