Schweizer 300CB was introduced in 1996. The 300CB features excellent flight training properties, a large useful load and comfortable cockpit, and safety characteristics. The 300CB helicopter is manufactured by Schweizer Aircraft in Elmira, New York and part of the 269 Series helicopter line of which more than 3,800 helicopters have been produced.
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Lowest cost |
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Designed-in crashworthiness features | |
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Exceptional safety margins | |
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Large power reserve | |
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Precise, vibration-free flight control | |
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Spacious cockpit | |
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Standard aircraft fully equipped | |
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Easy maintenance |
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Less down time and lower costs | |
| Performance | Power Plant-Textron Lycoming | |||
| ˙ | Vne (Kias) at Sea Level 94 kts | ˙ | HO-360 CIA | |
| ˙ | Cruise Speed 80 kts | ˙ | Maximum takeoff 180 shp | |
| ˙ | Maximum Endurance (35 gal) 3.3 hrs | ˙ | Maximum continuous 180 shp | |
| ˙ | Maximum Endurance (65 gal) 6.2 hrs | ˙ | Rotor system | |
| ˙ | Maximum Range (35 gal) 240 mi | ˙ | Main rotor diameter 26.83 ft | |
| ˙ | Maximum Range (65 gal) 440 mi | ˙ | Main rotor disk areas 565 sq.ft | |
| ˙ | Hover Ceiling IGE (1600 lbs) 7,000 ft | ˙ | Main rotor RPM 471 | |
| ˙ | Hover Ceiling OGE (1600 lbs) 4,800 ft | ˙ | Tail rotor diameter 4.25 ft | |
| Dimensions | Fuel | |||
| ˙ | Height (overall) 8.72 ft | ˙ | Standard capacity 210 lbs | |
| ˙ | Length (overall) 30.83 ft | ˙ | Auxiliary fuel 180 lbs | |
| ˙ | Fuselage length 22.19 ft | ˙ | Empty weight 1,088 lbs | |
| ˙ | Landing gear tread width 6.54 ft | ˙ | Gross weight 1,750 lbs | |
| ˙ | Seating Capacity | ˙ | Useful load 662 lbs | |
| ˙ | Standard Right Hand PIC 2 | |||
| ˙ | Optional Left Hand PIC 3 | |||