Flight manual evektor sportstar

Procedure for weighing the airplane and the calculation method for establishing the permitted payload range are contained in the Aircraft Maintenance and Inspection Procedures for the SportStar MAX Light Sport Aircraft. Check, whether the intersection of Take-off weight horizontal line and Total Static Moment vertical line is inside the envelope.

Page Introduction This section describes systems of the airplane and its operation. Page Control Pilot Operating Handbook 7. Directional control is connected by means of pull rods with nose landing gear control. Main landing gear brakes are controlled by pedals of directional control. Airplane is equipped with dual control enabling flight with two-member crew.

Control Stick 2. Fuel Selector 3. Flaps Control 4. Ignition 6. Throttle Knob 7. Choke 8. Engine Instruments Page Instrument Panel Wheels can be fitted with fiber-glass aerodynamic pants. Brake system is composed of toe-brake pedals these are a part of rudder control pedals , brake pumps, brake fluid reservoir, brake fluid central bottle on the firewall, hoses for leading brake liquid, brake yokes with wheel cylinders and brake pads.

Page Power Unit 7. Cooling circuit of cylinder heads is designed as a closed system containing pump, expansion reservoir 1 with pressure closure 3 , cooler of cooling liquid 2 and drainage reservoir 4. Scheme of cylinder head cooling system is shown in Fig. The engine lubrication system is equipped with an oil pump 1 ensuring oil feeding from the reservoir 4 located on the fire wall through the oil cooler 5 and the oil cleaner 6 to the lubricated points of engine.

Page Ignition System Both circuits are on and starter is cranking the engine 7. The fuel system of the SportStar MAX airplane is composed of integral fuel tanks, fuel line, fuel selector, fuel filter, mechanical fuel pump - located on the engine auxiliary electrical fuel pump can be installed , a distribution pipe for delivery of fuel to the engine, with a fuel return branch, fuel gauges and fuel tank drain valves.

The fuel filter is under the cockpit on the left airframe panel. A Watt generator, feeding by a drive belt from the engine, is the primary source of electrical energy.

Page 79 Pilot Operating Handbook 7. It is located under the left half of the wing. Total pressure is sensed through the opening in the Pitot-static tube face. Page 80 Pilot Operating Handbook 7.

Vents are connected to the NACA scoops through tip-up canopy frame front flaps. Cockpit heating is provided by air conducted through a hose guided from a fiberglass collector behind the engine radiator into the heat exchanger and then into the mixture flap on the firewall and further through a directional flap to the cockpit floor or to the hot air outputs through the Page 82 Pilot Operating Handbook - Termination.

Page 83 Pilot Operating Handbook Print page 1 Print document 83 pages. Rename the bookmark. Delete bookmark? Cancel Delete. Delete from my manuals? Sign In OR. By continuing to use this website, you consent to our use of these cookies. Learn more. The EuroStar, SportStar and the Harmony are state-of-the-art two seater airplanes for pilot training and leisure flying. Evektor assures development activities in the aircraft and automotive industries as well as in the general engineering industry.

We employ experienced designers, state-of-the-art software tools and we also offer advanced rapid prototyping technologies. Evektor has the necessary know-how and software tools for complex stress analysis, fatigue life analysis, aerodynanamic calculations and analysis of electromagnetic field effects.

Evektor is one of the pioneers in the use of Rapid Prototyping technologies in aircraft development. List of the available manuals for the SportStar RTC airplane and latest revisons are stated in the following table:. SportStar RTC. Harmony LSA. EV Outback. VUT Cobra. Aircraft development.