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Mid Range regional Turboprop now with “neo” engines they are on paper less powerful than the base version in terms of BHP but because of the larger blades more thrust is able to be genrated iut of slightly less powerful emgimes which actually makes it more powerful than the base model with 25 percent less emissions and 25 percent more range its also faster at 500 kmph compared to 350 kmph and to top it all of its a STOL aircraft ENGINE SPECIFICATIONS (EASTERN INTERNATION TB-neo) 2493 BHP each 4900 bhp combined thrust 105 inch schimitar blades in 6-6 config. )
Specifications
General Characteristics
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- Wingspan 50.6ft (15.4m)
- Length 78.2ft (23.8m)
- Height 16.9ft (5.2m)
- Empty Weight 8,195lbs (3,717kg)
- Loaded Weight 14,060lbs (6,377kg)
Performance
- Horse Power/Weight Ratio 0.354
- Wing Loading 39.4lbs/ft2 (192.2kg/m2)
- Wing Area 357.1ft2 (33.2m2)
- Drag Points 4584
Parts
- Number of Parts 39
- Control Surfaces 7
- Performance Cost 356
