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The Hawk GafHawk ("General Aviation Freighter") was a small, turboprop-powered freighter aircraft developed in the United States in the 1980s but which only flew in prototype form. It was designed by as a means of transporting drilling equipment in and out of remote locations, and was designed to be simple, rugged, and have good STOL and rough-field performance. The resulting design was a boxy aircraft with a rectangular-section fuselage with a high-set tail and rear loading ramp. The high aspect-ratio wings were high-set and braced with struts. The landing gear was fixed and of tricycle configuration, with the main units having dual wheels.

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  • Hawk GAFHawk (en)
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  • The Hawk GafHawk ("General Aviation Freighter") was a small, turboprop-powered freighter aircraft developed in the United States in the 1980s but which only flew in prototype form. It was designed by as a means of transporting drilling equipment in and out of remote locations, and was designed to be simple, rugged, and have good STOL and rough-field performance. The resulting design was a boxy aircraft with a rectangular-section fuselage with a high-set tail and rear loading ramp. The high aspect-ratio wings were high-set and braced with struts. The landing gear was fixed and of tricycle configuration, with the main units having dual wheels. (en)
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span ft
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stall speed mph
stall speed note
  • (en)
wing area sqft
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  • imp (en)
first flight
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  • United States (en)
crew
  • Two pilots (en)
height ft
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ref
  • Jane's All the World's Aircraft 1988–89 (en)
type
  • Freighter (en)
has abstract
  • The Hawk GafHawk ("General Aviation Freighter") was a small, turboprop-powered freighter aircraft developed in the United States in the 1980s but which only flew in prototype form. It was designed by as a means of transporting drilling equipment in and out of remote locations, and was designed to be simple, rugged, and have good STOL and rough-field performance. The resulting design was a boxy aircraft with a rectangular-section fuselage with a high-set tail and rear loading ramp. The high aspect-ratio wings were high-set and braced with struts. The landing gear was fixed and of tricycle configuration, with the main units having dual wheels. Certification proved elusive, however, and Hawk eventually abandoned the project without building any other examples. (en)
aspect ratio
ceiling ft
climb rate ftmin
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  • at sea level (en)
cruise speed mph
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empty weight lb
eng1 hp
eng1 name
  • Pratt & Whitney Canada PT6A-65B/R (en)
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gross weight lb
length in
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  • *Take-off run to 50 ft : *Landing run from 50 ft : (en)
number built
range miles
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  • with maximum fuel (en)
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number built
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