Edge540
Plane/Edge540.png
Edge540

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General
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Engine:
Modified Textron-Lycoming AEIO-540-EXP 
producing 310 HP @ 2700RPM

Propeller: Hartzell HC-C3YR-4AX composite,
three blade, constant speed, counter 
balanced with Hartzell governor. 

Crew: 1

Length:	20 ft 7 in (6.27 m)
Wingspan: 24 ft 4 in (7.42 m)
Height: 7 ft 9 in (2.36 m)
Wing area: 98 ft² (9.1045 m²)

Wing:
Span: 24 ft 4” (7.41 m)
Area: 98 ft²  (9.10 m²)
Air-foil design: Unique John Roncz Design
Chord: Root: 62” Tip: 29” (1.57 m / .73 m )
Aileron Deflection: +/-25deg

Horizontal:
Span: 8 ft 1” (2.46 m)
Area: 22 ft²  (2.04 m²)
Elevator Deflection: +/-25deg

Vertical:
Area: 14 ft 10” (4.52 m)
Height: 5 ft 2” (1.57 m)
Rudder Deflection: +/-30deg

Empty weight: 1170 lbs (530.7 kg)
Max aerobatic weight: 1550 lbs (703 kg)
Gross weight: 1800 lbs (816.4 kg)

Maximum airspeed Vne: 230 Kts
Max full aerobatic airspeed Va: 170 Kts
Power off stall Vso: 51 Kts @1550lbs
Max roll rate: 420 deg/sec typ.
Max rate of climb: 3,700 ft/min

Fuel Capacity: 61.5 US Gallons (232.8 lit)
(17.5 fuselage+22 each wing)(66.24 lit/83.27 lit)

Inverted Flight Time: Unlimited