A hard landing indicator assembly (202) is disclosed herein. The hard landing indicator assembly includes a pressure relief valve (230), a hydraulic tube (232) having a first end and a second end, the first end coupled to the pressure relief valve (230), and a plunger (238) having a top portion and a shaft (23 8b), the plunger disposed in the hydraulic tube (232), wherein a portion of the shaft (23 8b) is a hard landing indicator (234) that extends outward from the hydraulic tube (232) in response to a hard landing event.
AIRCRAFT HARD LANDING INDICATOR
INDIKATOR FÜR HARTE LANDUNGEN IN FLUGZEUGEN
INDICATEUR D'ATTERRISSAGE DUR POUR AVION
2024-06-12
Patent
Electronic Resource
English