Engineering:Sport Hornet LRS
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| Sport Hornet LRS | |
|---|---|
| General information | |
| Type | Personal use and flight training aircraft |
| Manufacturer | Higher Class Aviation |
| Designer | Jim Millet |
| History | |
| First flight | 1992 |
The company and website appear to be defunct.[speculation?]
Specifications
Data from Sport Hornet [1]
General characteristics
- Crew: one pilot
- Capacity: one passenger 540 lb (245 kg) useful load (option dependent)
- Length: 21 ft 6 in (6.55 m)
- Wingspan: 30 ft 0 in (9.14 m)
- Height: 9 ft 0 in (2.74 m)
- Wing area: 155 sq ft (14.4 m2)
- Airfoil: Eiffel 370
- Empty weight: 680 lb (308 kg)
- Max takeoff weight: 1,320 lb (600 kg)
- Powerplant: 1 × Rotax 912 ULS IVO Medium 3, 100 hp (74.6 kW)
Performance
- Maximum speed: 120 kn (138 mph, 222 km/h)
- Cruise speed: 100 kn (115 mph, 185 km/h)
- Stall speed: 35 kn (40 mph, 64 km/h)
- Never exceed speed: 120 kn (138 mph, 222 km/h)
- Range: 440 nmi (620 mi, 1,000 km)
- Service ceiling: 10,000 ft (3,050 m)
- Rate of climb: 1,000 ft/min (5.1 m/s)
References
- ↑ "Sport Hornet Light Sport Airplane". Higher Class Aviation. http://www.sporthornet.com. Retrieved 2008-11-20.
External links
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