Pilatus PC-21 MK.II
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Ailerons are smaller, overall appearance tweaks for accuracy. The Pilatus PC-21 is a single-turboprop, low wing swept monoplane advanced trainer with a stepped tandem cockpit manufactured by Pilatus Aircraft of Switzerland. Roll-out of the PC-21 prototype was on 30 April 2002 at Pilatus' factory in Stans, Switzerland, with the first flight taking place on 1 July of the same year. -Wikipedia
Specifications
General Characteristics
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- Wingspan 24.3ft (7.4m)
- Length 23.6ft (7.2m)
- Height 12.2ft (3.7m)
- Empty Weight 3,450lbs (1,565kg)
- Loaded Weight 4,495lbs (2,038kg)
Performance
- Horse Power/Weight Ratio 0.333
- Wing Loading 33.5lbs/ft2 (163.4kg/m2)
- Wing Area 134.3ft2 (12.5m2)
- Drag Points 1604
Parts
- Number of Parts 33
- Control Surfaces 5
- Performance Cost 218