Английская Википедия:Cessna 441 Conquest II
Шаблон:Short description Шаблон:Use mdy dates Шаблон:Use American English
The Cessna 441 Conquest II is the first turboprop powered aircraft 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, 8–9 passenger turbine development of the Cessna 404 Titan.
Development
The original design from 1972 for this aircraft was known as the Model 435 and was to be powered by Continental GTSIO-520X engines with three-bladed propellers. By 1975, the designed evolved into the turboprop-powered Model 441.[1] It was certified by the FAA on August 19, 1977.[2] Cessna renamed the Model 441 the Conquest II in 1983. 1984 models starting with constructor number 195 used lighter-weight, four-bladed McCauley propellers.[1] A 441 with Pratt & Whitney Canada PT6A-112 turboprops was flown in 1986, but did not enter production. A smaller aircraft was marketed as the Cessna 425 Conquest I, itself a turbine development of the Cessna 421.
In September 2007, Cessna limited the Conquest II to 22,500 hours of air time through a Supplemental Inspection Document. This makes it effectively mandatory for US air carriers but only advisory for private operators.[3] Cessna built 362 of the aircraft between 1977 and 1986.[4]
Design
The Cessna 441 cruises at Шаблон:Cvt true airspeed while burning Шаблон:Cvt of fuel per hour at flight level 290 (FL290), or about 29,000 feet. The aircraft's maximum range is Шаблон:Cvt at Шаблон:Cvt TAS and Шаблон:Cvt/h at FL350. With six to nine seats, its Шаблон:Cvt basic operating weight (BOW) allows a Шаблон:Cvt payload at full fuel, but MTOW can be increased by Шаблон:Cvt with aftermarket modifications. Most have been upgraded from twin Garrett TPE331-8s engines to -10s for better climb performance, a ceiling raised to FL350 from FL330, and TBO raised from 3,000 to 5,000h for $225,000 per engine.[4]
Converting from the standard three-blade propellers to smaller diameter Hartzell four-blade propellers results in a climb rate improved by 200 fpm (1.01 m/s) and a Шаблон:Cvt increase in cruise speed as well as reduced cabin noise and improved ground clearance.[5] The aircraft has a retractable tricycle landing gear and has a ground roll of 1,785 ft (544 m) on takeoff. The high aspect ratio wings use bonded construction techniques.[6] The ICAO designator for the Cessna Conquest as used in flight plans is C441.
Operational history
By May 2019, 290 aircraft remained in service, at a $.75-.9M value down from $1-1.9M in 2011. The King Air B200 has a roomier cabin but Шаблон:Cvt less range, a slower cruise and higher fuel burn. The Mitsubishi MU-2B-60 has a similar fuel burn and speed but flies lower. The Piper Cheyenne III is fast but has poorer fuel efficiency and Шаблон:Cvt less range. The Piper Cheyenne 400 is Шаблон:Cvt faster but burns fuel like a light jet.[4]
The Conquest II is operated by corporate owners, air charter operators and previously by the Royal Flying Doctor Service in Australia. Examples of the type have been exported to many countries including Austria, Australia, Canada, Ecuador, Finland, Germany, Iceland, Mexico, Norway, Peru, South Africa, Sweden and the United Kingdom.
Specifications (Conquest II)
See also
References
External links
Шаблон:Cessna 310 family Шаблон:Cessna
- ↑ 1,0 1,1 Phillips, Edward H.: Wings of Cessna, Model 120 to the Citation III, Flying Books, 1986. Шаблон:ISBN
- ↑ Шаблон:Cite web
- ↑ Шаблон:Cite news
- ↑ 4,0 4,1 4,2 Шаблон:Cite news
- ↑ Шаблон:Cite news
- ↑ Шаблон:Cite journal
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