BHT-429-MPI
ConditionalInspections-FlightThroughHail
Table1.ConditionalInspections-FlightThroughHail
INITIAL
DATAREFERENCEINSPECTIONTASKDESCRIPTION
MECHOTHER
DATE:
W.O.
FACILITY:
HELICOPTERS/N:
REGISTRYNO.:
TOTALTIME:
SIGNATURE:
NOTE
Iftheinformationcontainedinthefollowingconditionalinspection
doesnotfullyreecttheoccurrenceorifadditionalinformationor
claricationisrequired,pleasecontactProductSupportEngineer-
ingforassistance.
Collisionwithhailcancauseextensivedamagetothehelicopter,
suchasdenting,tearing,andpuncturingofthefuselage,blades,and
controls,shatteringofthewindshield,delaminationofthenosecap,and
instrumentdamage.Haildamageaffectslargesurfaceareasofthe
helicopter.Inmostcases,Bellrecommendsreplacementofanypart(s)
showinghaildamage.
Ifightthroughhailisreported,doaninspectionofthehelicopterforhail
damageasfollows:
429-MM,Chapter53FUSELAGE
BHT-ALL-SRM,Chapter
2,StructuralRepairManual
1.Visuallyexaminethefuselage,cowling,andfairingskinsforcracks,
dents,tears,punctures,impactdamage,perforationofairinletscreens,
asapplicable,andconditionofthepaint.Payextraattentiontothese
particularlyexposedcomponents:
•Nosecap
•Cockpitplenumanduppernosedoors
•Nosebaydoors
•Noseshell
•Landinglightcoverpanelandwindow
•Forwardfairing
•Cabinplenumdoor
•Forwardcowlassemblies
•Transmissioncowlings
•Enginecowlings
•Sidebodypanels
2.Visuallyexaminethetailboomskinsforcracks,dents,tears,punctures,
impactdamage,andconditionofthepaint.Payextraattentiontothe
driveshaftcovers.
3.Visuallyexaminethehorizontalstabilizers,auxiliarynassemblies,
andverticalnassemblies,forcracks,dents,tears,punctures,impact
damage,andconditionofthepaint.Payextraattentiontotheleading
edgesandtheupperskins,asapplicable.
429-MM,Chapter52DOORSANDWINDOWS
Applicableto:ALL429-A-05-50-00-10A-284A-A
ECCNEAR99
10JAN2019-Issue1Page1