S-434  
Initial Operational Capability (IOC): 16 December 2009
Total Production: 10
Origin: United States of America
Corporations: Schweizer Aircraft
Parent System: S-434
Initial Operational Capability (IOC): 16 December 2009
Total Production: 10
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Description: The S-434 is the next-generation light single-turbine helicopter being developed by Sikorsky and Schweizer Aircraft based on the Schweizer 333 helicopter. The new aircraft will incorporate many of the design and performance technologies developed on the RQ-8 Fire Scout VTUAV. It will feature a new four-bladed main rotor system and a larger fuel tank. It will be powered with a more powerful engine which may be the newest Rolls-Royce RR300 turboshaft. All in, the new aircraft will fly faster and farther and having a larger useful load then Schweizer 333 helicopter. The S-434 helicopter was launched at Heli-Expo on February 24, 2008.

S-434 Specifications

Main Rotor Blades: 4
Number of Engines: 1
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)

S-434 News

There are 3 news between
4 Sep 2008 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, September 4, 2008Sikorsky Aerospace Services to Support Saudi Arabia's Ministry of Interior Helicopter Fleet

Operators & Related Equipment


OperatorsItems
Poland1
Aircraft ordered by Aircom SP Z.O.O. (1)
Saudi Arabia9
Aircraft ordered in 2007 by the Ministry of the Interior for training purposes (9)

Grand Total 102
Propulsion Systems
RR300x1
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