Aircraft Description

Gulfstream G550 Large Jet for charter

The G550, a variant of the Gulfstream V, initially named Gulfstream V SP, was released to the market in 2003. It has increased performance. Range is increased to 6,750 nautical miles (12,500 km), mostly due to reductions in aerodynamic drag. The Gulfstream 550 has the longest flight range in its class. Additionally, this aircraft has a “PlaneView” cockpit, which consists of 4 Honeywell DU-1310 EFIS screens, a Gulfstream-designed cursor control system, and an Enhanced Vision System (EVS). EVS is an infrared camera that displays an image of the view in front of the camera on a head up display. The system permits the aircraft to land in lower-visibility instrument meteorological conditions than a non-EVS-equipped aircraft. This aircraft may be distinguished from the legacy Gulfstream V by a seventh passenger window on both sides of the aircraft, and by the square outflow valve on the aircraft right side as compared to the circular one on the GV. More than 182 Gulfstream G550 aircraft have been produced as of 2008. The Gulfstream 550 competes against the Airbus Corporate Jet, Boeing Business Jet, and the Bombardier Global Express.

Gulfstream G550 Specifications

PERFORMANCE

Maximum Range:* 6,750 nm / 12,501km (Mach 0.80, 8 passengers, 4 crew and nbaa iFr reserves)

Normal Cruise Speed: Mach 0.80 / 459 ktas / 850 km/h

High Speed Cruise Mach: 0.87 / 500 ktas / 926 km/h

Mmo: (Maximum Operating Mach number) Mach 0.885

Takeoff Distance: (Sl, iSa, MTOW) 5,910 ft / 1,801 m

Landing Distance: (Sl, iSa, MlW) 2,770 ft / 844 m

Initial Cruise Altitude: 41,000 ft / 12,497 m

Maximum Cruise Altitude: 51,000 ft / 15,545 m

WEIGHTS

Maximum Takeoff Weight: 91,000 lb / 41,277 kg

Maximum Landing Weight: 75,300 lb / 34,156 kg

Maximum Zero Fuel Weight: 54,500 lb / 24,721 kg

Basic Operating Weight: (including 4 crew)** 48,300 lb / 21,909 kg

Maximum Payload:** 6,200 lb / 2,812 kg

Payload with Maximum Fuel:** 1,800 lb / 816 kg

Maximum Fuel Weight: 41,300 lb / 18,733 kg

DESIGN STANDARDS

Avionics Gulfstream PlaneView®

Engines Two Rolls-Royce: BR710 C4-11 Rated Takeoff Thrust (each) 15,385 lb / 68.40 kN

Passengers: Typical Outfitting 14 – 18

INTERIOR

Total Interior Length: 50 ft 1 in / 15.27 m

Cabin Length: (excluding baggage) 43 ft 11 in / 13.39 m

Cabin Height: 6 ft 2 in / 1.88 m

Cabin Width: 7 ft 4 in / 2.24 m

Cabin Volume: 1,669 cu ft / 47.26 cu m

Baggage Compartment Volume: 226 cu ft / 6.40 cu m

COMFORT

14 Gulfstream Signature Oval Windows Forward or Aft Galley Forward and Aft Lavatory

12 Select Floorplans or Tailored Floorplan

* NBAA IFR theoretical range. Actual range will be affected by ATC routing, operating 
 speed, weather, outfitting options and other factors.
 ** Stated weights are based on theoretical standard outfitting configurations. Actual 
 weights will be affected by outfitting options and other factors