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Schweizer 333
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Schweizer333 - Engine(s) Rolls-Royce 250-C20W HP (takeoff) 280 shp
Dimensions main rotor 27.51 ft/8.39 m Tail rotor 4.25 ft/1.3 m
Height 11.14 ft/3.40 m Length 17 ft/5.18 m Width 6.29 ft/1.91 m
Empty weight 1,250 lbs Gross weight 2,550 lbs
Useful load 1,300 lbs External N/A
Vne 120 kts/222 km/hr Max cruise 105 kts/194 km/hr
Max rate of climb 1,500 fpm
HIGE 12,300 ft/3,749 m HOGE 9,200 ft/2,804 m (@2,300 lbs/1,045 kg)
Service ceiling 13,000 ft/3,902 m S/E service ceiling N/A
Std fuel 73 gal/137 lit
Max range std fuel (no reserve) 310 nm/590 km
VFR Crew 1 Passengers 3
Standard avionics Optional factory-installed avionics available.
Schweizer333 - Engine(s) Rolls-Royce 250-C20W HP (takeoff) 280 shp Dimensions main rotor 27.51 ft/8.39 m Tail rotor 4.25 ft/1.3 m Height 11.14 ft/3.40 m Length 17 ft/5.18 m Width 6.29 ft/1.91 m Empty weight 1,250 lbs Gross weight 2,550 lbs Useful load 1,300 lbs External N/A Vne 120 kts/222 km/hr Max cruise 105 kts/194 km/hr Max rate of climb 1,500 fpm HIGE 12,300 ft/3,749 m HOGE 9,200 ft/2,804 m (@2,300 lbs/1,045 kg) Service ceiling 13,000 ft/3,902 m S/E service ceiling N/A Std fuel 73 gal/137 lit Max range std fuel (no reserve) 310 nm/590 km VFR Crew 1 Passengers 3 Standard avionics Optional factory-installed avionics available.
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