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Fact Files  >  Gulfstream 200, G200

Gulfstream Aerospace - Gulfstream 200, G200
Category: Jet > 20,000 lbs.
Years Aircraft Manufactured: 2001 - current
Printer friendy version
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The Gulfstream G200 mid size corporate jet was built by Israel Aircraft Industries and was originally marketed and supported by subsidiary Galaxy Aerospace Inc, before being acquired by Gulfstream in May 2001. The G200 (Galaxy) features a wing design based on the swept high speed unit of the Astra, but otherwise is a completely new design. It features a new ""widebody"" fuselage, significantly wider and longer than the Astra's, with standup room. The rear fuselage is area ruled to reduce drag, while the wing features winglets. The Galaxy also features an EFIS Collins Pro Line 4 cockpit and nonstop trans Atlantic and one stop trans Pacific range. IAI selected the Pratt & Whitney Canada PW-306A turbofans for the Galaxy. The PW-306A is a growth development (with increased fan diameter, improved hot end material and a forced mixer in the exhaust) of the PW-305 series that powers the Hawker 1000 and Learjet 60. In June 2001, Galaxy Aerospace was acquired by Gulfstream Aerospace, and rebadged the Galaxy the G200.

Seating (normal) 10 Max Takeoff (lbs) 35,450
Seating (maximum) - Certified Ceiling (ft) 45,000
Engines 2 P&WC PW306A To (Sealevel, ISA Temp) (ft) 6,083
Output lbs ea. Flat Rating 6,040/ISA+10 Landing Distance (ft) 2,590
Maximum Mach No. 0.85 Max Range (fuel) (nm) 3,432
High Speed Cruise (Kts) 470 Max Range (payload) (nm) 2,371
Flight Time 300nm 0 + 48 Flight Time 1000nm 2 + 26
Flight Time 600nm 1 + 30    
External Internal
Length (ft) 62.30 Length (ft) 24.40
Height (ft) 21.40 Height (ft) 6.30
Span (ft) 58.10 Width: Max floor (ft) 7.20
 

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