Schweizer 330 / 333
Photo ©: Wim Sonneveld (Photos at airliners.net)
330 / 333
Light Utility Helicopter
| Crew | 1-2 | |
| Passengers | 2-3 | |
| Propulsion | 1 Turboshaft Engine | |
| Engine Model | Allison / Rolls-Royce 250-C20W | |
| Engine Power | 209 kW | 280 shp |
| Speed | 222 km/h | 120 kts 138 mph |
| Service Ceiling | 3.962 m | 13.000 ft |
| Range | 561 km | 303 NM 349 mi. |
| Empty Weight | 590 kg | 1.300 lbs |
| max. Takeoff Weight | 1.157 kg | 2.550 lbs |
| Rotor Blades (main/tail) | 3/2 | 3/2 |
| Main Rotor Diameter | 8,39 m | 27,5 ft |
| Tail Rotor Diameter | 1,30 m | 4,3 ft |
| Rotor Disc Area | 55,3 m² | 595 ft² |
| Length (Fuselage) | 6,82 m | 22,4 ft |
| Length | 9,51 m | 31,2 ft |
| Height | 3,34 m | 11,0 ft |
| First Flight | 14.06.1988 | |
| Production Status | in production | |
| Developed from | Schweizer 300 | |
| Data for (Version) | Schweizer 333 | |
Remarks
Development of Schweizer 300 with a turboshaft engine. Official FAA designation is Schweizer 269D, Configuration A.
| Extras | |
print view| [Photo-ID: 3452] © Karsten Palt 2010-06-11 | |
 | Schweizer / Sikorsky S-434 Sikorsky (Saudi Ministry of Interior) Reg.: MOI-86 c/n: 0086MB |
| ILA Berlin 2010 [Berlin - Schönefeld (EDDB / SXF)] | |