Procedure for Failure Mode, Effects, and Criticality Analysis (FMECA) (original) (raw)

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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.

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-TN44397RA-006-013-1ANASA-TM-X-65227Report Number: HQ-E-DAA-TN44397Report Number: RA-006-013-1AReport Number: NASA-TM-X-65227

Accession Number

70N76197

Distribution Limits

Public

Copyright

Work of the US Gov. Public Use Permitted.

Available Downloads

NameType 19700076494.pdf STI

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