Gulfstream V (GV)

The Gulfstream V (GV) is a landmark in aviation history, recognized as the world’s first purpose-built ultra-long-range business jet. Officially launched in the early 1990s as a direct response to the emerging ultra-long-range market, it performed its first flight on November 28, 1995, and received FAA certification on April 11, 1997. It officially entered service in June 1997, instantly setting a new standard for non-stop intercontinental travel by connecting distant city pairs like New York to Tokyo or London to Buenos Aires.

1. Performance & Range

The GV was engineered to traverse oceans and continents with massive fuel reserves and high-altitude efficiency, allowing it to fly above most commercial traffic and weather.

  • Maximum Range: 6,500 nm (~12,038 km)
  • Maximum Speed: Mach 0.885 (508 ktas / 585 mph)
  • High-Speed Cruise: Mach 0.83 (476 ktas)
  • Typical Cruise Speed: Mach 0.80 (459 ktas)
  • Maximum Operating Altitude: 51,000 ft (15,545 m)
  • Takeoff Distance (MTOW): 6,100 ft (1,859 m)
  • Landing Distance: 3,386 ft (1,032 m)

2. Interior & Cabin Dimensions

The GV features a stretched airframe compared to earlier models, allowing for up to four distinct living areas and a dedicated crew rest area—essential for missions lasting up to 14 hours. It was also the first civil aircraft to introduce the Enhanced Vision System (EVS) for increased safety.

  • Passenger Capacity: 14–19 (typical executive configurations seat 14)
  • Cabin Height: 6.2 ft (1.88 m)
  • Cabin Width: 7.3 ft (2.23 m)
  • Cabin Length: 50.1 ft (15.27 m) — overall interior length
  • Baggage Capacity: 226 cubic feet (fully accessible in-flight)
  • Amenities: Signature large oval windows, full-service forward or aft galley, 100% fresh air ventilation, and low cabin altitude (6,000 ft at cruise)

3. Weights & Capacities

The aircraft’s structural design was specifically optimized to handle the heavy fuel loads required for its 6,500 nm range while maintaining strong takeoff performance.

  • Max Takeoff Weight (MTOW): 90,500 lbs (41,050 kg)
  • Max Landing Weight: 75,300 lbs (34,156 kg)
  • Maximum Payload: 6,600 lbs (2,994 kg)
  • Fuel Capacity: 41,300 lbs (18,733 kg)

4. Technical Systems

  • Engines: 2 × Rolls-Royce BR710A1-10 turbofans
  • Thrust: 14,750 lbf each (29,500 lbf total)
  • Avionics: Honeywell SPX-8500 suite (6-tube EFIS cockpit)
  • Notable Features: Full Authority Digital Engine Control (FADEC) and the first factory-installed Enhanced Vision System (EVS) with Head-Up Display (HUD)

The Gulfstream V remains an enduring icon of global mobility. With its historic 6,500-nautical-mile range and a cabin designed to sustain productivity and wellness on ultra-long-haul missions, it is a premier choice for those who value time, comfort, and a world-class travel experience.

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