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Gulfstream GVSP Private Jet Charter

The Gulfstream GVSP boasts notable improvements over its predecessor, including a new and advanced wing design that has been optimized for speed.

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Gulfstream GVSPprivate jet charter

Get a quick Gulfstream GVSP Charter Price Estimate

Gulfstream GVSP Private Jet Charter Flights and Prices

The Gulfstream GVSP boasts notable improvements over its predecessor, including a new and advanced wing design that has been optimized for speed.

The average hourly rental rate of the Gulfstream GVSP is around 8,100 USD per hour.

Aircraft Size

Aircraft size English Metric
Length 96.46 ft 29.4 m
Wing Span 93.5 ft 28.5 m
Height 25.82 ft 7.86 m
Bag. Capacity 226 ft³ 6.4 m³

Cabin Size

Cabin size English Metric
Length 43.94 ft 13.4 m
Width 7.32 ft 2.24 m
Height 6.18 ft 1.88 m
Area 1669 ft³ 47.26 m³

Aircraft Seats

Layout Seats
Max Seating 15
Typical Seating 15
Pilots 2

Average Prices

Purchase New - -
Purchase Used - -
Hourly rate 8,100 USD/hour 8,100 EUR/hour

Performance Specifications

Performance English Metric
IFR Range 6750 nm 12501 km
Cruise Speed 508 KTAS 941 km/h
Certified Ceiling 51000 ft 15545 m
Rate of Climb 3610 ft/m 1100 m/m
Takeoff Distance 5910 ft 1801 m
Landing Distance 2770 ft 844 m
Max Takeoff Weight 91000 lbs 41277 kg
Max Landing Weight 75300 lbs 34156 kg
Useful Weight 36500 lbs 16556 kg
Payload with Full Fuel 1800 lbs 816 kg

More about the Gulfstream GVSP

The original inspiration for the Gulfstream GV-SP can be traced to the original late 1950’s Grumman Gulfstream I turboprop aircraft. However, with the upgrades implemented in this model, the original design is hard to detect, with the fuselage cross section being the only discernable feature retained from the original design. The straight wing design and turboprop engines utilized on the G1 were replaced with swept wings and turbofan engines, allowing the Gulfstream GV-SP to fill the market need for a intercontinental, large executive aircraft.


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Key Features of the Gulfstream GVSP

The Gulfstream GV-SP is capable of comfortably accommodating nineteen passengers while still allowing for a crew of up to four. However, the cabin is usually arranged to accommodate eight to ten passengers while featuring amenities such as a full lavatory with shower, a crew rest area, a conference or dining room, and work stations. The cabin of the Gulfstream GV-SP measure 43.93 feet in length, reaches 6.2 feet in height, and stretches 5.5 feet in width with a maximum width of 7.3 feet. This private business jet offers 226 cubic feet of luggage capacity capable of accommodating 2,500 pounds of baggage. With a cabin pressure differential of 10.2 psi, the GV-SP is capable of maintaining a sea level cabin altitude while flying at an altitude of 29,200 feet.

Capabilities of the Gulfstream GVSP

The Gulfstream GV-SP comes equipped with two Rolls-Royce BR-710A engines. Each engine is capable of producing 15,385 pounds of thrust at 15 degrees Celsius. With these powerful engines, the GV-SP needs 5,960 feet of runway to take off on a standard day. To land, this private business jet requires only 2,200 feet of runway with four passengers on board. The GV-SP features an intercontinental range of 6,750 nautical miles and has a maximum certificated service ceiling of 51,000 feet. The Gulfstream GV-SP is capable of climbing to an altitude of 37,000 feet in just 18 minutes. For a flight to a more distant destination, the GV-SP is capable of maintaining an airspeed of 459 knots at an altitude of 45,000 feet in a long range cruise configuration. For a swifter flight, this private business jet is capable of maintaining an airspeed of 488 knots at an altitude of 43,000 feet in a high-speed cruise configuration.

The avionics system selected for the GV-SP is the Honeywell SPZ-8500 system, which is a combination of select Primus 2000 equipment and the SPZ-8000 system. Six large-format cathode ray tube (CRT) displays have been incorporated into the design. Included in the avionics systems are triple Laseref III inertial reference systems, two flight management systems (FMSs) with provisions for an additional FMS, dual Mode S transponders, triple digital air data computers (ADCs), a Primus 880 weather radar, an automatic direction finder (ADF), dual Collins VHF comm and nav radios with distance measuring equipment (DME), high frequency (HF) transceivers, and radio altimeters. This system also offers the option to include a heads up display (HUD) system with Enhanced Vision System (EVS) system capability.

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