Overview
The Gulfstream G280 entered service in the early 2010s as the successor to the G200. Designed for improved performance and systems integration, it occupies the super-midsize segment. The aircraft offers transcontinental and select intercontinental capability.
Live Fleet Activity (G280)
📡
Fetching live data…
Specifications
Units
- Engine
- 2 × Honeywell HTF7250G
- Engine type
- Turbofan
- Thrust
- 2 × 7,624 lbf · 34 kN
- Avionics
- Rockwell Collins ProLine Fusion
- Wing tips
- Blended tips
- Seats
- 12
- Crew
- —
- Cabin width
- 6 ft 11 in · 2.11 m
- Cabin height
- 6 ft 1 in · 1.85 m
- Cabin length
- 25 ft 10 in · 7.87 m
- Exterior length
- 66 ft 7 in · 20.30 m
- Tail height
- 21 ft 4 in · 6.50 m
- Fuselage diameter
- 7 ft 7 in · 2.30 m
- Wing span
- 63 ft 0 in · 19.20 m
- Baggage volume
- 120 ft³ · 3.4 m³
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 39,600 lb · 18,000 kg
- Max landing weight
- 32,700 lb · 14,800 kg
- Max payload
- 4,050 lb · 1,850 kg
- Fuel capacity
- 2,200 gal · 8,300 L · 6,600 kg (Jet A)
- Max cruise speed
- 547 kt · 629 mph · 1,013 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- 140 kt · 161 mph · 259 km/h
- Range
- 3,400 nm · 3,910 mi · 6,300 km
- Fuel burn
- 1.56 nm/gal · 0.76 km/L
- Ceiling
- 45,000 ft · 13,700 m
- Rate of climb
- 5,000 ft/min · 25 m/s
- Takeoff distance
- 4,750 ft · 1,450 m
- Landing distance
- 2,700 ft · 830 m
Gallery
(/)
tap to zoom
(/)
Live fleet activity details
📡