GULFSTREAM III Civil Aircraft Model Details

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General Information of GULFSTREAM III

Developed From : Grumman Gulfstream II

First Flight : 2 December 1979[1]

Introduction : 1980

Manufacturer : Gulfstream Aerospace

Number Built : 202

Primary Users : United States; Gabon; India; Italy

Produced : 1979–1986

Role : Business jet

Unit_Cost : US$37M

Variants : Gulfstream IV/G400/G450

General characteristics of GULFSTREAM III

Aspect Ratio : 6.0:1

Capacity : 19 passengers (standard seating)

Crew : Two or three

Empty Weight : 38,000 lb (17,236 kg)

Height : 24 ft 4½ in (7.43 m)

Length : 83 ft 1 in (25.32 m)

Max Takeoff Weight : 69,700 lb (31,615 kg)

Powerplant : 2 × Rolls-Royce Spey RB.163 Mk 511-8 Turbofan, 11,400 lbf (50.7 kN) each

Wing Area : 934.6 sq ft (86.83 m²)

Wingspan : 77 ft 10 in (23.72 m)

Performance of GULFSTREAM III

Cruise Speed : 508 mph (442 knots, 818 km/h) (long range cruise)

Maximum Speed : 576 mph (501 knots, 928 km/h) (max cruise)

Range : 4,200 mi (3,650nmi, 6,760 km) (eight passengers, IFR reserves)

Rate Of Climb : 3,800 ft/min (19.3 m/s)

Service Ceiling : 45,000 ft (13,716 m)

Stall Speed : 121 mph (105 knots, 194 km/h)

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