Verfahren und Vorrichtung zur Ermittlung eines Überschreitens der Belastungsgrenzen einer Flugzeugstruktur

摘要

The process involves comparing a measured effective speed of an aircraft with the maximal speed relative to actual flight configuration. A vertical load factor of the aircraft is measured, and the measured factor is compared to a limiting value of the vertical load factor. Structural inspection at the level of a aircraft structural part is to be carried out or not is determined based on the results of both the comparisons. An independent claim is also included for an aircraft.