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  2. Cessna 421 Golden Eagle - Wikipedia

    en.wikipedia.org/wiki/Cessna_421_Golden_Eagle

    Cessna 421B Golden Eagle with aftermarket RAM-modified engines A Cessna 421B Golden Eagle, front view A Cessna 421B Golden Eagle 1982 Cessna 421C 421 Type approved 1 May 1967, powered by two Continental GTSIO-520-Ds of 375 hp (280 kW) each, maximum takeoff weight 6,800 lb (3,084 kg).

  3. Cessna 425 - Wikipedia

    en.wikipedia.org/wiki/Cessna_425

    The 425 was introduced in 1980 and was a derivation of the Cessna 421, powered by two 450 hp (336 kW) Pratt & Whitney PT6 engines. In comparison to the King Air C90, "the result was an $875,000 pressurized twin-turboprop that could fly 15 knots to 20 knots faster than the C90, cruise 250 miles farther with four passengers aboard and burn 15 ...

  4. Cessna 402 - Wikipedia

    en.wikipedia.org/wiki/Cessna_402

    The Cessna 401 and 402 are a series of 6 to 10 seat, ... (3,110 kg), creating a much more useful airplane. Fuel capacity was increased to 213 US gallons (810 L). Even ...

  5. 3 dead after small plane crashes into town homes in Oregon ...

    www.aol.com/news/small-plane-crashes-residential...

    Three people are confirmed dead after a small plane crashed into a row of town houses and sparked a massive fire Saturday in Fairview, Oregon.

  6. Continental IO-520 - Wikipedia

    en.wikipedia.org/wiki/Continental_IO-520-F

    The IO-520 series engines normally produce 285 to 310 horsepower (210 to 230 kW) and are used in numerous aircraft such as certain models of the Bellanca Viking 300 and Super Viking, the Beech Bonanza and Baron, and Cessna 185- 206-, 210-, 310-, and 400-series aircraft. The IO-520 remained in production in 2019.

  7. Cessna 414 - Wikipedia

    en.wikipedia.org/wiki/Cessna_414

    The pressurized 414 was developed to appeal to owners of unpressurized, twin-engined aircraft, and was based on the fuselage of the Cessna 421 and used the wing design of the Cessna 401. The 414 is a low-wing cantilever monoplane with a conventional tail unit and a retractable tricycle landing gear.

  8. File:Cessna 421C Golden Eagle, Arctic Air AN1811454.jpg

    en.wikipedia.org/wiki/File:Cessna_421C_Golden...

    Permission is granted to copy, distribute and/or modify this document under the terms of the GNU Free Documentation License, Version 1.2 only as published by the Free Software Foundation; with no Invariant Sections, no Front-Cover Texts, and no Back-Cover Texts.

  9. Cessna Citation Mustang - Wikipedia

    en.wikipedia.org/wiki/Cessna_Citation_Mustang

    Cessna Citation Mustang instrument panel A Mustang PW615F engine uncowled. Data from Cessna Aircraft Company [14] General characteristics. Crew: one or two pilots; Capacity: 4 to 5 passengers and 3130 lb (1420 kg) useful load; Length: 40 ft 7 in (12.37 m) Wingspan: 43 ft 2 in (13.16 m) Height: 13 ft 5 in (4.09 m) Empty weight: 5,600 lb (2,540 kg)