2.3.2 - Reliability Maintainability Availability

2.3.2-10 Level 2 Tasks

Tasks Applicable Mission Phases Description SFWC Artifacts References
2.3.2-10-1 Ensure that test failure analysis and corrective action reports are adequate and complete and drive to root cause Phase B | Phase C | Phase D1 | Phase D2 | Ensure that the Failure Reporting and Corrective Action System (FRACAS) meet contractual requirements; root cause analysis is complete for all critical performance anomalies; and current mission impact determined. Ensure corrective action/technical solution is implemented. SFWC 2.2.4.3, SFWC 2.7.1, SFWC 2.7.2, SFWC 2.7.3, SFWC 2.7.4 NA Mission Assurance Guide, TOR-2007(8546)-6018, Rev B, Reliability Chapter; Space Vehicle Systems Engineering Handbook, TOR-2006(8506)-4494,Chapter 21; SMC-S-013, Reliability Program for Space Systems, 13 June 2008 (also published as TOR-2007(8583)-6889 under same title) or equivalent
2.3.2-10-2 Ensure the Corrective Action Boards (CABs) process is documented and executed Phase C | Phase D1 | Phase D2 | Phase D3 | Ensure appropriate technical solution is determined for implementation and corrective actions applicable to the system are completed. SFWC 2.2.3.3, SFWC 2.2.4.3, SFWC 2.4.2.1.1, SFWC 2.7.1, SFWC 2.7.2, SFWC 2.7.3, SFWC 2.7.4 NA SMC-S-013, Reliability Program for Space Systems, 13 June 2008 (also published as TOR-2007(8583)-6889 under same title) or equivalent
2.3.2-10-3 Ensure that failures at subcontractors are properly evaluated and resolved Phase C | Phase D1 | Phase D2 | Ensure the flow-down of the failure review and corrective action system (FRACAS) requirements to all supplier/subcontractors who are involved in the design, test, production, or operations of the program. The contractor should ensure the subcontractor/supplier provides recurring feedback regarding the status and changes to their FRACAS process. SFWC 2.2.4.3 NA Mission Assurance Guide, TOR-2007(8546)-6018, Rev B, Reliability Chapter; Space Vehicle Systems Engineering Handbook, TOR-2006(8506)-4494, Reliability Engineering chapter; SMC-S-013, Reliability Program for Space Systems, 13 June 2008 (also published as TOR-2007(8583)-6889 under same title) or equivalent
2.3.2-10-4 Ensure that End-Item Data Packages adequate address reliability requirements compliance and closure of test failure reports Phase D1 | Ensure that all test failure reports are complete with a good description of the failure, failure analysis and adequately identify root cause and corrective action. SFWC 2.2.4.3 NA Mission Assurance Guide, TOR-2007(8546)-6018, Rev B, Reliability Chapter; Space Vehicle Systems Engineering Handbook, TOR-2006(8506)-4494, Reliability Engineering chapter