RTCA DO 160:2010

RTCA DO 160:2010 Environmental Conditions And Test Procedures For Airborne Equipment Defines standard procedures and environmental test criteria for testing airborne equipment for the entire spectrum of aircraft from light, general aviation aircraft and helicopters through the "jumbo

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Table of Contents

Foreword
TableofContents
Section1.0Purposeandapplicability
Section2.0Definitionsofterms-general
Section3.0Conditionsoftests
Section4.0Temperatureandaltitude
Section5.0Temperaturevariation
Section6.0Humidity
Section7.0Operationalshocksandcrashsafety
Section8.0Vibration
Section9.0Explosionproofness
Section10.0Waterproofness
Section11.0Fluidssusceptibility
Section12.0Sandanddust
Section13.0Fungusresistance
Section14.0Saltspray
Section15.0Magneticeffect
Section16.0Powerinput
Section17.0Voltagespike
Section18.0Audiofrequencyconductedsusceptibility-
powerinputs
Section19.0Inducedsignalsusceptibility
Section20.0Radiofrequencysusceptibility(radiated
andconducted)
Section21.0Emissionofradiofrequencyenergy
Section22.0Lightninginducedtransientsusceptibility
Section23.0Lightningdirecteffects
Section24.0Icing
AppendixAEnvironmentaltestidentification
AppendixBMembership
AppendixCChangeCoordinatorsandAssignments

Abstract

Defines standard procedures and environmental test criteria for testing airborne equipment for the entire spectrum of aircraft from light, general aviation aircraft and helicopters through the "jumbo jets" and SST categories of aircraft.

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