The Model 333 provides:

• Thirty percent (30%) more useful load than a comparably equipped 330SP
• Upgraded main rotor system including: blades with cambered airfoil; large diameter, splined hub assembly; oil-filled drive shaft
• Superior cruise and hover performance in high and hot operating conditions
• Bottom line value: the most cost-effective turbine helicopter on the market today
• Unequaled flight stability and outstanding handling characteristics
• High stance landing gear with improved ground clearance
• Spacious cabin with superb visibility
• Reduced pilot fatigue because of: ergonomically designed seats, low control forces, low vibration levels, and low cabin noise levels
• Broad range of customer services, from spare parts support to maintenance training
• New standard for safety: forgiving flight characteristics and components with proven reliability reduce the risk of accident; unparalleled energy absorption for crew protection
• Lowest noise signature of any conventional tail rotor turbine helicopter

Performance

• VNE(Kias) SeaLevel 120knots 222km/hr
• Cruise Speed 105 knots 192 km/hr
• Maximum Endurance 4.1 hrs
• Maximum Range 310nm 574km

Weight

• Empty weight 1250 lbs 567 kg
• Gross weight 2550 lbs 1157 kg
• Useful load 1300 lbs 590 kg

Rotor System

• Main rotor diameter 27.51 ft 8.39 m
• Main rotor disk area 594 sq/ft 55.18 sq/m
• Main rotor RPM 466 - 471 466 - 471
• Tail rotor diameter 4.25 ft 1.30 m

Powerplant

• Rolls-Royce 250-C20W Gas Turbine Engine
• Maximum takeoff (Derated) 250 shp 186 kw
• Maximum continuous (Derated) 230 shp 171 kw

Fuel (Turbine Fuel)

• Usable capacity (73 gal) 493 lbs 224 kg

Weight

• Empty weight 1250 lbs 567 kg
• Gross weight 2550 lbs 1157 kg
• Useful load 1340 lbs 590 kg