Detailed profile for this aircraft model.
333 (269D-A) is a helicopter model with turboshaft engine(s).
ICAO: -
IATA: -
Engine Count: 1
Fuel capacity: 227 litre
Height: 2.61 metre
Length: 9.42 metre
MLW: 1157 kilogram
MTOW: 1157 kilogram
Main rotor blades: 3
Main rotor count: 1
Main rotor diameter: 8.18 metre
Maximum operating altitude: 13000 foot
Tail rotor blades: 2
Tail rotor count: 1
Tail rotor diameter: 1.3 metre
Vne: 110 knot
Width: 2.08 metre
