Ultrasport 496T | |
---|---|
Role | Helicopter |
National origin | Cyprus |
Manufacturer | LAE Helicopters Cyprus |
Status | Production completed |
Developed from | American Sportscopter Ultrasport 496 |
The LAE Ultrasport 496T is a Cypriot helicopter that was produced by LAE Helicopters Cyprus of Larnaca. Now out of production, when it was available the aircraft was supplied complete and ready-to-fly. [1]
The aircraft was reportedly in production in 2015, but by the end of 2017 production had ended in favour of the new LAE Piranha. [1]
The Ultrasport 496T is derived from the American Sportscopter Ultrasport 496, replacing the two-stroke powerplant with a turboshaft engine. [1]
The 496T was designed to comply with the European Class 6 microlight helicopter rules. It features a single main rotor and tail rotor, a two-seats-in side-by-side configuration enclosed cockpit with a windshield, skid landing gear and a 160 hp (119 kW) Solar T62 turbine engine. [1]
The aircraft fuselage is made from composites. It has a two-bladed main and a ring-mounted tailrotor. The aircraft has a typical empty weight of 260 kg (573 lb) and a gross weight of 450 kg (992 lb), giving a useful load of 190 kg (419 lb). [1]
Reviewer Werner Pfaendler, noted that it has "an exceptional power to weight ratio". [1]
Data from Tacke [1]
General characteristics
Ultrasport 496T | |
---|---|
Role | Helicopter |
National origin | Cyprus |
Manufacturer | LAE Helicopters Cyprus |
Status | Production completed |
Developed from | American Sportscopter Ultrasport 496 |
The LAE Ultrasport 496T is a Cypriot helicopter that was produced by LAE Helicopters Cyprus of Larnaca. Now out of production, when it was available the aircraft was supplied complete and ready-to-fly. [1]
The aircraft was reportedly in production in 2015, but by the end of 2017 production had ended in favour of the new LAE Piranha. [1]
The Ultrasport 496T is derived from the American Sportscopter Ultrasport 496, replacing the two-stroke powerplant with a turboshaft engine. [1]
The 496T was designed to comply with the European Class 6 microlight helicopter rules. It features a single main rotor and tail rotor, a two-seats-in side-by-side configuration enclosed cockpit with a windshield, skid landing gear and a 160 hp (119 kW) Solar T62 turbine engine. [1]
The aircraft fuselage is made from composites. It has a two-bladed main and a ring-mounted tailrotor. The aircraft has a typical empty weight of 260 kg (573 lb) and a gross weight of 450 kg (992 lb), giving a useful load of 190 kg (419 lb). [1]
Reviewer Werner Pfaendler, noted that it has "an exceptional power to weight ratio". [1]
Data from Tacke [1]
General characteristics