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MIL-HDBK-189 Appendix C 20.2.2.4: failure-terminated tank test, 26 failures in miles
| Tool | Reliability Growth |
| Source | U.S. Department of Defense (1981). Reliability Growth Management. MIL-HDBK-189, 13 February 1981. Appendix C, Section 20.2.2.4, and Tables C-II and C-III. |
| Level | Professional |
Problem
A tank failed at the cumulative mileages 1, 57, 187, 252, 310, 485, 693, 720, 727, 779, 1,028, 1,561, 1,766, 1,793, 1,938, 2,030, 2,065, 2,289, 2,423, 2,560, 2,879, 3,086, 3,456, 3,626, 4,252 and 4,582, the test ending at the last failure. Fit the Crow-AMSAA model for a failure-terminated test, check the fit at the 10 % level and give the mean miles between failures with a 95 % interval.
Inputs to Enter
- Cumulative failure times as above; termination failure terminated (T* = 4,582); unit miles
- Confidence 95 %, goodness-of-fit significance 0.10
Answers
- β̂ = 0.626, λ̂ = 0.132; intensity at the end 0.00355 per mile, mean miles between failures 281
- Cramér–von Mises 0.058 as printed (biased β̂ in the statistic); 0.0545 with β̄ as the text prescribes; both far below the critical 0.172 (M = N − 1 = 25, α = 0.10)
- 95 % interval from Table C-III (L 0.6333, U 1.919): 178 to 541 miles
Notes
Paste the 26 mileages, set the termination select to failure terminated and the unit to miles.
More Examples for This Tool
- MIL-HDBK-189 Appendix C / 189C Table VI: Crow-AMSAA fit to 27 failures of two prototypes, time terminated at 300 h
- 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