SCHWEIZER SALES (page 4 of 4)
The Schweizer 333 
The Model 333 has more power, more gross weight, more useful load, more speed, more hover performance; and best of all, the lowest operating cost of any turbine-powered helicopter. The Model 333...a new helicopter for a new millennium; a new standard for light turbine-powered helicopters.
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.
| Schweizer 333 Specification | ||
| Imperial | Metric | |
| Performance |
||
| VNE(Kias) SeaLevel | 120 knots | 222 km/hr |
| Cruise Speed | 105 knots | 192 km/hr |
| Maximum Endurance | 4.1 hrs | 4.1 hrs |
| Max Range | 310 nm | 574 km |
| Weight | ||
| Empty weight | 1250 lbs | 567 kg |
| Gross weight | 2550 lbs | 1157 kg |
| Useful load | 1300 lbs | 590 kg |
| Dimensions | ||
| Length (overall) | 31.17 ft | 9.51 m |
| Fuselage length | 22.38 ft | 6.82 m |
| Landing gear tread width | 6.99 ft | 2.13 m |
| Power Plant - Rolls-Royce 250-C20W Gas Turbine Engine | ||
| Maximum Take Off (Derated) | 250 shp | 186 kw |
| Maximum Continuous (Derated) | 230 shp | 171 kw |
| 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 |
| Fuel (Turbine Fuel) | ||
| Usable capacity (73 gal) | 493 lbs | 224 kg |
| Seating Capacity | ||
| Training 3, Utility 4 | ||
|
|
 |
|||||
 |
 |
||||
|
|
|||||
|
|
|||||
|
|
|||||
|
|
|||||
|
[email protected] |
|||||
|
|
|||||
|
|
|||||
|
|
|||||
|
[email protected] |
|||||
|
|
|||||
|
|
Email: [email protected]
HOME • FOR SALE • SIKORSKY • SCHWEIZER • SERVICES • ABOUT US • NEWS • CONTACT • GALLERY • LINKS • LEGAL
©2005 - All rights reserved.