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Sikorsky S92 - Engine(s) GE CT7-8 A HP (takeoff) 2,520 shp/1,879 kw
Dimensions main rotor 56.33 ft/17.17 m Tail rotor 11.0 ft/3.35 m
Height 17.95 ft/5.47 m Length 68.50 ft/20.88 m Width 17.26 ft/5.26 m (includes horizontal stabilizer)
Empty weight *16,752 lbs/7,597 kg Gross weight 26,500 lbs/12,018 kg
Useful load *9,748 lbs/4,421 kg External max. 8,000 lbs/3,628 kg
Vne 165 kts Max cruise 151 kts /280 kph
Max rate of climb 1,600 fpm @ max GW
HIGE 9,000 ft/2,743 m HOGE 6,500 ft/1,981 m
Service ceiling 14,000 ft/4,267 m S/E service ceiling 5,000 ft/1,542 m
Std fuel 755gal/2,858 l Max fuel 760 gal/2,877 l
Max range std fuel (no reserve) 539 nm/999 km
IFR Crew 2 Passengers 19
Standard avionics Collins Proline IV
Sikorsky S92 - Engine(s) GE CT7-8 A HP (takeoff) 2,520 shp/1,879 kw Dimensions main rotor 56.33 ft/17.17 m Tail rotor 11.0 ft/3.35 m Height 17.95 ft/5.47 m Length 68.50 ft/20.88 m Width 17.26 ft/5.26 m (includes horizontal stabilizer) Empty weight *16,752 lbs/7,597 kg Gross weight 26,500 lbs/12,018 kg Useful load *9,748 lbs/4,421 kg External max. 8,000 lbs/3,628 kg Vne 165 kts Max cruise 151 kts /280 kph Max rate of climb 1,600 fpm @ max GW HIGE 9,000 ft/2,743 m HOGE 6,500 ft/1,981 m Service ceiling 14,000 ft/4,267 m S/E service ceiling 5,000 ft/1,542 m Std fuel 755gal/2,858 l Max fuel 760 gal/2,877 l Max range std fuel (no reserve) 539 nm/999 km IFR Crew 2 Passengers 19 Standard avionics Collins Proline IV
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