Omega LSA

by Omega Aircraft
2.7
3
Omega LSA - Photo #1

Omega Aerobatic
The Omega design features rear sliding canopy, adjustable sliding seats, drop-hinged, ailerons and flaps, large aerodynamic counter balanced rudder and elevator, with dorsal fin to aid in spin recovery, in a traditional aluminium monocoque airframe

Wing spars
The wing spars are machined from solid 2024 T3 bar for ultimate strength. Solid rivets are used to construct the spar web.

Fuel system
Fuel is stored in two wing tanks of 50 litres capacity each. The fuel tanks are mounted in the leading edge of the spar and are removable for inspection.

Roll Over Protection
The Omega has a steel roll bar supporting the front screen and a high turtle deck offering additional protection. The canopy is rear sliding for easy exit. The fin has been designed to help also in a roll over situation.

Control system
Omega will feature either dual or single control sticks from a central pivoted point. To change from single to dual is just a matter of pulling a pin. The rudder is controlled by stainless steel cables. The multi electric position Fowler flaps All control system components are fabricated on CNC machines, assuring a high level of precision. Will be a viable soon www.omega-aircraft.co.nz

Specifications

Empty weight:
661 lbs (300 kg)
MTOW:
1340 lbs (608 kg)
Stall speed:
42 kts (48 mph) (78 kph)
Cruise speed:
110 kts (127 mph) (204 kph)
VNE:
160 kts (184 mph) (296 kph)
Climb:
1000 ft/min (5.1 m/s)
Take-off distance:
918 ft (280 m)
Landing distance:
1000 ft (305 m)
Engine:
Gemimi, ULpower
Fuel consumption:
5 GPH (18.9 LPH)
For sale for: USD 75,000 / EUR 69,000