An assembly (70, 72) for an aircraft propulsion system (20) includes a propulsor section (28) for the aircraft propulsion system (20), a plurality of imaging devices (98), and a controller (96). The propulsor section (28) includes a propulsor (40). The propulsor (40) includes a plurality of propulsor blades (46). The plurality of imaging devices (98) are mounted in the propulsor section (28). Each imaging device (98) includes a camera (108). The controller (96) includes a processor (102) in communication with a non-transitory memory (104) storing instructions, which instructions when executed by the processor (102), cause the processor (102) to: control the camera (108) of each imaging device (98) of the plurality of imaging devices (98) to capture image data (146) of each propulsor blade (148) of the plurality of propulsor blades (46) and identify a presence or an absence of damage for each propulsor blade (148) of the plurality of propulsor blades (46) using the image data (146) from the camera (108) of two or more imaging devices (98) of the plurality of imaging devices (98).