SCHWEIZER S333™
Specifications
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SCHWEIZER S333™
Schweizer’s turbine-powered aircraft features a 1,250 lb. useful load, making it a versatile platform for everything from military training and public service to personal use. With three- and four-seat configurations, this helicopter is an ideal initial turbine aircraft with lower direct operating costs comparable to other light turbine helicopters.
Turbine Power
Small and powerful, the S333 features a 1,250 lb. useful load and 120 kts speed making it a cost-effective turbine helicopter.
Increased Passenger Capacity
The S333 is available in three- and four-seat configurations, providing operators versatility for a variety of missions.
Multi-mission Capable
The S333 is a proven military training and operations aircraft currently in service around the world. With interior and exterior cargo capability, it is also a capable platform for public safety, utility, ISR, and personal use.
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SCHWEIZER S333™ Specifications
Performance
Standard day, sea level, maximum gross weight unless otherwise noted
- Maximum speed (VNE) 120kts. 222km/hr
- Maximum cruise speed (vh) 95kts. 176km/hr
- Hover ceiling, In-Ground-Effect (2550 lb.) 8,900 ft / 2,713 m
- Hover ceiling, Out-of-Ground-Effect (2550 lb.) 5,900 ft. / 1,798 m
- Range (long range cruise* speed @ 2,000 ft, std day) (no reserve) • 303 nm • 561 km
Weights
- Maximum takeoff gross weight 2,550 lb. / 1,157kg
- Empty weight, standard configuration 1,300 lb. / 590 kg Useful load
- 1,250 lb. / 567 kg
Dimensions
- Fuselage length 22.38 ft. / 6.83 kg
- Fuselage width 5.65 ft. / 1.72 m
- Fuselage height (to top of tail pylon) 8.06 ft. / 2.46 m
- Overall length (rotors turning) 31.17 ft. / 9.51 m
- Overall height (to top of tail rotor) 11.00 ft. / 3.34 m
- Width (horizontal stabilizer) 6.70 ft. / 2.04 m
- Main rotor diameter 27.51 ft. / 8.39 m
- Tail rotor diameter 4.25 ft. / 1.30 m
Accommodations
- Normal cabin seating (training) 3 passengers
- Maximum certified cabin seating (utility) 4 passengers
- Cabin length 6.50 ft. / 1.98 m
- Cabin width 6.03 ft. / 1.85 m
Powerplant
- Type Rolls Royce 250-C20W Gas Turbine
- Powerplant ratings (per engine, standard day, sea level) -Takeoff (5-minute) 280 shp / 209 kw -Maximum continuous 232 shp / 164 kw
Fuel Capacity
- Standard fuel capacity (73 0 US gal) 493 lb. / 224 kg