Overview
The Sikorsky S-76C++ is a twin-engine medium helicopter developed for corporate, offshore, and government missions. It represents one of the most refined versions of the long-running S-76 family. The aircraft combines executive comfort with strong operational performance.
Specifications
Units
- Engine
- 2 × Turboméca Arriel 2S1
- Engine type
- Turboshaft
- Power
- 2 × 922 shp · 688 kW
- Avionics
- Honeywell Avionics
- Wing tips
- No winglets
- Seats
- 12
- Crew
- —
- Cabin width
- 6 ft 4 in · 1.93 m
- Cabin height
- 4 ft 5 in · 1.35 m
- Cabin length
- 7 ft 11 in · 2.41 m
- Exterior length
- 52 ft 6 in · 16.00 m
- Tail height
- —
- Fuselage diameter
- —
- Wing span
- 44 ft 0 in · 13.41 m
- Baggage volume
- 35 ft³ · 1.0 m³
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 11,700 lb · 5,300 kg
- Max landing weight
- —
- Max payload
- 3,450 lb · 1,600 kg
- Fuel capacity
- 280 gal · 1,100 L · 900 kg (Jet A)
- Max cruise speed
- 155 kt · 178 mph · 287 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 345 nm · 400 mi · 640 km
- Fuel burn
- 1.23 nm/gal · 0.60 km/L
- Ceiling
- 15,000 ft · 4,600 m
- Rate of climb
- 1,350 ft/min · 7 m/s
- Takeoff distance
- —
- Landing distance
- —
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