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MIL-HDBK-189 Appendix C / 189C Table VI: Crow-AMSAA fit to 27 failures of two prototypes, time terminated at 300 h
| Tool | Reliability Growth |
| Source | U.S. Department of Defense (1981). Reliability Growth Management. MIL-HDBK-189, 13 February 1981. Appendix C, Sections 20.1.3 and 20.2.1.4; and (2011). MIL-HDBK-189C, 14 June 2011. Table VI. |
| Level | Professional |
Problem
Two prototypes tested concurrently with design changes accumulated 27 failures at the combined times 2.6, 16.5, 16.5, 17.0, 21.4, 29.1, 33.3, 56.5, 63.1, 70.6, 73.0, 77.7, 93.9, 95.5, 98.1, 101.1, 132.0, 142.2, 147.7, 149.0, 167.2, 190.7, 193.0, 198.7, 251.9, 282.5 and 286.1 hours before the test stopped at 300 hours. Fit the Crow-AMSAA (NHPP) model, test its fit by the Cramér–von Mises statistic, and give the current MTBF with a 90 % interval.
Inputs to Enter
- Cumulative failure times (loaded by default), time terminated at T = 300 hours
- Confidence 90 %, goodness-of-fit significance 0.05
Answers
- β̂ = 0.716, λ̂β̂ = 0.325 (intensity 0.325 t^−0.284); ρ(300) = 0.0645 failures per hour, MTBF 15.5 hours; cumulative MTBF 300/27 = 11.1 hours
- Unbiased β̄ = (N − 1)β̂/N = 0.690; Cramér–von Mises C² = 0.091 against the critical 0.218 (Table C-II, M = 27, α = 0.05): model accepted
- 90 % interval on the MTBF from Table C-I (L 0.636, U 1.682): 9.9 to 26.1 hours
Notes
The tool's default data and termination are this example; press Submit. MIL-HDBK-189C §6.2.2.9 quotes F = 45 and β̂ = 0.826 for Table VI, which prints these 27 times; the 1981 values above are the ones the data give.
More Examples for This Tool
- MIL-HDBK-189 Appendix C 20.2.2.4: failure-terminated tank test, 26 failures in miles
- MIL-HDBK-189C Table VII: Crow-AMSAA fit to grouped aircraft failure counts
- ReliaSoft reference: Crow-AMSAA on 22 failure times, failure terminated at 620 h, with Fisher and Crow bounds
- ReliaSoft reference: six systems tested concurrently, equivalent single system and projection to 3,000 h