Classify the failure effects by severity.Identify failure modes (piece-part level or functional).Define ground rules and assumptions in order to help drive the design.By RAC CRTA–FMECA, the FMECA analysis procedure typically consists of the following logical steps: Slight differences are found between the various FMECA standards. MIL–STD–1629A was canceled without replacement in 1998, but nonetheless remains in wide use for military and space applications today. In 1980, MIL–STD–1629A replaced both MIL–STD–1629 and the 1977 aeronautical FMECA standard MIL–STD–2070. The British Standards Institute published BS 5760–5 in 1991 for the same purpose. The International Electrotechnical Commission published IEC 812 (now IEC 60812) in 1985, addressing both FMEA and FMECA for general use. Model, and by the 1980s FMEA was gaining broad use in the automotive industry. The civil aviation industry now tends to use a combination of FMEA and Fault Tree Analysis in accordance with SAE ARP4761 instead of FMECA, though some helicopter manufacturers continue to use FMECA for civil rotorcraft.įord Motor Company began using FMEA in the 1970s after problems experienced with its Pinto In 1967 the Society for AutomotiveĮngineers released the first civil publication to address FMECA. Īt the same time as the space program developments, use of FMEA and FMECA was already Possibly because MIL–P–1629 was replaced by MIL–STD–1629 (SHIPS) in 1974, development of FMECA is sometimes incorrectly attributed to NASA. FMECA was subsequently used on other NASA programs including Viking, Voyager, Magellan, and Galileo. In 1966 NASA released its FMECA procedure for use on the Apollo program. National Aeronautics and Space Administration (NASA) were using variations of FMECA under a variety of names. By the early 1960s, contractors for the U.S. FMECA tends to be preferred over FMEA in space and North Atlantic Treaty Organization (NATO) military applications, while various forms of FMEA predominate in other industries.įMECA was originally developed in the 1940s by the U.S military, which published MIL–P–1629 in 1949. The result highlights failure modes with relatively high probability and severity of consequences, allowing remedial effort to be directed where it will produce the greatest value. FMECA extends FMEA by including a criticality analysis, which is used to chart the probability of failure modes against the severity of their consequences. Systematic technique for failure analysisįailure mode effects and criticality analysis ( FMECA) is an extension of failure mode and effects analysis (FMEA).įMEA is a bottom-up, inductive analytical method which may be performed at either the functional or piece-part level.
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