Thorp T-211
From Wikipedia, the free encyclopedia
| T-211 | |
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| Type | sportplane |
| Manufacturer | Homebuilt design IndUS Aviation as Light Sport |
| Designed by | John Thorp |
| Maiden flight | 1945 |
The T-211 is a light aircraft designed in the US by John Thorp in 1945. It is a low-wing monoplane of conventional design with fixed tricycle undercarriage and a sliding canopy. It bears some family resemblance to the Piper Cherokee, a design that Thorp contributed to significantly.
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[edit] Development
Thorp constructed eight prototypes, and had the design certified by the FAA, but was unable to find a foothold in the Cessna-dominated post-war US market. The project was therefore shelved until the homebuilding boom saw the rights to the aircraft acquired first by Adams Industries and then by Thorp Aero in the 1970s, the latter firm building five examples as the Thorp Arrow. The kits were then manufactured by AD Aerospace in the United Kingdom and Venture Light Aircraft in the United States.
IndUS Aviation recently began production of the T-211 to the guidelines of Light Sport Aircraft, allowing it to be flown by those with a sport pilot certificate. The Thorp T-211 was the first US-designed Special Light Sport Aircraft to receive certification from the Federal Aviation Administration. The light-sport version uses the 120 hp Jabiru 3300 engine, while the fully certificated version uses a 100 hp Continental O-200 engine and is equipped for both VFR and IFR flying.
[edit] Specifications (T-211)
This aircraft article is missing some (or all) of its specifications. If you have a source, you can help Wikipedia by adding them.General characteristics
- Crew: 1 pilot
- Capacity: 1 passenger
- Length: 18 ft 2 in (5.49 m)
- Wingspan: 25 ft 0 in (7.62 m)
- Height: 6 ft 1 in (1.92 m)
- Wing area: 105 ft² (9.67 m²)
- Empty weight: 750 lb (339 kg)
- Max takeoff weight: 1,270 lb (575 kg)
- Powerplant: 1× Continental O-200-A, 100 hp (75 kW)
- * Fuel capacity: 21 gal usable (78 l)
- Baggage capacity: 40 lb (18 kg)
Performance
- Maximum speed: 120 mph (193 km/h)
- Range: 375 miles (764 km)
- Service ceiling 12,500 ft (3,810 m)
- Rate of climb: 750 ft/min (229 m/min)
- Wing loading: 12.1 lb/ft² (60 kg/m²)
- Power/mass: 0.08 hp/lb (0.13 kW/kg)
[edit] External links
- Goyer, Norm (April 2000). "Custom-Build the Thorp T-211". Custom Planes: 52-57.
- AD Aerospace product page
- IndUS Aviation
- Sport Pilot articlePDF (1.15 MiB)
[edit] See also
Related development
Comparable aircraft
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