The Ultrasport 496 meet the FAA Part 21.191 (g) as Amateur-Built Aircrafts
* Denotes FAA 14 CFR PART 103 Restriction for Ultralights
Specifications Ultrasport 496
Dual Seat Experimental small helicopter
Engine: 150 Hp T62-T32, Electric Start, 12VDC & 24VDC, Starter Gen
Transmission: 11.1Two Stage Xmn ,engine 2.61
Fuel Capacity: 75 litres
Endurance: 2 Hours
Service Ceiling: 10.000
H.I.G.E. 8000
H.O.G.E. TBD
Main Rotor: 2 Blade, 23 Ft. Rotor Dia., 6.7 In. Chord, Composite Construction
Tail Rotor: 4 Blade, 2.6 Ft. Rotor Dia., 2 In. Chord, Composite Construction
Cabin Length: 53 Inches (1,346 mm)
Cabin Width: 48 Inches (1,219 mm)
Cabin Height: 59 Inches (1,499 mm)
Cruise Speed: 70 Knots
Max Speed (VNE): 90 Knots (103 mph) (166 km/h)
Empty Weight: 500lbs
Useful Load: TBD
Gross Weight: 1130 lbs
Width (at Skid Tubes): 7Ft
Height: 8 Feet, 0.5 Inches. (2,451 mm)
Length: 26 Feet, 9 Inches (8,153 mm)
Length (Blade Folded): 19 Feet, 9 Inches. (6,020 mm)