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Charter, Buy or Lease a G200

The Gulfstream 200, featuring impressive cruise speed and range, is especially notable for its comfort-level. With the tallest and widest cabin in its class, at 6'3 cabin height and 7'1 cabin width, the Gulfstream 200 is equipped with a fully heated and pressurized baggage compartment, along with a roomy refreshment center.

Aircraft Size

G200 Exterior
Aircraft Size English Metric
Length 62.24 ft 18.97 m
Wing Span 58.07 ft 17.70 m
Height 21.42 ft 6.53 m
Bag. Capacity 150.00 cu³ 004.25 m³

Cabin Size

G200 Interior
Cabin Size English Metric
Length 24.41 ft 7.44 m
Width 7.15 ft 2.18 m
Height 6.27 ft 1.91 m
Area 868.00 ft³ 24.58 m³

Aircraft Seats

Layout Seats
Max Seating 10
Typical Seating 9
Pilots 2

Average Prices

Costs USD EUR
Price - New - -
Price - Used - -
Hourly Rate 5,700 USD 5,700 EUR

Performance Specifications

Performance English Metric
IFR Range 3,312 nm 6,134 km
Cruise Speed 494 KTAS 915 km/h
Certified Ceiling 45,000 ft 13,716 m
Rate of Climb 1,947 ft/m 594 m/m
Takeoff Distance 6,080 ft 1,853 m
Landing Distance 3,280 ft 1,000 m
Max Takeoff Weight 35,450 lbs 16,080 kg
Max Landing Weight 30,000 lbs 13,608 kg
Useful Weight 11,450 lbs 5,194 kg
Payload with Full Fuel 400 lbs 181 kg

More about the G200

Following the acquisition of Gulfstream in 1999, General Dynamics acquired Galaxy Aerospace Company from Israel Aerospace Industries Ltd in 2001. This acquisition included the type certificates for the family of aircraft, which General Dynamics gave to Gulfstream. The Galaxy model was later renamed the Gulfstream G200. With an expansive range, roomy cabin, and high airspeed capabilities, the G200 is formidable even when considered to later Gulfstream aircraft. The airframe of this private business jet was designed with the aid of 3D computer-aided structural analysis programs. Aluminum alloys, titanium, and steel are utilized for much of the main structures, with composite materials for some of the secondary structures.

Key Features of the G200

The cabin of the Gulfstream G200 measures 24.4 feet in length, reaches 6.3 feet in height, and stretches a maximum of 7.2 feet in width with a floor width of 5.7 feet. While typically arranged to accommodate 10 passengers, the cabin of the G200 can be configured to seat from eight to nineteen passengers. With 125 cubic feet of storage capable of accommodating 2,400 pounds of luggage, the G200 offers more than enough space to accommodate any luggage your passengers require. With a maximum pressure differential of 8.8, the G200 is capable of maintaining a sea level cabin altitude at an altitude of 23,000 feet. Sixteen windows surround the cabin, allowing a light environment for productive business or a relaxing view.

Capabilities of the G200

The Gulfstream G200 comes standard with two Pratt & Whitney PW306A engines. These engines, similar to those used on the Learjet 60 and Hawker 1000, are rated at 6,040 pounds of thrust each. As such, these powerful engines allow the G200 to climb to an altitude of 37,000 feet in just 19 minutes. The G200 requires 6,083 feet of runway to take off on a standard day. At an airport with an altitude of 5,000 feet, this requirement increases to 8,804 feet. With four passengers, the G200 needs only 2,590 feet of runway to land. This private business jet features an impressive transoceanic range of 3,400 nautical miles, making the G200 an ideal choice for flights to distant destinations. In a long range cruise configuration, the G200 is capable of flying at an altitude of 41,000 feet and an airspeed of 430 knots. For a swifter flight, the G200 is capable of maintaining an airspeed of 470 knots at an altitude of 37,000 feet.

The avionics suite selected for the G200 is the Collins Pro Line 4 avionics suite. Five screens are utilized in this arrangement, with one main Engine Indicating and Crew Alert System (EICAS) screen in the center surrounded by four smaller screens that display relevant flight and system information. Typical systems included in this package are dual ARINC 429 Pro Line communication, navigation, and identification radios with dual DMEs and ADEs, a WXR-840 weather radar diagnostic computer, a digital autopilot, a Allied Signal GNS-X/EX Flight Management System (FMS), and an attitude and heading reference system.

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