Overview
Robinson R66 — single-engine turbine light helicopterDevelopment of the R66 built directly on the success of the R44 series. The helicopter first flew in 2007 and entered service in 2010. Externally similar to its piston predecessors, it features a two-blade main rotor system and a stretched fuselage to accommodate a fifth seat and additional baggage space.A single Rolls-Royce RR300 turboshaft engine rated at approximately 300 shaft horsepower powers the aircraft. Typical cruise speed is about 110 knots (204 km/h). Maximum takeoff weight exceeds 2,700 pounds (1,225 kg), allowing improved payload compared with earlier Robinson designs.The R66 quickly gained popularity in law enforcement, tourism, and light utility work. Its turbine engine improved high-altitude performance and reliability in hot climates. Production continues, making it one of the most accessible turbine helicopters on the market.
Live Fleet Activity (R66)
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Specifications
- Engine
- 1 × Rolls-Royce RR300 turboshaft
- Engine type
- Turboshaft
- Power
- 270 shp · 201 kW
- Avionics
- —
- Wing tips
- No winglets
- Seats
- 5
- Crew
- —
- Cabin width
- 4 ft 0 in · 1.21 m
- Cabin height
- 4 ft 4 in · 1.31 m
- Cabin length
- —
- Exterior length
- 41 ft 3 in · 12.57 m
- Tail height
- 11 ft 5 in · 3.48 m
- Fuselage diameter
- 4 ft 6 in · 1.37 m
- Wing span
- 33 ft 0 in · 10.06 m
- Baggage volume
- 18 ft³ · 0.5 m³
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 3,000 lb · 1,350 kg
- Max landing weight
- —
- Max payload
- 1,300 lb · 600 kg
- Fuel capacity
- 70 gal · 300 L · 200 kg (Jet A)
- Max cruise speed
- 113 kt · 130 mph · 209 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 400 nm · 460 mi · 740 km
- Fuel burn
- 6.67 nm/gal · 3.26 km/L
- Ceiling
- 14,000 ft · 4,300 m
- Rate of climb
- 1,000 ft/min · 5 m/s
- Takeoff distance
- —
- Landing distance
- —
Gallery
Live fleet activity details
Robinson R44
Kazan Aktai