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FAA AC 25-24:2000

FAA AC 25-24:2000 Sustained Engine Imbalance Gives acceptable means, but not the only means, of demonstrating compliance with the provisions of 14 CFR part 25 related to the aircraft design for sustained engine rotor imbalance conditions.

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Table of Contents

1PURPOSE
2RELATEDDOCUMENTS
3DEFINITIONS
4BACKGROUND
5EVALUATIONOFTHEWINDMILLINGIMBALANCECONDITIONS
6ANALYSISMETHODOLOGY
7MATHEMATICALMODELING
8VALIDATION
9HIGHPOWERIMBALANCECONDITION

Abstract

Gives acceptable means, but not the only means, of demonstrating compliance with the provisions of 14 CFR part 25 related to the aircraft design for sustained engine rotor imbalance conditions.

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