Harman Patil (Editor)

Ullmann 2000 Panther

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Top speed
  
463 km/h

Length
  
7.87 m

Wingspan
  
10 m

Manufacturer
  
Ullmann Aircraft Company

The Ullmann 2000 Panther is an American four-seat high-wing cabin monoplane designed by Ullmann Aircraft Company of Wichita, Kansas to be sold as kits for Amateur construction.

Contents

Design and development

The design of the Panther began in 1997 with construction of the prototype starting in Jun 1998, this prototype registered N202KT first flew on 29 March 2003. The Panther is a high-wing cantilever monoplane with an all-metal wing and a steel-tube fuselage covered with aluminum sheet. The prototype is powered by a 300 hp (224 kW) Continental IO-550-L engine driving a three-bladed constant-speed tractor propeller. The Panther has a tricycle landing gear and an enclosed cabin for a pilot and three passengers, side-by-side in two rows, access by split doors on each side of the fuselage and a small baggage door.

Specifications (Prototype)

Data from Jane's All the World's Aircraft 2003-2004

General characteristics

  • Crew: 1
  • Capacity: 3 passengers
  • Length: 25 ft 10 in (7.87 m)
  • Wingspan: 34 ft 3 in (10.44 m)
  • Height: 9 ft 6 in (2.90 m)
  • Wing area: 130.0 ft2 (12.08 m2)
  • Empty weight: 2040 lb (925 kg)
  • Gross weight: 3050 lb (1383 kg)
  • Powerplant: 1 × Continental IO-550-L, 300 hp (224 kW)

    • Performance

  • Maximum speed: 287 mph (463 km/h)
  • Cruise speed: 230 mph (370 km/h)
  • Stall speed: 68 mph (110 km/h)
  • Range: 1412 miles (2272 km)
  • G limits: +3.8/-1.52

    • References

    Ullmann 2000 Panther Wikipedia
    (Text) CC BY-SA