Detailed profile for this aircraft model.
DH.125 Series 1A/S-522 is a airplane model with turbojet engine(s).
ICAO: -
IATA: -
Engine Count: 2
Fuel capacity: 4662 litre
MLW: 8868 kilogram
MTOW: 9843 kilogram
MZFW: 6123 kilogram
Maximum operating altitude: 40000 foot
Mmo: 0.765
Va: 185 knot
Vfe: 145 knot
Vle: 210 knot
Vlo: 210 knot
Vmca: 93 knot
Vmo: 285 knot
