Sikorsky Aircraft Corporation

Sikorsky S-434

The Sikorsky S‑434 is a light utility helicopter developed by Sikorsky Aircraft Corporation as a modern evolution of the company’s long‑standing S‑300 series. First rolled out in 2005, the S‑434 entered service with both civilian operators and military customers, offering a blend of proven reliability and advanced technology. Its airframe incorporates composite materials and a streamlined fuselage that reduce weight while improving corrosion resistance. Power is supplied by a Turbomeca Arriel 2S1 turboshaft engine delivering 750 shaft horsepower, giving the aircraft a maximum cruise speed of 140 knots and a service ceiling above 20,000 feet. The cabin can be configured for up to eight passengers, medevac stretchers, or external cargo sling loads, making it versatile for transport, law‑enforcement, and offshore support missions. Modern avionics include a glass cockpit with dual Garmin G5000 displays, FADEC engine control, and integrated GPS‑based navigation, enhancing safety and reducing pilot workload. The S‑434’s significance lies in its role as a bridge between legacy rotorcraft and next‑generation platforms, demonstrating how incremental upgrades can extend the operational life of a proven design while meeting contemporary performance and efficiency demands.
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Classification

Dimensions

Length
9.4 metre
Height
3.35 metre
Mass
610.08 kilogram

Production & History

First Flight
2008

Design & Classification

Manufacturer
Sikorsky Aircraft Corporation
Engine
Allison 250-C20W
Wikidata ID
Q2285606