Sport Hornet LRS
 | This article has multiple issues. Please help improve it or discuss these issues on the talk page. (Learn how and when to remove these messages)
|
| Sport Hornet LRS | |
|---|---|
| Role | Personal use and flight training aircraft |
| Manufacturer | Higher Class Aviation |
| Designer | Jim Millet |
| First flight | 1992 |
The Sport Hornet LRS is a Light Sport Aircraft. One unique attribute that sets the Sport Hornet LRS apart from other LSA Aircraft is the air spring suspension system on the landing gear. This protects the aircraft from damage in the event of "miscalculated" landings and allows for a better experience for the pilot and passengers.[citation needed]
The company and website appear to be defunct.[speculation?]
Specifications
[edit]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
[edit]- ^ "Sport Hornet Light Sport Airplane". Higher Class Aviation. Archived from the original on 2007-07-03. Retrieved 2008-11-20.
External links
[edit]
 | This article on an aircraft of the 1990s is a stub. You can help Wikipedia by expanding it. |