G280 Aircraft - The Gulfstream G280 is a twin-engine jetliner built by Israel Aerospace Industries (IAI) for Gulfstream Aerospace. It started shipping to customers in 2012.
In 2005, Gulfstream and IAI designed a follow-on aircraft for the Gulfstream G200. A new model called the G250 was launched in 2008. Planned improvements include a new glass pilot and gins; Larger wings and heated fronts are included.
G280 Aircraft
The company changed the name to G280 in July 2011, stating that "G280 is a more friendly number than G250 in some cultures."
Gulfstream G280 Recently Sold
After the flight test program; The G280 demonstrated a range of 3,600 nmi (6,667 km) at Mach 0.80 with four passengers and NBAA IFR backup in 2011. It can fly from London to New York or Singapore in Dubai. Its fairway length has been reduced from the G200's 4,960 feet (1,512 m) to 4,750 feet (1,448 m).
In July 2012, the United States' FAA issued a report with conditions to ensure that there were no security gaps in the G280's electronic systems.
Aerodynamic design and interior design of its wing and empnage were carried out by Gulfstream. Detailed design was carried out by IAI for Gulfstream's requirements.
There were several improvements to the aircraft, among them increased interior length (the external dimensions of the fuselage remained unchanged, the rear fuselage fuel tank was removed to make use of 17 inches (43 cm) of internal area).
Gulfstream G280 Gets Garmin Ads B Solution
It includes the new HTF7250G gen. new T-tail (with greater horizontal and vertical stabilizers); ice wings supported by gine bleed air; The cabin has four additional windows and access to the luggage compartment. Compete against the Bombardier Challenger 300 and the Cessna Citation X+. fuselage The empnage and landing gear are manufactured by Spirit AeroSystems (now part of the Triumph Group) and the wing IAI.
) and the aircraft is assembled in Israel. Dallas for interior and painting; Shipping to Texas.
Its wing is a new design using the Gulfstream G550 airfoil and has a larger area of 495 ft² versus the G200's 369 ft². This would allow the business jet to climb directly to an altitude of 43,000 feet (13,000 meters). Design cruise for the new airfoil is Mach 0.80 and Mach 0.75 for the G200 wing.
Flying at an altitude of 41,000 ft (12,000 m) and Mach 0.82 (467 kn or 865 km/h), each engine burns 900 lb (410 kg) of fuel per hour.
Pilot Report: Gulfstream G280
[1] Under license from Fouga. [2] Joint venture with RUAG. [3] Common car with Rafael. [4] Joint venture with DRDO. [5] Joint venture with Boeing.
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