| ADI Stallion | |
|
HW100 - 45000
UAW55 - 105000 RRW100 - 175000 PKRR - 7500 |
ADI Stallion Stallion Role - Light utility aircraft National origin - United States of America Manufacturer - Aircraft Designs Inc Designer - Martin Hollmann First flight - July 1994 Number built - 7 (2007) The ADI Stallion is a US civil utility aircraft that first flew in July 1994. It is marketed in kit form for homebuilding by Aircraft Designs Inc. Design and development The Stallion is a single-engined high-winged monoplane, with wings based on those of the Lancair ES and a retractable tricycle landing gear from the Lancair IV. It has a steel-tube fuselage center section, with the remainder of the airframe of composite construction, and is designed to be powered by engines of 230-350 hp (172-261 kW). The recommended engine is the 300 hp (224 kW) Continental IO-550, but engines as powerful as the 750 hp (559 kW) Walter M601 have been used. It is available in two versions, the four seat ADI Stallion and the six-seat Super Stallion. Operational history Seven examples had been completed and flown by December 2007. Specifications (ADI Super Stallion - 350 hp engine) Data from Jane's All The World's Aircraft 2003-2004 General characteristics Crew: one pilot Capacity: 5 passengers Length: 25 ft 0 in (7.62 m) Wingspan: 35 ft 0 in (10.67 m) Height: 9 ft 6 in (2.90 m) Wing area: 140.1 sq ft (13.00 m2) Aspect ratio: 8.8:1 Empty weight: 2,200 lb (998 kg) Max takeoff weight: 3,800 lb (1,784 kg) Powerplant: 1 × Continental TSIO-550-B air-cooled turbocharged flat-six engine, 350 hp (224 kW) Performance Maximum speed: 306 mph (493 km/h, 266 kn) Cruise speed: 295 mph (474 km/h, 256 kn) Stall speed: 71 mph (115 km/h, 62 kn) Range: 2,700 mi (4,345 km, 2,346 nmi) Service ceiling: 32,000 ft (9,750 m) Rate of climb: 2,600 ft/min (13.2 m/s) wikipedia.org (en) |