Assessing Helicopter Safety with Respect to Component Fatigue: A Procedure Based on Statistical Methods of Data Analysis Requiring a Catastrophic Failure Rate of less than I0–3 after 10,000 flying hours

Author： B.Sc. A.D. Hall  

Publisher： Emerald Group Publishing Ltd

ISSN： 0002-2667

Source： Aircraft Engineering, Vol.35, Iss.4, 1993-12, pp. : 97-99

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