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

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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