Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:military
|
| gptkbp:appliesTo |
gptkb:aircraft
military systems |
| gptkbp:cancellationDate |
4 August 1998
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:fullName |
Procedures for Performing a Failure Mode, Effects and Criticality Analysis
|
| gptkbp:issuedBy |
gptkb:United_States_Department_of_Defense
|
| gptkbp:language |
English
|
| gptkbp:publicationDate |
24 November 1980
|
| gptkbp:replacedBy |
MIL-STD-1629
industry standards such as SAE J1739 and IEC 60812 |
| gptkbp:status |
cancelled
|
| gptkbp:subject |
gptkb:Failure_Mode_and_Effects_Analysis
Criticality Analysis |
| gptkbp:usedFor |
risk assessment
reliability engineering system safety |
| gptkbp:bfsParent |
gptkb:Fault_Tree_Analysis
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
MIL-STD-1629A
|