Disclosed is a landing gear controller for an aircraft. The controller is configured to: detect an extension time for a landing gear, and if the detected extension time meets a predetermined criterion, provide a warning signal to indicate potential failure of a landing gear uplock hook. Also disclosed is a landing gear system, a method to detect failure of a landing gear uplock hook, and an aircraft.
LANDING GEAR CONTROLLER
FAHRWERKSREGLER
ORGANE DE COMMANDE DE TRAIN D'ATTERRISSAGE
2024-02-28
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |