Specifications
| Engine | 2 x General Electric CT7-8A 2740 shp |
|---|---|
| Capacity | 2 + 19 |
| Length (m) | 17.1 |
| Height (m) | 4.7 |
| Blades | 4 |
| Rotor diam. (m) | 17.17 |
| Disc area (m2) | 246 |
| Weight (kgs) | Empty: 7000 Max: 12000 |
| Speed (km/h) | Cruise: 280 Max: 306 |
| Range (km) | 1000 |
| Ceiling (m) | 4000 |
Derivatives & Versions
| S-92F | 2001 | Prototype military transport and civil freighter version of S-92 Superhawk, first flown 2001. |
| S-92A | 2004 | First production model |
| S-92A VVIP | 2005 | Head of State VIP version of S-92A. |
| CH-148 Cyclone | 2008 | Canadian Armed Forces shipboard helicopter to replace the Sea King |
| VH-92A Patriot | 2014 | After the cancellation of the AgustaWestland VH-71, the S-92 was selected as the new presidential VIP aircraft Marine One to be operated by HMX-1 The basic S-92A from the production line at Sikorsky plant in Coatesville, Pennsylvania is taken to a dedicated VH-92A facility for subsystem integration in Stratford, Connecticut where some components such as circuit breaker panels, engines, and main and tail rotor blades are changed. |
| S-92A+ | 2019 | The S-92A is an upgrade package proposed for existing Sikorsky S‑92 helicopters. |
| S-92B | 2019 | First announced at Heli-Expo 2019, the second generation S-92 introduces CT7-8A6 engines, phase IV main gearbox. |