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Grumman Gulfstream I

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The Grumman Gulfstream I is a twin-turboprop business aircraft. It first flew on August 14, 1958. The G-I is a low-wing monoplane powered by two Rolls-Royce Dart turboprops with four-bladed constant speed propellers. The Gulfstream I has a retractable tricycle landing gear, with twin wheels on the two main units and the nose gear. The cabin is designed to take up to twenty-four passengers in a high-density arrangement or only eight in an executive layout, although ten to twelve was more usual. The aircraft has a hydraulically operated airstair in the forward cabin for entry and exit.

General Characteristics

  • Successors 1 airplane(s)
  • Created On Windows
  • Wingspan 54.1ft (16.5m)
  • Length 43.9ft (13.4m)
  • Height 15.7ft (4.8m)
  • Empty Weight 2,976lbs (1,350kg)
  • Loaded Weight 9,237lbs (4,189kg)

Performance

  • Horse Power/Weight Ratio 0.216
  • Wing Loading 37.0lbs/ft2 (180.8kg/m2)
  • Wing Area 249.4ft2 (23.2m2)
  • Drag Points 6339

Parts

  • Number of Parts 54
  • Control Surfaces 5
  • Performance Cost 368