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AIRCRAFT HARDWARE COMPONENT ROTABILITY CLASSIFICATION USING MACHINE LEARNING

Application US20260079985A1 Kind: A1 Mar 19, 2026

Inventors

Shivam Sharma, James E. Allman, JR., Sean M. Lanagan, John P. Herrman, Heather O. Levesque

Abstract

An application extracts a plurality of features of a hardware component of an aircraft. The application inputs a first subset of features of the plurality of features into a first machine learning model, and receives as output a first determination of whether the hardware component is rotable. The application inputs a second subset of features of the plurality of features into a second machine learning model, and receives as output a second determination of whether the hardware component is rotable. The applications determines, based on the first determination and the second determination, a final determination of whether the hardware component is rotable, and adds a data structure for the hardware component with the final determination in a searchable database. The application receives a query from a user that is associated with the hardware component, runs a search, outputs whether the hardware component is rotable.

CPC Classifications

G06F 16/3347 G06F 16/316 G06F 16/353 G06F 30/27 G06N 5/04 G06N 20/00

Filing Date

2025-09-23

Application No.

19337630