Vehicle

Grumman Gulfstream II

General Aviation and Light Aircraft

The Gulfstream II is a twin-engine, swept-wing business jet designed and first built by Grumman, and later marketed under the Grumman American and Gulfstream American names. It followed the turboprop Gulfstream I and is powered by two aft-mounted Rolls-Royce Spey turbofans, chosen for high speed and long range without giving up airport performance. The first prototype flew from Bethpage on 2 October 1966 on a 52-minute maiden flight. Aircraft were built as green aircraft and delivered to a completion centre for their interiors and avionics, and production ended at Savannah in December 1979. The Gulfstream III succeeded it.

Facts
Year
1966 1
Engine Class
Jet 1
Status
Out of production 1
Maximum Mass (kg)
30,935 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Grumman Gulfstream II (Wikipedia)

Of Make

Source Grumman Gulfstream II (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Grumman Gulfstream II (Wikipedia)Lead sentence
Quote, Lead sentence
The Gulfstream II (G-II) is an American twin engine business jet designed and first built by Grumman, then Grumman American and finally Gulfstream American.

Originated In

Also in Geography Atlas: where this subject originated.

Source Grumman Gulfstream II (Wikipedia)Lead sentence, country
Quote, Lead sentence, country
The Gulfstream II (G-II) is an American twin engine business jet designed and first built by Grumman, then Grumman American and finally Gulfstream American.
Sources
1. Grumman Gulfstream II (Wikipedia)
  • Lead sentence, country
    The Gulfstream II (G-II) is an American twin engine business jet designed and first built by Grumman, then Grumman American and finally Gulfstream American.
  • Lead, first flight
    The first Gulfstream II flew on October 2, 1966.
  • Production, end of production
    Production of the Gulfstream II ended at Savannah in December 1979.
  • Design, engines
    powered by two Rolls-Royce Spey turbofan engines
  • Specifications (Gulfstream II-B), maximum takeoff weight
    Max takeoff weight: 68,200 lb (30,935 kg)
  • Of Make: Grumman, Lead sentence
    The Gulfstream II (G-II) is an American twin engine business jet designed and first built by Grumman, then Grumman American and finally Gulfstream American.
  • Exemplifies: Aviation, Lead sentence
    The Gulfstream II (G-II) is an American twin engine business jet designed and first built by Grumman, then Grumman American and finally Gulfstream American.
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