An indicator assembly (300) for an aircraft landing gear for providing indication of a hard landing. The indicator assembly including an actuator member (314) pivotably movable when the pressure on a shock strut of the aircraft landing gear exceeds a desired load and stroke threshold indicative of a hard landing. A shear pin (306) is coupled to the actuator member which is configured to shear when a desired level of force is applied to at least a portion of the shear pin. A visibly recognizable indicator (308) is moved from a non-indicating position to an indicating position upon shearing of the shear pin.
SYSTEM FOR INDICATING AN AIRPLANE HARD LANDING
SYSTEM ZUR ANZEIGE EINER HARTEN FLUGZEUGLANDUNG
SYSTÈME POUR INDIQUER UN ATTERRISSAGE BRUTAL D'AVION
2017-06-21
Patent
Electronic Resource
English
Engineering Index Backfile | 1931
|TIBKAT | 1931
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