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Procedure for Failure Mode, Effects, and Criticality Analysis (FMECA)This document provides guidelines for the accomplishment of Failure Mode, Effects, and Criticality Analysis (FMECA) on the Apollo program. It is a procedure for analysis of hardware items to determine those items contributing most to system unreliability and crew safety problems.
Document ID
19700076494
Acquisition Source
Headquarters
Document Type
Technical Memorandum (TM)
Date Acquired
August 5, 2013
Publication Date
August 1, 1966
Subject Category
Quality Assurance And Reliability
Report/Patent Number
HQ-E-DAA-TN44397
RA-006-013-1A
NASA-TM-X-65227
Accession Number
70N76197
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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