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Schweizer 333  
Initial Operational Capability (IOC):
Total Production: ?
Also Known As: S-333
Origin: United States of America
Corporations: Schweizer Aircraft
Parent System: Schweizer 333
Initial Operational Capability (IOC):
Total Production: ?
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Description: The Schweizer 333 is a light, single-turbine powered helicopter developed by Schweizer Aircraft suitable for law enforcement patrol, commercial and military flight training, power line/pipeline patrol, personal use and lift operations. The aircraft features low acquisition and direct operating costs in the single-turbine helicopter segment. The Schweizer 333 helicopter spacious cabin offers superb visibility and a seating capacity for up to four passengers, usually three passengers. It is powered by a single Rolls-Royce Model 250-C20W engine driving a three-bladed main rotor and a two-bladed tail rotor. The helicopter features outstanding low noise signature, reliability, crashworthy airframe and flight performance.

The Schweizer Model 333 was selected by Northrop Grumman as the basis for the RQ-8 Fire Scout Vertical Takeoff Unmanned Aerial Vehicle (VTUAV) used by the United States Armed Forces.

Schweizer 333 Applications


Support Aircraft RQ-8A Fire Scout

Schweizer 333 Specifications

Crew: 1
Main Rotor Blades: 3
Number of Engines: 1
Passengers: 3
Tail Rotor Blades: 2
Area
Main Rotor Disc Area: 594 square foot (55 square meter)
Dimensions
Cabin Width: 72 inch (1.84 meter)
Height: 11 foot (132 inch)
Length: 31.0 meter (1,222 inch)
Main Rotor Diameter: 27.5 foot (330 inch)
Tail Rotor Diameter: 4.25 foot (51 inch)
Width: 5.65 foot (68 inch)
Performance
Ceiling: 12,300 foot (3,749 meter)
Hovering Ceiling: 8,900 foot (2,713 meter)
Max Range: 310 nautical mile (357 mile)
Power
Max Continuous Power: 232 shp (173 kW)
Max Power at TakeOff: 253 shp (189 kW)
Rates
Main Rotor RPM: 471 roundperminute
Speed
Cruise Speed: 105 knot (194 kph)
Time
Flight Endurance: 3.90 hour (234 minute)
Volume
Fuel Tank Capacity: 73 galon (277 liter)
Weight
Empty Weight: 1,300 pound (590 kilogram)
Fuel Load: 493 pound (224 kilogram)
Max Takeoff Weight: 2,550 pound (1.16 ton)
Useful Load: 1,250 pound (567 kilogram)
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)

Schweizer 333 News

There are 5 news between
4 Nov 2005 and 16 Dec 2009
Wednesday, December 16, 2009Sikorsky Delivers First Two S-434 Helicopters
Tuesday, February 24, 2009Aircom Orders First S-434 Certified Commercial Helicopter
Thursday, May 31, 2007MQ-8B Fire Scout to Enter Production
Tuesday, February 6, 2007US Navy Buys Two Additional Fire Scouts to Help Refine Concept of Operations
Friday, November 4, 2005X2 Fly-By-Wire Surrogate Vehicle First Flight

Operators & Related Equipment


OperatorsItems
Poland?
Aircraft ordered by Aircom SP Z.O.O. (2)

Grand Total ?2
Propulsion Systems
Model 250-C20Wx1
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