Comparative evaluation of landing safety of AN-100-124 aircraft in two landing configurations

Aviation technics and technology


Аuthors

Sharov V. D.

Abstract

In this article there are presented the results of research of comparative evaluation of landing safety of AN-124-100 in landing configuration 30/17 и 40/17 for the purpose of approving an acceptable risk level of landing in configuration 40/17 and for approving a practicability of certification of this aircraft for usage in airlines in both of these two configurations.

Keywords:

flight safety, risk.


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