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Piper PA-16 Clipper

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A Piper PA-16 Clipper seen at Sun n Fun 2006
File:Pa16clipper.jpg
Piper PA-16 Clipper

The Piper PA-16 Clipper is an extended fuselage model of the PA-15 Vagabond. Both models were designed in 1947 for the same reason - Piper Aircraft found itself in dire financial straits and needed to create new, competitive models using existing parts and tooling. The result was the Vagabond, essentially a side-by-side version of the tandem J-3 Cub that is credited with saving the company! [1]

The PA-16 Clipper is a stretched and refined version of the Vagabond intended to seat four people (or "two-and-a-half to three" as often told by Clipper pilots). It is equipped with an extra wing tank, added doors to accommodate the new seating, and a Lycoming O-235, the same engine that would later power the Cessna 152 and the PA-22-108 Colt, itself essentially a Vagabond with a nosewheel. The PA-16 Clipper retained the control sticks that had up to that point been common in aircraft derived from the "Cub" family.

In 1949, the Clipper sold for $2995. The average four place airplane on the market at that time cost over $5000. Fewer than 800 Clippers were built in the one year of production before Piper changed to the Piper PA-20 Pacer.

Pan Am Airlines, who traditionally called its famous luxury airliners "Clippers", took offense at Piper using the name for their light aircraft. As a result of this pressure Piper further refined the model, adding wing flaps, further fuel tanks and replaced the control sticks with yokes. A more powerful Lycoming O-320 150 hp engine was installed and this model became the Piper PA-20 Pacer.[2]

Aircraft Specifications

General characteristics

  • Crew: one, pilot
  • Capacity: 3 passengers
  • Length: 20 ft 1 in (6.12 m)
  • Wingspan: 29 ft 3 in (8.92 m)
  • Height: 6 ft 2 in (1.88 m)
  • Empty: 850 lb (385.56 kg)
  • Maximum takeoff: 1,650 lb (748.42 kg)
  • Powerplant: 1x Lycoming O-235, 115 hp (85.79 kW) (108 hp - 80.57 kW - with cruise pitch propellor)
  • Fuel: 12 gal (45.42 l) in cowl tank and 18 gal (68.14 l) in wing tank (many converted to two 18 gal - 68.14 l - wing tanks)

Performance

  • Maximum crusing speed: 117 mph (188 km/h)
  • Never exceed speed: 140 mph (225 km/h)
  • Cruise speed: 112 mph (180 km/h)
  • Stall speed: 50 mph (80 km/h)
  • Rate of climb: 580 ft/min (176.78 m/min)

Related Content

Similar Aircraft

Designation Sequence

PA-11 - PA-12 - PA-14 - PA-15 - PA-16 - PA-17 - PA-18 - PA-19 - PA20


References