BHT-429-MPI
ConditionalInspections-LightningStrike
Table1.ConditionalInspections-LightningStrike
INITIAL
DATAREFERENCEINSPECTIONTASKDESCRIPTION
MECHOTHER
DATE:
W.O.
FACILITY:
HELICOPTERS/N:
REGISTRYNO.:
TOTALTIME:
SIGNATURE:
NOTE
Iftheinformationcontainedinthefollowingconditionalinspection
doesnotfullyreecttheoccurrenceorifadditionalinformationor
claricationisrequired,pleasecontactProductSupportEngineer-
ingforassistance.
Becauselightningbehaviorisdifculttopredict,doafullinspection
ofthehelicopter.Lightningdamagecanshowasburnmarks,heat
discoloration,arcmarks,orassmallweldmarks(wherethemetalhas
meltedandbecomesolidagain).Honeycombandothercomposite
materialsmayshowsignsofdelamination.Localizedpaintremovalin
compositematerialsmayindicatedamagetotheexpandedcopperfoil
protection.
NOTE
Inallinstancesbelow,ifdamageisfoundinanyarea,extendthe
inspectioninthoseareasuntilnomoredamageisfound.Ifany
componentshowssignsofarcburns,discardthecomponent.
Useamagnetometerwitharangenolargerthan±5gauss.Putthe
arroworthereddot(dependingonthemagnetometermodel)within0.5
inch(13mm)ofthecomponentyouarechecking.Pointthearrowatthe
component.Ifpartsofanycomponenthaveareadingthatisgreaterthan
1gauss,degaussthesecomponents.
1.Ifahelicopterlightningstrikeisreportedorsuspected,doavisual
inspectionofthehelicopterasfollows:
a.Visuallyexaminethefollowingcomponentsforsignsofarcing,
burning,andcondition,speciallyintheareaaroundthemountingbolts
andelectricalbondingstraps:
429-MM,Chapter62
•Mainrotorhubandbladeassembly
429-MM,Chapter63
•Transmissionandmastassembly
•Pylonbeamassemblies,verticalLiquidInertialVibrationEliminator
(LIVE)mounts,andpitchrestraintspringassemblies
•Engine-to-transmissiondriveshafts
429-MM,Chapter67
•Flightcontrols
429-MM,Chapter71
•Enginesandenginemounts
429-MM,Chapter65•T ailrotordriveshaftassembly
•T ailrotorgearboxandattachmentstothetailrotorgearboxsupport
429-MM,Chapter64
•T ailrotorhubandbladeassemblies
Applicableto:ALL429-A-05-50-00-08A-284A-A
ECCNEAR99
10JAN2019-Issue1Page1