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  2. Pratt & Whitney Canada PT6 - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_Canada_PT6

    The Pratt & Whitney Canada PT6 is a turboprop aircraft engine produced by Pratt & Whitney Canada.Its design was started in 1958, it first ran in February 1960, first flew on 30 May 1961, entered service in 1964, and has been continuously updated since.

  3. Honeywell TPE331 - Wikipedia

    en.wikipedia.org/wiki/Honeywell_TPE331

    The 715 shp TPE331-6 used in the Beech King Air B100 have a 400-hr. fuel nozzle cleaning interval, 1,800-hr. hot section inspection interval and a 5,400-hr. time between overhaul; approval is possible for 3,000-hr. HSIs and 6,000-hr. overhauls and engine reserves are cheaper than for the PT6A.

  4. Pratt & Whitney Canada PT6T - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_Canada_PT6T

    Pratt & Whitney Canada PT6 The Pratt & Whitney Canada PT6T Twin-Pac is a turboshaft engine designed for helicopters. Manufactured by Pratt & Whitney Canada , its first application was in the Bell 212 and UH-1N Twin Huey helicopter family.

  5. Pratt & Whitney Canada PT6A-20 - Wikipedia

    en.wikipedia.org/?title=Pratt_&_Whitney_Canada...

    Retrieved from "https://en.wikipedia.org/w/index.php?title=Pratt_%26_Whitney_Canada_PT6A-20&oldid=514171462"

  6. de Havilland Canada DHC-6 Twin Otter - Wikipedia

    en.wikipedia.org/wiki/De_Havilland_Canada_DHC-6...

    The availability of the 550 shaft horsepower (410 kW) Pratt & Whitney Canada PT6A-20 turboprop in the early 1960s made the concept of a twin feasible. A DHC-3 Otter with its piston engine replaced with two PT6A-4 [3] engines had already flown in 1963. It had been extensively modified for STOL research. [4]

  7. Piper PA-31T Cheyenne - Wikipedia

    en.wikipedia.org/wiki/Piper_PA-31T_Cheyenne

    Data from Jane's All the World's Aircraft 1976–77 General characteristics Crew: 2 Capacity: 4–6 passengers Length: 34 ft 8 in (10.57 m) Wingspan: 42 ft 8 + 1 ⁄ 4 in (13.011 m) (over tip tanks) Height: 12 ft 9 in (3.89 m) Wing area: 229 sq ft (21.3 m 2) Airfoil: NACA 63 2 -415 at root, 63A212 at tip Empty weight: 4,870 lb (2,209 kg) Max takeoff weight: 9,000 lb (4,082 kg) Fuel capacity ...

  8. Biden takes departing jab at Trump, says he was a 'genuine ...

    www.aol.com/news/biden-takes-departing-jab-trump...

    President Biden took a departing jab at Trump, saying that what the president-elect did was a "genuine threat to democracy.". Ahead of the anniversary of the Jan. 6, 2021, riot at the U.S. Capitol ...

  9. Piper PA-42 Cheyenne - Wikipedia

    en.wikipedia.org/wiki/Piper_PA-42_Cheyenne

    The PA-42-1000 Cheyenne IV was certified in 1984, 43 were built until 1991 and 37 remain in service in 2018. [3] Due to its top speed over 351 kn (404 mph; 650 km/h) it was renamed the Cheyenne 400LS when Lear Siegler owned Piper, then the Cheyenne 400. [3] Flat rated to ISA+37, the turboprops maintains its power to almost 20,000 ft (6,100 m).

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