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Structural Fatigue and Other Airworthiness Aspects

Published online by Cambridge University Press:  04 July 2016

J. K. Williams
J. K. Williams*
Affiliation:
Air Registration Board
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Extract

In this paper the emphasis is on safety problems connected with the use of light fixed-wing aircraft for agricultural purposes. Most of the aircraft concerned are between 2000 and 6000 lb all-up weight and are single piston-engined types. About 97 per cent of all hours flown in agricultural aviation all over the world are by such small fixed-wing aircraft, the remainder by larger aircraft such as the DC-3 and helicopters.

The mass of statistics available on this type of flying is therefore confined to the small fixed-wing aircraft and since this type is obviously the most important with respect to this activity, then it is appropriate to concentrate on this type.

Information

Type
Requirements for Agricultural Aircraft – Pilot's Viewpoint and Engineering Aspects
Information
The Aeronautical Journal , Volume 67 , Issue 636 , December 1963, pp. 776 - 782
Copyright
Copyright © Royal Aeronautical Society 1963

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References

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