Atec ATEC 212 SOLO ROTAX 912 UL manual Fuel System, Instrument Equipment

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7.7.Fuel System

The fuel system is formed by an integral fuselage tank with a fuel drain. Double fuel supply circuit with a spare electric pump. The pressure of supplied fuel is measured with a fuel- pressure gauge. The fuel reserve 10 l at flight position is indicated by control light.

7.8.Instrument Equipment

The instrument equipment consists of basic instruments for flight control, engine control and navigation. The static and total pressure is taken from the Pitot tube at the bottom of the port wing.

7.9.The Sense of Motion of the Control Elements

Foot-operated control

By pressing the left pedal, the aeroplane turns left when mowing at sufficient speed on the ground or in the air, and vice versa.

Hand-operated control

By pulling the control stick towards the pilot, the nose lifts up (the angle of incidence increases) and the aeroplane climbs. By pushing the control stick, the aeroplane descends. By deflecting the control stick to left, the aeroplane banks to left, and vice versa.

Wing flaps

By switching over the flap change-over switch to I, II, III or OFF position, the flaps are moved to corresponding deflection by electric actuator. Each position is indicated by LED control light.

The engine throttle

By moving the throttle in the flight direction, the engine power increases, and vice versa.

Choke

Choke lever backwards – the choke is turned on

Choke lever forwards – the choke is turned 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 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