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Sikorsky S-92A
The S-92A is a large twin-engine helicopter with four-blade main and tail rotors, retractable wheeled landing gear and an aluminium fuselage with composite parts. The FAA certified it in December 2002 and EASA in June 2004. Two General Electric CT7-8 or CT7-8A turboshaft engines drive a main rotor 17.17 meters across. Two pilots fly it with up to 19 passengers. The maximum take-off weight is 12,020 kg, or 12,565 kg with the gross weight expansion option, and it can lift an external load of 3,629 kg. The fuselage is 17.10 meters long and the tanks hold 2,872 litres of usable fuel.
- Engines
- Two General Electric CT7-8 or CT7-8A turboshafts mounted above the fuselage
- Max takeoff weight
- 26,500 lb (12,020 kg)
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Specifications
| Length | 56 ft 1 in (17.10 m) |
|---|---|
| Height | 14 ft 2 in (4.32 m) |
| Ceiling | 15,000 ft (4,600 m) |
| Fuel capacity | 760 US gal (2,872 L) |
| Status | In service |
| Type codes | ICAO S92 |
Who flies it now
152 flights by other operators
From flights seen in US airspace in the last 14 days (public flight data).
In the air now
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Flights of this type in the air now, from public flight data.