PlaneSpottingWorld welcomes all new members! Please gives your ideas at the Terminal.

Cessna 441

From PlaneSpottingWorld, for aviation fans everywhere

The Cessna 441 Conquest II was the first turboprop designed by Cessna and was meant to fill the gap between their jets and piston-engined aircraft. It was developed in November 1974, with the first aircraft delivered in September 1977. It is a pressurized, turbine development of the Cessna 404.

Cessna 441 Conquest - C441 - N6860C - NASA chase plane photographed at Cambridge Bay airport 17th June 2005 01:02 MDT (07:02 UTC).

The Conquest is powered by two Garrett TPE331 turboprops powering two four-bladed McCauley propellers. A 441 with Pratt & Whitney Canada PT6A-112 turboprops was flown in 1986 but did not enter production. The aircraft has retractable tricycle landing gear and on takeoff has a ground roll of 1,785 ft (544 m).

The ICAO designator for the Cessna Conquest as used in flight plans is C441.

A smaller aircraft was marketed as the Cessna 425 Conquest I, itself a turbine development of the Cessna 421.

Specifications (Standard 441)

General characteristics

  • Crew: one or two pilots
  • Capacity: 8-10 passengers
  • Length: 39 ft 0 in (11.89 m)
  • Wingspan: 49 ft 4 in (15.04 m)
  • Height: 13 ft 2 in (4.01 m)
  • Wing area: 253 ft² (23.5 m&sup2)
  • Empty: 5,488 lb (2,489 kg)
  • Loaded: lb ( kg)
  • Maximum takeoff: 9,856 lb (4,470 kg)
  • Powerplant:Garrett TPE331 turboprops, 636 shp (474 kW) each

Performance

  • Maximum speed: 339 mph (545 km/h)
  • Range: 1,291 miles (2,077 km)
  • Cruise: 285 mph
  • Service ceiling: 35,000 ft (10,668 m)
  • Rate of climb: 2,435 ft/min (742 m/minmpm)
  • Wing loading: lb/ft² ( kg/m²)
  • Power/mass: hp/lb ( kW/kg)

External links

Related content

Comparable aircraft

See also

de:Cessna 441