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Bell 222 is the first dual engine light civil helicopter bell222 developed by American Daxin Bell Helicopter Company. Its prototype was first tested on August 13, 1976, approved by FAA on August 16, 1979 and put into production for the first time. On January 16, 1980, it was put into operation for the first time. VTOL controls up and down
Specifications
Spotlights
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General Characteristics
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- Wingspan 23.5ft (7.2m)
- Length 62.4ft (19.0m)
- Height 16.1ft (4.9m)
- Empty Weight 23,310lbs (10,573kg)
- Loaded Weight 29,489lbs (13,376kg)
Performance
- Power/Weight Ratio 6.096
- Wing Loading 617.4lbs/ft2 (3,014.4kg/m2)
- Wing Area 47.8ft2 (4.4m2)
- Drag Points 7916
Parts
- Number of Parts 84
- Control Surfaces 0
- Performance Cost 461
