A method for determining failure conditions associated with aircraft installed line-replaceable-units, the method comprising: receiving, by a remote computing system , first operational data collected by a first line-replaceable-unit of a first aircraft during flight operations of the first aircraft, the first operational data including information associated with detection of one or more single event upsets detected by the first line-replaceable unit, the first operational data further including information pertaining to a parameter or environmental condition associated with an operating environment of the first line-replaceable-unit during the flight operations of the first aircraft; receiving, by the remote computing system, second operational data collected by at least one second line-replaceable-unit (10B-10N) of at least one second aircraft (5B-5N) during flight operations of the at least one second aircraft, the second operational data including information associated with detection of one or more single event upsets detected by the second at least one line-replaceable unit, the second operational data further including information to parameter or environmental condition associated with an operating environment of the at least one second line-replaceable-unit during the flight operations of the at least one second aircraft, the at least one second line-replaceable-unit being a same type of line-replaceable-unit as the first line-replaceable unit of the first aircraft and the second operational data being a same type of operational data as the first operational data; predicting, by the remote computing system, based at least in part on the first operational data and the second operational data, a failure condition associated with the first line-replaceable-unit of the first aircraft; and outputting, by the remote computing system, for display at a graphical user interface associated with the remote computing system, an indication of the failure condition. receiving, by a remote computing system , first operational data collected by a first line-replaceable-unit of a first aircraft during flight operations of the first aircraft, the first operational data including information associated with detection of one or more single event upsets detected by the first line-replaceable unit, the first operational data further including information pertaining to a parameter or environmental condition associated with an operating environment of the first line-replaceable-unit during the flight operations of the first aircraft; receiving, by the remote computing system, second operational data collected by at least one second line-replaceable-unit (10B-10N) of at least one second aircraft (5B-5N) during flight operations of the at least one second aircraft, the second operational data including information associated with detection of one or more single event upsets detected by the second at least one line-replaceable unit, the second operational data further including information to parameter or environmental condition associated with an operating environment of the at least one second line-replaceable-unit during the flight operations of the at least one second aircraft, the at least one second line-replaceable-unit being a same type of line-replaceable-unit as the first line-replaceable unit of the first aircraft and the second operational data being a same type of operational data as the first operational data; predicting, by the remote computing system, based at least in part on the first operational data and the second operational data, a failure condition associated with the first line-replaceable-unit of the first aircraft; and outputting, by the remote computing system, for display at a graphical user interface associated with the remote computing system, an indication of the failure condition. <EOS>