Overview
The Gulfstream G200 entered service in the late 1990s as a super-midsize business jet. Originally developed by Israel Aircraft Industries, it was later marketed under Gulfstream branding. The aircraft offered extended range and cabin comfort for its class.
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Specifications
Units
- Engine
- 2 × Pratt and Whitney PW306A
- Engine type
- Turbofan
- Thrust
- 2 × 6,040 lbf · 27 kN
- Avionics
- Rockwell Collins Pro Line 4
- Wing tips
- Blended tips
- Seats
- 18
- Crew
- —
- Cabin width
- 7 ft 2 in · 2.18 m
- Cabin height
- 6 ft 3 in · 1.90 m
- Cabin length
- 24 ft 5 in · 7.44 m
- Exterior length
- 62 ft 3 in · 18.97 m
- Tail height
- 21 ft 5 in · 6.53 m
- Fuselage diameter
- 7 ft 3 in · 2.22 m
- Wing span
- 58 ft 1 in · 17.70 m
- Baggage volume
- 127 ft³ · 3.6 m³
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 35,500 lb · 16,100 kg
- Max landing weight
- 30,000 lb · 13,600 kg
- Max payload
- 4,050 lb · 1,850 kg
- Fuel capacity
- 2,250 gal · 8,500 L · 6,800 kg (Jet A)
- Max cruise speed
- 470 kt · 541 mph · 870 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- 100 kt · 115 mph · 185 km/h
- Range
- 3,400 nm · 3,910 mi · 6,300 km
- Fuel burn
- 1.52 nm/gal · 0.74 km/L
- Ceiling
- 45,000 ft · 13,700 m
- Rate of climb
- 3,700 ft/min · 19 m/s
- Takeoff distance
- 6,100 ft · 1,850 m
- Landing distance
- 2,600 ft · 790 m
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