The AIDC XC-2 is a prototype turboprop powered civil transport and cargo monoplane aircraft,first flown in 1978 in Taiwan.It's powerplants are two Lycoming/Honeywell T53 turboprop engines.
Specifications
General Characteristics
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- Wingspan 48.3ft (14.7m)
- Length 36.2ft (11.0m)
- Height 17.1ft (5.2m)
- Empty Weight 6,789lbs (3,079kg)
- Loaded Weight 7,354lbs (3,336kg)
Performance
- Horse Power/Weight Ratio 0.231
- Wing Loading 31.1lbs/ft2 (151.6kg/m2)
- Wing Area 236.8ft2 (22.0m2)
- Drag Points 7934
Parts
- Number of Parts 74
- Control Surfaces 5
- Performance Cost 347
