Ultimate 10-200

Ultimate 10-200
Role	Homebuilt aircraft
National origin	Canada
Manufacturer	Streamline Welding
Introduction	1990s
Status	Production completed

TheUltimate 10-200is a Canadianhomebuilt aerobatic biplanethat was designed produced byStreamline WeldingofHamilton, Ontario,introduced in the 1990s. When it was available the aircraft was supplied as a kit or in the form of plans for amateur construction.^[1]

Design and development

The aircraft started out as a replacement set of wings for thePitts Specialand eventually a new fuselage was designed to go with the wing set. The resulting aircraft features astrut-bracedbiplane layout, withcabane struts,interplane strutsandflying wires,a single-seat, enclosed cockpit under abubble canopy,fixedconventional landing gearwithwheel pantsand a single engine intractor configuration.^[1]

The aircraft is made from metal with its flying surfaces covered indoped aircraft fabric.Its wing span is only 16.00 ft (4.9 m). The acceptable power range varies by each model. Standard equipment includes an inverted fuel system and rear-hinged canopy. Operationalg loadsare +7 and -5 g. The aircraft has a roll rate of 360 degrees per second.^[1]

The 10-200 version has a typical empty weight of 925 lb (420 kg) and a gross weight of 1,320 lb (600 kg), giving a useful load of 395 lb (179 kg). With full fuel of 22 U.S. gallons (83 L; 18 imp gal) the payload for the pilot and baggage is 263 lb (119 kg).^[1]

The standard day, sea level, no wind, take off with a 200 hp (149 kW) engine is 450 ft (137 m) and the landing roll is 500 ft (152 m).^[1]

The manufacturer estimated the construction time from the supplied kit as 1200 hours.^[1]

Operational history

In March 2014 six examples wereregisteredin the United States with theFederal Aviation Administration,although a total of 12 had been registered at one time. Also in March 2014 two were registered in Canada withTransport Canada.^[2]^[3]

Variants

Ultimate 10-180: Model powered by the 180 hp (134 kW)Lycoming O-360powerplant
Ultimate 10-200: Model powered by the 200 hp (149 kW)Lycoming IO-360powerplant
Ultimate 10-300: Model powered by the 300 hp (224 kW)Lycoming IO-540powerplant

Specifications (Ultimate 10-200)

Data fromAeroCrafter^[1]

General characteristics

Crew:one
Length:16 ft 6 in (5.03 m)
Wingspan:16 ft 0 in (4.88 m)
Empty weight:925 lb (420 kg)
Gross weight:1,350 lb (612 kg)
Fuel capacity:22 U.S. gallons (83 L; 18 imp gal)
Powerplant:1 ×Lycoming IO-360four cylinder, air-cooled,four stroke aircraft engine,200 hp (150 kW)
Propellers:3-bladedconstant speed propeller

Performance

Maximum speed:220 mph (350 km/h, 190 kn)
Cruise speed:170 mph (270 km/h, 150 kn)
Stall speed:60 mph (97 km/h, 52 kn)
Range:500 mi (800 km, 430 nmi)
Rate of climb:2,000 ft/min (10 m/s)

References

^^a ^b ^c ^d ^e ^f ^gPurdy, Don:AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition,page 264. BAI Communications, 15 July 1998.ISBN 0-9636409-4-1
^Federal Aviation Administration(15 March 2014)."Make / Model Inquiry Results".Retrieved15 March2014.
^Transport Canada(15 March 2014)."Canadian Civil Aircraft Register".Archived fromthe originalon 18 July 2011.Retrieved15 March2014.

External links

Photo of an Ultimate 10-200

[Aerocrafter-1] ^^a ^b ^c ^d ^e ^f ^gPurdy, Don:AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition,page 264. BAI Communications, 15 July 1998.ISBN 0-9636409-4-1

[FAAReg-2] Federal Aviation Administration(15 March 2014)."Make / Model Inquiry Results".Retrieved15 March2014.

[TCCAR-3] Transport Canada(15 March 2014)."Canadian Civil Aircraft Register".Archived fromthe originalon 18 July 2011.Retrieved15 March2014.

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