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Enstrom F-28F - Engine(s) Lycoming HIO-360-F1AD w/turbocharger HP (takeoff) 225 shp
Dimensions main rotor 32 ft/9.75 m Tail rotor 4.7 ft/1.43 m
Height 9 ft/2.74 m Length 29.3 ft/8.9 m Width 7.3 ft/2.23 m
Empty weight 1,640 lbs/744 kg Gross weight 2,600 lbs/1,180 kmh
Useful load 960 lbs/435 kg External 1,000 lbs/454 kg
Vne 97 kts/180 kmh (SL to 915 m) Max cruise 100 kts/185 kmh
Max rate of climb 1,450 fpm/442 mpm 
HIGE 13,200 ft/4,023 m; 7,700 ft/2,347 m
HOGE 8,700 ft/2,652 m @ 2,350 lbs 
Service ceiling 12,000 ft/3,658 m (max. alt.) S/E service ceiling N/A 
Std fuel 40 gal/159 lit Max fuel 53 gal/201 lit 
Max range std fuel (no reserve) 229 nm/424 km
Range with opt fuel 313 nm/580 km VFR Crew 1 Passengers 2
Stanard avionics Furnished upon request.
Enstrom F-28F - Engine(s) Lycoming HIO-360-F1AD w/turbocharger HP (takeoff) 225 shp Dimensions main rotor 32 ft/9.75 m Tail rotor 4.7 ft/1.43 m Height 9 ft/2.74 m Length 29.3 ft/8.9 m Width 7.3 ft/2.23 m Empty weight 1,640 lbs/744 kg Gross weight 2,600 lbs/1,180 kmh Useful load 960 lbs/435 kg External 1,000 lbs/454 kg Vne 97 kts/180 kmh (SL to 915 m) Max cruise 100 kts/185 kmh Max rate of climb 1,450 fpm/442 mpm HIGE 13,200 ft/4,023 m; 7,700 ft/2,347 m HOGE 8,700 ft/2,652 m @ 2,350 lbs Service ceiling 12,000 ft/3,658 m (max. alt.) S/E service ceiling N/A Std fuel 40 gal/159 lit Max fuel 53 gal/201 lit Max range std fuel (no reserve) 229 nm/424 km Range with opt fuel 313 nm/580 km VFR Crew 1 Passengers 2 Stanard avionics Furnished upon request.
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