Gulfstream · United States · ICAO: GALX · 1999–2011 ·
$23 million (2011)

Balancing the Act The Gulfstream G200

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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
Cabin width:
ft 2 in · 2.18 m
Cabin height:
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:
ft 3 in · 2.22 m
Wing span / rotor:
58 ft 1 in · 17.70 m
Baggage volume:
127 ft³  ·  3.6 
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
Approach speed (Vref):
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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Detailed information, specs, interiors, fuel cost, performance stats and pictures of the Gulfstream G200 private charter jet.

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