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Piper PA-32R (John Kennedy Jr Death Plane)
https://en.wikipedia.org/wiki/Piper_PA-32R
The Piper PA-32R is a six-seat, high-performance, single engine, all-metal fixed-wing aircraft produced by Piper Aircraft of Vero Beach, Florida. The design began life as the Piper Lance, a retractable gear version of the Piper Cherokee Six. Later models became known by the designation Piper Saratoga. The primary difference between the Lance and early Saratoga is the development of a tapered wing on the Saratoga, replacing the "Hershey Bar" wing on the Lance that was a carryover from the Cherokee Six. Later Saratoga models provided updated/improved avionics, engine and interior touches but retained the same airframe design. Production of the Saratoga was discontinued in 2009. The Saratoga competed for sales with the Beechcraft Bonanza, Mooney Ovation, Cirrus SR22, Cessna 206 Stationair, and Cessna 350. Until 1972, when the assembly line was destroyed in a flood, the Comanche was Piper's luxury high-performance single. Afterwards, Piper began modifying its heavy lifting single engine PA-32 Cherokee Six, adding retractable landing gear and designating the type as the "PA-32R". For the 2008 model year, the Saratoga II HP (normally aspirated) model was eliminated, along with the 6X and 6XT (fixed-gear versions of the Saratoga), leaving the turbocharged Saratoga II TC as the only production model in the PA-32 line. Role Personal use, air taxi & freight aircraft National origin United States Manufacturer Piper Aircraft First flight 30 August 1974 Introduction 1975 Produced 1975-2009 Developed from Piper Cherokee Six John F. Kennedy Jr., along with his wife, Carolyn Bessette-Kennedy, and sister-in-law Lauren Bessette died on July 16, 1999, when the Saratoga Kennedy was flying crashed into the Atlantic Ocean 7 miles (11 km) off the coast of Martha's Vineyard due to spatial disorientation. Specifications (1972 model PA-32RT-300) General characteristics Crew: One Capacity: five passengers (optional additional seat on some) Length: 27 ft 9 in (8.44 m) Wingspan: 32 ft 10 in (9.99 m) Height: 9 ft 6 in (2.9 m) Wing area: 174.5 ft2 (16.2 m2) Wing profile: NACA 65-415 Empty weight: 2011 lb (912 kg) Gross weight: 3600 lb (1633 kg) Powerplant: 1 × Lycoming IO-540-K1G5, 300 hp (225 kW) Performance Maximum speed: 190 mph (306 km/h) Cruise speed: 160 mph (258 km/h) Range: 1000 miles (1600 km) Service ceiling: 14600 ft (4450 m) Rate of climb: 1050 ft/min (5.3 m/s) * |
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