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FAA AC 33.78-1:2000

FAA AC 33.78-1:2000 Turbine Engine Power-loss And Instability In Extreme Conditions Of Rain And Hail Gives guidance and acceptable methods, but not the only methods, that may be used to demonstrate compliance with the requirements contained under Title 14 of the Code of Federal Regulations (14 CFR),

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Table of Contents

1PURPOSE
2BACKGROUND
3DEFINITIONS
4DISCUSSION
5GENERAL
6METEOROLOGICALDATA
7RAINANDHAILCONCENTRATIONAMPLIFICATIONAND
ATTENUATIONEFFECTS
8ROTORCRAFTTURBINEENGINES
9TURBINEENGINEOPERABILITYEFFECTS
10CASECONTRACTION
11GENERAL
12DESIGNFEATURES
13OPERATIONALFACTORS
14GENERAL
15CRITICALPOINTANALYSISELEMENTS
16CRITICALPOINTANALYSISPROCEDURE
17GENERAL
18TESTPOINTSELECTION
19CRITICALPOINTTESTINGATGROUNDLEVEL
20OTHERCOMPLIANCEALTERNATIVES
21GENERAL

Abstract

Gives guidance and acceptable methods, but not the only methods, that may be used to demonstrate compliance with the requirements contained under Title 14 of the Code of Federal Regulations (14 CFR), part 33, section 33.78(a)(2), and 33.78(c).

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