A locking system for an aircraft door having a door handle housing to mount to the aircraft door; a locking mechanism supported by the door handle housing; an exterior handle and an interior handle each to manipulate the locking mechanism. The locking mechanism having a door gear axis to rotate via operation of the interior handle and the exterior handle to lock and unlock the locking mechanism; and a locking pin extending from the door gear axis and into a chamber of the door handle housing, the locking pin having a first position and a second position, the first position of the locking pin blocks rotation of the door gear axis and the second position of the locking pin allows rotation of the door gear axis. The locking pin is moveable from the first position to the second position via operation of the interior handle and the exterior handle.
Locking System for an Aircraft Door
03.04.2025
Patent
Elektronische Ressource
Englisch
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