Detailed profile for this aircraft model.
DH.125 Series 1A is a airplane model with turbojet engine(s).
ICAO: -
IATA: -
Engine Count: 2
Fuel capacity: 4662 litre
MLW: 8868 kilogram
MTOW: 9616 kilogram
MZFW: 5897 kilogram
Maximum operating altitude: 40000 foot
Mmo: 0.735
Va: 181 knot
Vfe: 145 knot
Vle: 210 knot
Vlo: 210 knot
Vmca: 98 knot
Vmo: 290 knot
