Taylor Monoplane
| J.T.1 Monoplane | |
|---|---|
 | |
| Taylor J.T.1 built in 1971 | |
| Role | home build aircraft |
| Designer | John Taylor |
| First flight | 4 July 1959 |
| Number built | 110 (2015)[1] |
| Unit cost |
approximately $1285 to build in 1971[2] |
The Taylor J.T.1 Monoplane is a British fixed-wing aircraft design for a homebuilt aircraft, developed in the 1950s by J.F. Taylor.[3]
History
The J.T.1 Monoplane was designed by John Taylor in 1956 and the prototype (registered G-APRT) was built by him at Ilford, Essex between 1958-1959. It flew for the first time on 4 July 1959 [4] at White Waltham. At that time it represented the first post war homebuilt design to come from England.
Construction
It was designed to be constructed in small spaces with the minimum of tools and material cost, requiring only average building skills from the constructor. It is aimed exclusively at the lower power range such as the 40 hp (30 kW) Volkswagen air-cooled engine, therefore giving economy with an acceptable cruise speed. It is semi- aerobatic.
Operation
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The airframe of the J.T.1 Monoplane was proof loaded to verify the stress calculations and no modification has ever been introduced since the prototype was approved. The total number flying to date is over 110 examples.[3]
As a result of a request for an aircraft with higher performance than the Taylor Monoplane, Taylor designed a high performance single-seater, the Taylor Titch. Taylor built the prototype, registered G-ATYO, at Leigh-on-Sea, Essex between 1965 and 1966; the Titch first flew at Southend Airport on 4 January 1967.[5]
Specifications
Data from Jane's All The World's Aircraft 1982–83[6]
General characteristics
- Crew: 1
- Length: 15 ft 0 in (4.57 m)
- Wingspan: 21 ft 0 in (6.40 m)
- Height: 4 ft 10 in (1.47 m)
- Wing area: 76 ft² (7.06 m²)
- Empty weight: 410 lb (186 kg)
- Max. takeoff weight: 610 lb (276 kg)
- Powerplant: 1 × J.A.P. two-cylinder piston, 38 hp (28 kW)
Performance
- Never exceed speed: 130 mph (113 knots, 209 km/h)
- Maximum speed: 105 mph (91 knots, 169 km/h) at sea level
- Cruise speed: 90 mph (78 knots, 145 km/h)
- Stall speed: 38 mph (33 knots, 62 km/h)
- Range: 230 mi (200 nmi, 370 km)
- Rate of climb: 1000 ft/min (5.1 m/s)
See also
- Related development
References
Notes
- ↑ Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 129. Flying Pages Europe SARL, 2015. ISSN 1368-485X
- ↑ Kohn. Leo J. "The true cost of building your own plane." Air Trails Winter 1971, p. 63.
- 1 2 Bayerl and Berkemeier et al. 2011, p. 122.
- ↑ Taylor 1988, p. 548.
- ↑ Purdy 1998, p. 267.
- ↑ Taylor 1982, p. 522.
Bibliography
- Bayerl, Robby, Martin Berkemeier et al. World Directory of Leisure Aviation 2011–12. Lancaster UK: WDLA UK, 2011. ISSN 1368-485X.
- Jackson, A.J. British Civil Aircraft since 1919, Volume 3. London: Putnam, 1974. ISBN 0-370-10014-X.
- Purdy, Don: AeroCrafter: Homebuilt Aircraft Sourcebook, Fifth Edition. Benicia, California: BAI Communications, 1998. ISBN 978-0-96364-093-2.
- Taylor, John W. R., ed. Jane's All The World's Aircraft 1982–83. London: Jane's Yearbooks, 1982. ISBN 0-7106-0748-2.
- Taylor, John W. R., ed. Jane's All the World's Aircraft 1988–1989. Coulsdon, Surrey, UK: Jane's Information Group, 1988. ISBN 0-7106-0867-5.
External links
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