EasyManua.ls Logo

Bell 429 - Page 152

Bell 429
192 pages
Print Icon
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
BHT-429-MPI
Table1.ConditionalInspections-SuddenStoppage(TailRotor)PowerONorOFF(continued)
INITIAL
DATAREFERENCEINSPECTIONTASKDESCRIPTION
MECHOTHER
Bentorbrokenpitchchangecontroltube
Damagetotheoutputshaftofthetailrotorgearbox
3.Discardalltherotatingcontrolboltsatthetailrotorhubandblade
assemblies.
4.Ifthevisualinspectionshowsnosignsofdamage,thedirectional
controlsareserviceable.
TAILROTOR
429-MM,Chapter64
1.Ifthesuddenstoppageistheresultofatailrotorbladestrike,discard
bothtailrotorhubandbladeassemblies.
2.Ifthesuddenstoppageoccurredatthemainrotor,transmission
assembly,tailrotordriveshaft(s),ortailrotorgearbox,doavisual
inspectionofthetailrotorasfollows:
a.Visuallyexaminebothtailrotorhubandbladeassembliesforexternal
damage.
b.Ifdamageisfoundonanyofthetailrotorhubandbladeassemblies,
removebothtailrotorhubandbladeassemblies.
c.AttachaTHISCOMPONENTWASREMOVEDFROMSERVICE
BECAUSEOFASUDDENSTOPPAGEtagonbothtailrotorhuband
bladeassemblies.
429-MM,Chapter64429-MM,
Chapter65
d.Disassemble,clean,anddoadetailedinspectionofbothtailrotor
hubandbladeassemblies.
e.Ifnodamageisfound,thetailrotorhubandbladeassembliesare
serviceable.
429-MM,Chapter53TAILBOOM
1.Visuallyexaminetheinternalandexternalareasofthetailboom
assemblyforcondition.
2.Examinethehangerbearingandsnubbersupportsforconditionand
securityofattachment.
3.Examinethehorizontalstabilizersandtheauxiliarynassembliesfor
conditionandsecurityofattachment.
4.Examinetheverticalnassemblyforconditionandsecurityof
attachment.
429-MM,Chapter65
5.Doadetailedinspectionofthetailrotorgearboxmountingstudsand
dowelpinsforcrackswitha10xmagnifyingglassorusingaFluorescent
PenetrantInspection(FPI).
6.Visuallyexaminetheattachinghardwarebetweentheaft
fuselage-to-tailboomandtailboom-to-aftfuselageframes,atFS361.00,
forconditionandsecurity.
7.Doatorquecheckofthetailboomattachments.
8.Doaatnesscheckoftheaftfuselage-to-tailboomandtailboom-to-aft
fuselageframes,atFS361.00.ContactProductSupportEngineering
forinformationconcerningtheapplicableproceduresandassociated
equipment.
429-A-05-50-00-02A-284A-AApplicableto:ALL
Page4Issue1-10JAN2019
ECCNEAR99

Table of Contents

Related product manuals