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A new helicopter system is under development. System failure data has been collected on five helicopters during the final test phase. The actual failure times cannot be determined since the failures are not discovered until after the helicopters are brought into the maintenance area. However, total flying hours are known when the helicopters are brought in for service and every two weeks, each helicopter undergoes a thorough inspection to uncover any failures that may have occurred since the last inspection. Therefore, the cumulative total number of flight hours and the cumulative total number of failures for the five helicopters are known for each two-week period. The total number of flight hours from the test phase is 500, which was accrued over a period of 12 weeks (6 2-week intervals). For each 2-week interval, the total number of flight hours and total number of failures for the five helicopters were recorded. The grouped data set is displayed in Table 5.3.
Table 5.3 - Grouped data for a new helicopter system
Interval |
Interval Length |
Failures In Interval |
1 |
0 - 62 |
12 |
2 |
62 -100 |
6 |
3 |
100 - 187 |
15 |
4 |
187 - 210 |
3 |
5 |
210 - 350 |
18 |
6 |
350 - 500 |
16 |
and: 
Crow confidence bounds can also be obtained on the parameters
and
at the
90% confidence level, as:
and: 
and: 
Figures 5.10 and 5.11 show plots of the Fisher Matrix confidence bounds for the cumulative and instantaneous MTBF.

Figure 5.10: Cumulative MTBF with 2-sided 90% Fisher Matrix confidence bounds |

Figure 5.11: Instantaneous MTBF with 2-sided 90% Fisher Matrix confidence bounds |
The Crow confidence bounds for the cumulative and instantaneous MTBF at the 90% 2-sided confidence level and for T = 500 hours are:
and: 
Figures 5.12 and 5.13 show plots of the Crow confidence bounds for the cumulative and instantaneous MTBF.

Figure 5.12: Cumulative MTBF with 2-sided 90% Crow confidence bounds |

Figure 5.13: Instantaneous MTBF with 2-sided 90% Crow confidence bounds |