Model
Gulfstream 250 G250
Manufacturer
Gulfstream Aero
Equipped Price
$ 24,000,000
Pax Exec
10
Description
The G250 was launched by Gulfstream in 2008. The G250 is a derivative of the G200, with many improvements, among them increased cabin length, new engine HTF7250G, new T-tail, wing bleed anti-ice, cabin with 4 more windows and access from it to the baggage compartment. It will compete against the Hawker 4000, Bombardier Challenger 300 and the planned Embraer Legacy 500. The fuselage, empenage and landing gear will be manufactured by IAI, the wing by Spirit AeroSystems, while the final assembly will be performed by Gulfstream. The first G250 has its maiden flight on December 11, 2009 from Tel Aviv, Israel. The second G250 first flew on March 25, 2010. With this flight, the two G250s have completed over 72 hours of flight testing. The G250 is planned to receive type certification in 2011, then enter service shortly afterwards.
Relative to Competitors in Class
Performance Stats
| Noise (db) | NA/NA/NA |
| Exterior Length (ft) | 66.8 |
| Exterior Height (ft) | 21.3 |
| Exterior Wingspan (ft) | 63 |
| Cabin Length Net (ft) | 25.8 |
| Cabin Height (ft) | 6.3 |
| Cabin Width Max (ft) | 7.2 |
| Engines | 2 Hon HTF7250G |
| Output (lbs) | 7,445 |
| Inspection Interval (hours) | OC |
| Max Takeoff Weight (lbs) | 39,600 |
| Max Payload (lbs) | 4,050 |
| Useful Load (lbs) | 15,600 |
| Executive Payload (lbs) | 2,000 |
| Available Payload with Max Fuel (lbs) | 1,000 |
| Take Off Distance - Sea Level/ISA (ft) | 4,960 |
| Take Off Distance - 5000ft /25degs (ft) | 0 |
| Max Certificated Altitude (ft) | 45,000 |
| High Speed - True Airspeed (kts) | NA |
| Max Payload Range - (NM) | 0 |
| Max Fuel Range - (NM) | 0 |
| 600nm Trip Flight Time | 1+26 |
| 600nm Trip Fuel Used | 2,531 |
| 1000nm Trip Flight Time | 2+19 |
| 1000nm Trip Fuel Used | 3,830 |