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FAA AC 33.4-3:2005

FAA AC 33.4-3:2005 Instructions For Continued Airworthiness; Aircraft Engine High Intensity Radiated Fields (hirf) And Lightning Protection Features Gives guidance and acceptable methods, but not the only methods, that may be used to demonstrate compliance for aircraft engines with Section 33.4, Instructions for Continued Airworthiness (ICA), of T

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Table of Contents

1PURPOSE
2APPLICABILITY
3RELATEDREGULATIONS
4RELATEDREADINGMATERIAL
5BACKGROUND
6GENERAL
7ICATASKS-HIRFANDLIGHTNINGPROTECTIONFEATURES
8TYPICALINSPECTION/MAINTENANCEFUNCTIONELEMENTS
9VALIDATIONOFINSPECTION/MAINTENANCEFUNCTIONSAND
DETERMINATIONOFTHEIREFFECTIVENESS
APPENDIX1AVERAGESYSTEMFAILURERATE

Abstract

Gives guidance and acceptable methods, but not the only methods, that may be used to demonstrate compliance for aircraft engines with Section 33.4, Instructions for Continued Airworthiness (ICA), of Title 14 of the Code of Federal Regulations. Provides guidance for developing ICA to ensure the continued airworthiness of aircraft engine HIRF and lightning protection features.

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