Detailed profile for this aircraft model.
C-26A is a airplane model with turboprop engine(s).
ICAO: -
IATA: -
Engine Count: 2
Vmo: 248 knot
Va: 174 knot
Vfe: 156 knot
Vlo: 176 knot
Vle: 176 knot
MTW: 5715 kilogram
MTOW: 5670 kilogram
MLW: 5670 kilogram
Fuel capacity: 2453 litre
Maximum operating altitude: 31000 foot
