Gulfstream G100 Private Jet Charter
Gulfstream G100 Private Jet Charter Flights and Prices
The Gulfstream G100 is equipped with a cruising speed of 459 mph and is capable of flying much further distances than most of the mid-size class. With a spacious cabin, including a full lavatory and extra baggage capacity, the G100 is able to service seven passengers.
The average hourly rental rate of the Gulfstream G100 is around 3,800 USD per hour.
|Length||55.58 ft||16.94 m|
|Wing Span||54.59 ft||16.64 m|
|Height||19.49 ft||5.94 m|
|Bag. Capacity||64 ft³||2 m³|
|Length||17.09 ft||5.21 m|
|Width||4.76 ft||1.45 m|
|Height||5.58 ft||1.70 m|
|Area||367 ft³||10 m³|
|Charter Rate||3,800 USD/hour||3,800 EUR/hour|
|IFR Range||2,438 nm||4,515 km|
|Cruise Speed||484 KTAS||896 km/h|
|Certified Ceiling||45,000 ft||13,716 m|
|Rate of Climb||1,348 ft/m||411 m/m|
|Takeoff Distance||5,395 ft||1,644 m|
|Landing Distance||2,920 ft||890 m|
|Max Takeoff Weight||24,650 lbs||11,181 kg|
|Max Landing Weight||20,700 lbs||9,389 kg|
|Useful Weight||7,650 lbs||3,470 kg|
|Payload with Full Fuel||800 lbs||363 kg|
More about the Gulfstream G100
In 1999, General Dynamics acquired Gulfstream and in 2001, General Dynamics acquired Galaxy Aerospace Company from Israel Aerospace Industries Ltd. This acquisition included the type certificates for the family of aircraft, which General Dynamics gave to Gulfstream. The Astra SPX, renamed the Gulfstream G100 in September of 2002, first flew in August of 1994.
Production on the Gulfstream G100 started in 2001 and ended in 2006. 21 aircraft have been built so far.
Key Features of the Gulfstream G100
The cabin of the G100 measures 17.1 feet in length, reaches 5.6 feet in height, and stretches a maximum width of 4.8 feet, with a floor width of 3.7 feet. The cabin of the G100 is usually configured to accommodate seven passengers, but can seat as many as nine. Amenities designed into the G100 include power outlets, an enclosed lavatory, and a galley. If the G100 is fitted with an extension fuel tank, this private business jet offers 42 cubic feet of baggage storage capable of accommodating 370 pounds of luggage. Without this fuel tank extension, this storage capacity increases to 55 cubic feet. With a maximum pressure differential of 8.8 psi, the G100 is capable of maintaining sea level cabin conditions at an altitude of 23,000 feet.
Capabilities of the Gulfstream G100
The G100 comes equipped with two Honeywell TFE731-40R-200F FADEC equipped turbofan engines. Each engine is rated for 4,250 pounds of thrust at sea level. Noise levels on takeoff are 79.1 EPNdB. With these engines, the G100 needs 5,395 feet of runway to take off at sea level on a standard day. At an airport with a 5,000 foot elevation and a temperature of 25 degrees Celsius, this take off distance increases to 8,700 feet of runway. With four passengers on board, the G100 requires only 2,520 feet of runway to land. This private business jet is capable of climbing to an altitude of 37,000 feet in just sixteen minutes and features a maximum certificated ceiling of 45,000 feet. The G100 features an impressive range of 2,950 nautical miles, easily capable of flying transcontinental flights. If your business venture takes you to a more distant location, the G100 is capable of maintaining an airspeed of 430 knots at an altitude of 43,000 feet with a fuel flow rate of 1,144 gallons per hour in a long range cruise configuration. For a swifter flight, the G100 is capable of maintaining an airspeed of 470 knots at an altitude of 41,000 feet with a fuel flow rate of 1,432 gallons per hour in a long range cruise configuration.
The G100 comes standard with a Collins Pro Line 4 avionics suite. This avionics system utilizes four 7.25 by 7.25 inch liquid crystal displays in a T arrangement. Designed to be as efficient as possible, systems are grouped by function with the display screens in close proximity to the functions they control. Some of the avionics systems incorporated into this suite include a Collins TWR-850 Doppler weather radar, an Allied Signal GNS-XES Flight Management System (FMS), and a dual channel Integrated Avionics Processor System (IAPS).
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