Overview
The Bell Agusta BA609, later known as the AW609, is a tiltrotor aircraft designed for civil markets. Developed to blend vertical takeoff capability with fixed-wing cruise performance, it first flew in the early 2000s. The program has experienced extended development timelines.
Live Fleet Activity (B609)
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Specifications
Units
- Engine
- 2 × Pratt & Whitney PT6C-67A
- Engine type
- Turboshaft
- Power
- 2 × 1,940 shp · 1,447 kW
- Avionics
- Rockwell Collins Pro-line 21
- Wing tips
- No winglets
- Seats
- 9 economy · 6 business
- Crew
- —
- Cabin width
- 5 ft 0 in · 1.52 m
- Cabin height
- 4 ft 8 in · 1.42 m
- Cabin length
- 17 ft 6 in · 5.33 m
- Exterior length
- 43 ft 8 in · 13.30 m
- Tail height
- 14 ft 9 in · 4.50 m
- Fuselage diameter
- 5 ft 3 in · 1.60 m
- Wing span
- 60 ft 0 in · 18.30 m
- Baggage volume
- 49 ft³ · 1.4 m³
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 16,800 lb · 7,600 kg
- Max landing weight
- —
- Max payload
- 5,500 lb · 2,500 kg
- Fuel capacity
- 370 gal · 1,400 L · 1,100 kg (Jet A)
- Max cruise speed
- 275 kt · 316 mph · 509 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 1,000 nm · 1,150 mi · 1,850 km
- Fuel burn
- 2.00 nm/gal · 0.98 km/L
- Ceiling
- 25,000 ft · 7,600 m
- Rate of climb
- 1,500 ft/min · 8 m/s
- Takeoff distance
- —
- Landing distance
- —
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Live fleet activity details
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