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Liberty Technologies, Inc. |
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Model Liberty 750T Specifications: The Liberty 750 is a two seat light turbine helicopter using a 24' Diameter, two bladed Semi rigid teetering rotor system with a 750 lb useful load and powered by a 150 hp turbine engine. It has an empty weight of 750 lbs, fuel capacity of 44 gal, and fuel burn of 16 gph at 100 knot (115 mph) cruise speed. (Max Range, 2.25hrs/.5hr reserve 258 miles) Airspeed Limits VNE (Never Exceed Speed) at sea level is 115 knots (132 mph) CAS. For reduction of VNE with altitude, temperature and N1, see FAA Approved Rotorcraft Flight Manual. Autorotation VNE at sea level is 115 knots (132 mph) CAS. Built under Kit and Amateur Built Rules.Sample
Primary
Function: Entry-level turbine trainer using two bladed rotor systems. Fuel:
Jet A, Jet B, JP4, JP8, Kerosene VNE:
115 Knots, 132 mph, 212.9 km/hr Ceiling: 15,000 feet (4572 meters) Range: 219nm, 253 miles (407 kilometers) Crew: student pilot and instructor Armament: None Date Deployed: Jan 2006 Base Unit Cost: $150,000 engine included, Optional IFR Lite Glass Cockpit including Remote Radios $40,000.
Liberty 750 Estimated Operational Cost
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