Abstract: A cargo door for an aircraft having a plurality of locking devices spaced near an edge of the cargo door, at least one vent panel, a control handle, and a torsion shaft actuating a plurality of pins to lock and unlock the plurality of locking devices is provided. A first drive connects the control handle to the torsion shaft to rotate the torsion shaft following a locking or unlocking command imparted to the control handle. A second drive connects the torsion shaft to the at least one vent panel to open or close the at least one vent panel following a rotation of the torsion shaft. The torsion shaft is a double shaft having two coaxial and rotationally integral shafts, namely an inner control shaft and an outer tubular control shaft.

Abstract: Door for cargo airplane, wherein a cargo compartment is accessible from the outside of the fuselage through an opening for loading goods provided with the door. The door is provided with a first operating handle accessible from the outside of the door and used to lock/unlock the pins that are used to connect the door to the fuselage and control the closing/opening of a ventilation door; and a second operating handle accessible from the outside of the door for advancing/retracting the pins in/from respective seats. According to the invention, the door is provided with a third handle accessible from the inside of the door and mechanically interconnected with the first handle for locking/unlocking the pins and controlling the closing/opening of the ventilation door; and a fourth operating handle accessible from the inside of the door and mechanically interconnected with the second handle for advancing/retracting the pins in/from respective seats.

Abstract: Door for cargo airplane, wherein a cargo compartment is accessible from the outside of the fuselage through an opening for loading goods provided with the door. The door is provided with a first operating handle accessible from the outside of the door and used to lock/unlock the pins that are used to connect the door to the fuselage and control the closing/opening of a ventilation door; and a second operating handle accessible from the outside of the door for advancing/retracting the pins in/from respective seats. According to the invention, the door is provided with a third handle accessible from the inside of the door and mechanically interconnected with the first handle for locking/unlocking the pins and controlling the closing/opening of the ventilation door; and a fourth operating handle accessible from the inside of the door and mechanically interconnected with the second handle for advancing/retracting the pins in/from respective seats.