GULFSTREAM G550 Civil Aircraft Model Details

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General Information of GULFSTREAM G550

Developed From : Gulfstream V

Introduction : 2004

Manufacturer : Gulfstream Aerospace

National Origin : United States

Number Built : 300+[1]

Primary Users : United States Air Force; United States Navy; Israeli Air Force; Netjets

Produced : 2003–present

Role : Business jet

Status : In service

Unit_Cost : G500: US$42 million (2010)[2]; G550: US$53.5 million (2011)[3]

General characteristics of GULFSTREAM G550

Capacity : 14–19 passengers

Crew : 2 pilots, 0–2 attendants

Empty Weight : 48,300 lb (21,900 kg)

Height : 25 ft 10 in (7.9 m)

Length : 96 ft 5 in (29.4 m)

Loaded_Weight : 54,500 lb (24,700 kg)

Max Takeoff Weight : 91,000 lb (41,300 kg)

Maximum Landing Weight : 75,300 lb (34,200 kg)

Powerplant : 2 × Rolls-Royce BR710 turbofan, 15,385 lbf (68.44 kN) each

Useful Load : 6,200 lb (2,800 kg)

Wingspan : 93 ft 6 in (28.5 m)

Performance of GULFSTREAM G550

Cruise Speed : 488 knots (562 mph, 0.85 Mach, 904 km/h)

Maximum Speed : 0.885 Mach (585 mph, 941 km/h)

Range : 6,750 nmi (7,768 miles, 12,500 km)

Service Ceiling : 51,000 ft (15,500 m)

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