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Gulfstream III

General Aviation and Light Aircraft

The Gulfstream III is a twin-engine business jet built by Gulfstream Aerospace at Savannah, Georgia, as an improved development of the Grumman Gulfstream II. Its designers kept the Gulfstream II wing box and trailing edge surfaces but gave it a new wing with about six feet more span, five-foot winglets, a longer leading edge, a fuselage two feet longer aft of the main door, a longer radome and a new curved windshield. Two Rolls-Royce Spey turbofans power it, and the FAA type certificate was issued on 22 September 1980. A total of 202 were built, the last in 1986, and the United States armed forces flew military versions as the C-20A to C-20E. The Gulfstream III was also the first business jet designed to fly over both poles.

Facts
Year
1980 2
Engine Class
Turbofan 1
Status
Out of production 1
Units Built
202 1
Top Speed (km/h)
928 1
Mass (kg)
17,237 1
Maximum Mass (kg)
31,615 1
Comparison
Body Style
Light Business Jet 1
Connections

Exemplifies

Aviation, Modes
Source Gulfstream III (Wikipedia)

Of Make

Source Gulfstream III (Wikipedia)
In the Other Atlases

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Gulfstream III (Wikipedia)Lead
Quote, Lead
a business jet produced by Gulfstream Aerospace

Originated In

Also in Geography Atlas: where this subject originated.

Source Gulfstream III (Wikipedia)Design and development
Quote, Design and development
built at Savannah, Georgia, in the United States
Sources
1. Gulfstream III (Wikipedia)
  • Lead
    a business jet produced by Gulfstream Aerospace
  • Variants, civil
    powered by two Rolls-Royce Spey turbofan engines
  • Design and development, last built
    A total of 202 Gulfstream IIIs were built, with the last example built in 1986.
  • Design and development, units built
    A total of 202 Gulfstream IIIs were built, with the last example built in 1986.
  • Specifications
    Maximum speed: 501 kn (577 mph, 928 km/h) (max cruise)
  • Specifications, empty weight
    Empty weight: 38,000 lb (17,237 kg)
  • Specifications, takeoff weight
    Max takeoff weight: 69,700 lb (31,615 kg)
  • Design and development
    built at Savannah, Georgia, in the United States
View the Source
2. Gulfstream Aerospace (Wikipedia)
1970s, first delivery
Quote, 1970s, first delivery
The GIII made its first flight in December 1979, with the first delivery in 1980.
View the Source
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