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Thorp T-211

The T-211 is a light aircraft designed in the US by John Thorp in 1945. It is a low-wing monoplane of conventional layout with a fixed tricycle undercarriage and a sliding canopy. John Thorp developed the Sky Scooter with lessons learned from developing the Lockheed Little Dipper project in 1944.[1] It bears some family resemblance to the Piper Cherokee,[clarification needed] a design that Thorp later significantly contributed to.

T-211
Role sportplane
Manufacturer Homebuilt design
IndUS Aviation as Light Sport
Designer John Thorp
First flight 1945
Status In production (2015)

Development Edit

 
2005-built Indus T211 Sky Skooter

Thorp constructed eight prototypes, had the design certified by the FAA but was unable to find a foothold in the Cessna-dominated post-war US market. The original prototypes were powered by a 65 hp Lycoming engine.[1] Novel features of the Sky Skooter include an all-movable horizontal stabilizer and externally ribbed wings and tailplane. The wings were corrugated to impart stiffness, each wing needing only three internal ribs. This feature simplified construction, reduced the number of rivits (and weight), and helped control the spanwise flow of air over the wings. [1] The T-211 was developed with a 90-horsepower Continental upgrade in 1953. 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 or T-211 Aero Sport built in Sturgis Kentucky, but only sold overseas or to part 141 operations due to current liability laws.[2] The kits were then manufactured by AD Aerospace in the United Kingdom and Venture Light Aircraft in the United States.

IndUS Aviation began production of the T-211 according to the guidelines of Light Sport Aircraft in the mid-2000s. 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 (89 kW) Jabiru 3300 engine, while the type certified version uses a 100 hp (75 kW) Continental O-200 engine and is equipped for both VFR and IFR flying.[3]

In 2010, the aircraft was also back in production as a kit aircraft by AD Aerospace of Manchester, United Kingdom. This model is powered by a four-cylinder 100 hp (75 kW) Continental O-200 or a six-cylinder 120 hp (89 kW) Jabiru 3300 powerplant.[3][4]

Variants Edit

Thorp Sky Skooter
1946
Thorp T-211
1953
Tubular Aircraft Products
1965 - Built 100 parts kits with Continental O-200 powerplants with 11 production models built
Thorp Aero
1983 - Purchased rights and tooling
IndUS Aviation
LSA production in India

Specifications (T-211) Edit

Data from Jane's All the World's Aircraft 1982–83[5]

General characteristics

  • Crew: 1 pilot
  • Capacity: 1 passenger
  • Length: 18 ft 0 in (5.49 m)
  • Wingspan: 25 ft 0 in (7.62 m)
  • Height: 8 ft 0 in (2.44 m)
  • Wing area: 105.0 sq ft (9.75 m2)
  • Empty weight: 733 lb (332 kg)
  • Max takeoff weight: 1,270 lb (576 kg)
  • Fuel capacity: 23 US gal (19 imp gal; 87 L)
  • Powerplant: 1 × Continental O-200-A air-cooled flat four, 100 hp (75 kW)
  • Propellers: 2-bladed McCauley fixed pitch propeller

Performance

  • Maximum speed: 158 mph (254 km/h, 137 kn) at sea level
  • Cruise speed: 120 mph (190 km/h, 100 kn) (75% power)
  • Stall speed: 39 mph (63 km/h, 34 kn) (flaps down)
  • Range: 480 mi (770 km, 420 nmi) at 55% power
  • Service ceiling: 19,000 ft (5,800 m)
  • Rate of climb: 950 ft/min (4.8 m/s)

See also Edit

Related development

Aircraft of comparable role, configuration, and era

References Edit

  1. ^ a b c Max Karant (August 1947). "The Thorp Sky Scooter". Flying Magazine.
  2. ^ "Tomorrows Trainer Yesterday?". Air Progress. October 1991.
  3. ^ a b Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011–12, page 60 and 90. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  4. ^ Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 92. Flying Pages Europe SARL, 2015. ISSN 1368-485X
  5. ^ Taylor, John W. R., ed. (1982). Jane's All the World's Aircraft 1982–83. London: Jane's Yearbooks. ISBN 0-7106-0748-2.

External links Edit

  • Goyer, Norm (April 2000). . Custom Planes: 52–57. Archived from the original on 2004-12-05. Retrieved 2008-05-05.
  • * (PDF). Archived from the original (PDF) on 2006-03-11. (1.15 MiB)
  • FAA Type Certificate Data Sheet for the AD Aerospace T-211

thorp, light, aircraft, designed, john, thorp, 1945, wing, monoplane, conventional, layout, with, fixed, tricycle, undercarriage, sliding, canopy, john, thorp, developed, scooter, with, lessons, learned, from, developing, lockheed, little, dipper, project, 194. The T 211 is a light aircraft designed in the US by John Thorp in 1945 It is a low wing monoplane of conventional layout with a fixed tricycle undercarriage and a sliding canopy John Thorp developed the Sky Scooter with lessons learned from developing the Lockheed Little Dipper project in 1944 1 It bears some family resemblance to the Piper Cherokee clarification needed a design that Thorp later significantly contributed to T 211Role sportplaneManufacturer Homebuilt designIndUS Aviation as Light SportDesigner John ThorpFirst flight 1945Status In production 2015 Contents 1 Development 2 Variants 3 Specifications T 211 4 See also 5 References 6 External linksDevelopment Edit nbsp 2005 built Indus T211 Sky SkooterThorp constructed eight prototypes had the design certified by the FAA but was unable to find a foothold in the Cessna dominated post war US market The original prototypes were powered by a 65 hp Lycoming engine 1 Novel features of the Sky Skooter include an all movable horizontal stabilizer and externally ribbed wings and tailplane The wings were corrugated to impart stiffness each wing needing only three internal ribs This feature simplified construction reduced the number of rivits and weight and helped control the spanwise flow of air over the wings 1 The T 211 was developed with a 90 horsepower Continental upgrade in 1953 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 or T 211 Aero Sport built in Sturgis Kentucky but only sold overseas or to part 141 operations due to current liability laws 2 The kits were then manufactured by AD Aerospace in the United Kingdom and Venture Light Aircraft in the United States IndUS Aviation began production of the T 211 according to the guidelines of Light Sport Aircraft in the mid 2000s 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 89 kW Jabiru 3300 engine while the type certified version uses a 100 hp 75 kW Continental O 200 engine and is equipped for both VFR and IFR flying 3 In 2010 the aircraft was also back in production as a kit aircraft by AD Aerospace of Manchester United Kingdom This model is powered by a four cylinder 100 hp 75 kW Continental O 200 or a six cylinder 120 hp 89 kW Jabiru 3300 powerplant 3 4 Variants EditThorp Sky Skooter 1946 Thorp T 211 1953 Tubular Aircraft Products 1965 Built 100 parts kits with Continental O 200 powerplants with 11 production models built Thorp Aero 1983 Purchased rights and tooling IndUS Aviation LSA production in IndiaSpecifications T 211 EditData from Jane s All the World s Aircraft 1982 83 5 General characteristicsCrew 1 pilot Capacity 1 passenger Length 18 ft 0 in 5 49 m Wingspan 25 ft 0 in 7 62 m Height 8 ft 0 in 2 44 m Wing area 105 0 sq ft 9 75 m2 Empty weight 733 lb 332 kg Max takeoff weight 1 270 lb 576 kg Fuel capacity 23 US gal 19 imp gal 87 L Powerplant 1 Continental O 200 A air cooled flat four 100 hp 75 kW Propellers 2 bladed McCauley fixed pitch propellerPerformance Maximum speed 158 mph 254 km h 137 kn at sea level Cruise speed 120 mph 190 km h 100 kn 75 power Stall speed 39 mph 63 km h 34 kn flaps down Range 480 mi 770 km 420 nmi at 55 power Service ceiling 19 000 ft 5 800 m Rate of climb 950 ft min 4 8 m s See also EditRelated development Thorp T 18Aircraft of comparable role configuration and era Erco Ercoupe Grumman American AA 1References Edit a b c Max Karant August 1947 The Thorp Sky Scooter Flying Magazine Tomorrows Trainer Yesterday Air Progress October 1991 a b Bayerl Robby Martin Berkemeier et al World Directory of Leisure Aviation 2011 12 page 60 and 90 WDLA UK Lancaster UK 2011 ISSN 1368 485X Tacke Willi Marino Boric et al World Directory of Light Aviation 2015 16 pages 92 Flying Pages Europe SARL 2015 ISSN 1368 485X Taylor John W R ed 1982 Jane s All the World s Aircraft 1982 83 London Jane s Yearbooks ISBN 0 7106 0748 2 External links Edit nbsp Wikimedia Commons has media related to Thorp T211 Goyer Norm April 2000 Custom Build the Thorp T 211 Custom Planes 52 57 Archived from the original on 2004 12 05 Retrieved 2008 05 05 IndUS Aviation Sport Pilot article PDF Archived from the original PDF on 2006 03 11 1 15 MiB FAA Type Certificate Data Sheet for the AD Aerospace T 211 Retrieved from https en wikipedia org w index php title Thorp T 211 amp oldid 1171949868, wikipedia, wiki, book, books, library,

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