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Bell 429
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BHT-429-MPI
Table1.ConditionalInspections-FlightThroughHail(continued)
INITIAL
DATAREFERENCEINSPECTIONTASKDESCRIPTION
MECHOTHER
BHT-ALL-SRM,Chapter
2,StructuralRepairManual
1.Visuallyexaminethedoorsforcracks,dents,tears,punctures,impact
damage,andconditionofthepaint.Payextraattentiontothecrewdoors.
2.Visuallyexaminethewindowsforcrazing,cracks,shattering,and
impactdamage.Payextraattentiontothewindshield,crewdoor
windows,andchinbubbles.
429-MM,Chapter62MAINROTOR
1.Visuallyexaminethemainrotorbladesforcracks,dents,tears,
impactdamage,andconditionofthecoating.Payextraattentiontothe
leadingedgeabrasionstrips,tipcaps,andupperskins.Ifdelaminationis
suspected,examinethebladesforvoids.
2.Ifanydamageisfoundonthemainrotorblades,dothefollowing:
a.Removethemainrotorblades.
b.AttachaTHISCOMPONENTWASREMOVEDFROMSERVICE
BECAUSEOFAFLIGHTTHROUGHHAILtagoneachmainrotorblade.
c.Sendthemainrotorbladestoanapprovedfacilityforfurtherinspection
andrepair.
3.Ifnodamageisfoundonthemainrotorblades,thebladesare
serviceable.
4.Visuallyexaminethemainrotorhubassemblyforcracks,dents,tears,
impactdamage,andconditionofthecoating.Payextraattentiontothe
exposedareasoftheyokeassemblies,gripassemblies,andupper
mountassembly.
5.Ifanydamageisfoundonthemainrotorhubassembly,dothe
following:
a.Removethemainrotorhubassembly.
b.AttachaTHISCOMPONENTWASREMOVEDFROMSERVICE
BECAUSEOFAFLIGHTTHROUGHHAILtagonthemainrotorhub
assembly.
429-MM,Chapter62
c.Disassemble,clean,anddoadetailedinspectionofthemainrotor
hubassembly.
6.Ifnodamageisfoundonthemainrotorhubassembly,themainrotor
hubassemblyisserviceable.
7.Visuallyexaminethemainrotorcontrolsforimpactdamageand
replaceanyunserviceablepartsasrequired.
429-MM,Chapter64TAILROTOR
1.Visuallyexaminethetailrotorbladesforcracks,dents,tears,impact
damage,andconditionofthecoating.Payextraattentiontotheleading
edgeabrasionstrips.Ifdelaminationissuspected,examinetheblades
forvoids.
2.Ifanydamageisfoundonthetailrotorblades,dothefollowing:
a.Removethetailrotorhubandbladeassemblies.
b.AttachaTHISCOMPONENTWASREMOVEDFROMSERVICE
BECAUSEOFAFLIGHTTHROUGHHAILtagonthetailrotorhub
assembliesandoneachtailrotorblades.
c.Sendthetailrotorbladestoanapprovedfacilityforfurtherinspection
andrepair.
429-MM,Chapter64
d.Disassemble,clean,anddoadetailedinspectionofthetailrotorhub
assemblies.
3.Ifnodamageisfoundonthetailrotorblades,thetailrotorhuband
bladeassembliesareserviceable.
429-A-05-50-00-10A-284A-AApplicableto:ALL
Page2Issue1-10JAN2019
ECCNEAR99

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