Detailed profile for this aircraft model.
U-125A is a airplane model with turbofan engine(s).
ICAO: -
IATA: -
Engine Count: 2
Fuel capacity: 5659 litre
MLW: 10591 kilogram
MTOW: 12428 kilogram
MTW: 12483 kilogram
MZFW: 7947 kilogram
Maximum operating altitude: 41000 foot
Mmo: 0.8
Va: 196 knot
Vfe: 165 knot
Vle: 220 knot
Vlo: 220 knot
Vmca: 108 knot
Vmo: 280 knot
