A systematic, analytical methodology for aircraft system safety assessment is explained. A try-out on a software controlled digital avionics system is summarized. Analysis of software components is emphasized. It is concluded that the same methodology can be applied to software and hardware. Conditions that have to be met to perform a successful hardware/software safety assessment are described.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Hardware/Software Failure Mode Effect Analysis (FMEA) Applied to Airplane Safety


    Contributors:

    Publication date :

    1984


    Size :

    9 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English