Detailed profile for this aircraft model.
L-382J Hercules II is a airplane model with turboprop engine(s).
ICAO: -
IATA: -
Engine Count: 4
Fuel capacity: 25817 litre
MLW: 58967 kilogram
MTOW: 70670 kilogram
MTW: 70670 kilogram
MZFW: 56245 kilogram
Maximum operating altitude: 32200 foot
Vfe: 149 knot
Vle: 170 knot
Vlo: 170 knot
