| CPC B64D 45/04 (2013.01) [B64C 25/28 (2013.01); B64C 25/30 (2013.01); B64C 29/00 (2013.01); B64D 27/24 (2013.01); B64D 2045/008 (2013.01)] | 20 Claims |

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1. A system for monitoring impact on an aircraft, the system comprising:
a flight component;
a strain gauge connected to the flight component, wherein the strain gauge is configured to measure impact data associated with the flight component during each landing by the aircraft; and
a computing device communicably coupled to the strain gauge and configured to:
determine a hazardous instance for the flight component based on an impact threshold and a change in the impact data measured over a plurality of landings by the aircraft,
determine an alert based on the hazardous instance, and
initiate display of the alert on a graphical user interface.
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