Folkerts Henderson Highwing
| Folkerts Henderson Highwing | |
|---|---|
 | |
| Folkerts Henderson Highwing on display | |
| Role | Homebuilt aircraft |
| National origin | United States |
| Designer | Clayton Folkerts |
| Number built | 1 |
|
| |
The Folkerts Henderson Highwing is an American single place homebuilt aircraft developed by air-racer Clayton Folkerts.
Design and development
The Folkerts Henderson Highwing is a single place, open cockpit, high-wing light aircraft powered by a Henderson-B4 engine. The aircraft features all-wood construction [1][2]
Specifications (Highwing)
Data from EAA
General characteristics
- Crew: 1
- Wingspan: 24 ft (7.3 m)
- Empty weight: 210 lb (95 kg)
- Gross weight: 450 lb (204 kg)
- Powerplant: 1 × Heath-Henderson B-4 Inline four cylinder, 20 hp (15 kW)
Performance
- Maximum speed: 65 kn; 121 km/h (75 mph)
- Cruise speed: 56 kn; 105 km/h (65 mph)
References
- ↑ "Folkerts Henderson Highwing". Retrieved 21 August 2014.
- ↑ Flight Global: 1920. December 1977. Missing or empty
|title=(help)
This article is issued from Wikipedia - version of the 6/23/2015. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.