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Bell 429
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BHT-429-MPI
Table1.ConditionalInspections-SuddenStoppage(TailRotor)PowerONorOFF(continued)
INITIAL
DATAREFERENCEINSPECTIONTASKDESCRIPTION
MECHOTHER
b.Cleanandexaminetheforwardandaftcompositesegmentedshaft
assembliesforcracks,voids,delamination,andloosepermanent
fasteners.
c.Ifanyoftheabovedriveshaftswasdamagedbyamainrotorblade
strikewherethebladehascontactedthetailboomorhasdamageother
thantorsionaloverload,dothefollowing:
(1)Discardthedamageddriveshaft.
(2)Discardthedriveshaftforwardand/oraftofthedamageddriveshaft,
asapplicable.
(3)Discardtheadjacentbearing(s)andhanger(s),asapplicable.
(4)Discardtheadjacentcouplingdiscpack(s),asapplicable,anddisc
packattachinghardware.
(5)Removetheremainingcomponentsbetweenthetransmissionand
thetailrotorgearbox.
(6)AttachaTHISCOMPONENTWASREMOVEDFROMSERVICE
BECAUSEOFASUDDENSTOPPAGEtagoneachofthese
components.
(7)Cleananddoadetailedinspectionofeachofthesecomponents.
d.Ifanyoftheabovedriveshaftswasdamagedbecauseoftorsional
overload,dothefollowing:
(1)Discardthedamageddriveshaft.
(2)Discardtheadjacentbearing(s)andhanger(s),asapplicable.
(3)Discardallthecouplingdiscpacksanddiscpackattachinghardware.
(4)Removetheremainingcomponentsbetweenthetransmissionand
thetailrotorgearbox.
(5)AttachaTHISCOMPONENTWASREMOVEDFROMSERVICE
BECAUSEOFASUDDENSTOPPAGEtagoneachofthese
components.
(6)Cleananddoadetailedinspectionofeachofthesecomponents.
e.Iftheinspectionshowsnosignsofdamage,thefanshaftassembly
andthesegmentedshaftassembliesareserviceable.
5.Doadetailedinspectionofthetailrotorgearboxasfollows:
a.Examinethetailrotorgearboxforcondition.Discardthetailrotor
gearboxifanyofthefollowingdamageisfound:
b.Ifthereisevidenceofacrackedordistortedhousing,fracturedstuds
ordowelpins,orbentordamagedoutputshaft,discardthetailrotor
gearbox.
c.Ifnodamageisfound,removethetailrotorgearbox.
d.AttachaTHISCOMPONENTWASREMOVEDFROMSERVICE
BECAUSEOFASUDDENSTOPPAGEtagonthetailrotorgearbox.
429-MM,Chapter65
e.Sendthetailrotorgearboxtoanapprovedrepairfacilityto
disassemble,clean,anddoadetailedinspection.
429-MM,Chapter67FLIGHTCONTROLS
1.Visuallyexaminethedirectionalcontrolsforconditionandcorrect
operation.Replacealldamagedparts.
2.Discardthepitchchangemechanismifoneormoreofthefollowing
defectsarefound:
Fractureorevidenceofyieldingonthetailrotorpitchhorn
Applicableto:ALL429-A-05-50-00-02A-284A-A
ECCNEAR99
10JAN2019-Issue1Page3

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