BHT-429-MPI
Table1.AirworthinessLimitationsSchedule(continued)
NOMENCLATURE
PARTNUMBER
(1)
AIRWORTHINESSLIFE
9
Foreveryoneautorotationlanding,youadd117RINtotheprevioustotal.
10
RefertotheAirworthinessLimitationssectionofthePW207D1/D2MaintenanceManual(P/N3071602).
11
Airworthinesslifeinyearsandmonthsappliestoshelfandoperatingtimefromdateofmanufacture.
12
RefertotheBHT-429-II-38forinformationontheapplicabilityoftheitemslistedtothespecicoatkitconguration
installedonthehelicopter.
13
Foreverylanding,youadd1RINtotheprevioustotal.
14
Foreverynormalretraction/extensionofthewheeledlandinggearsystem,youadd1RINtotheprevioustotal.For
everyemergencygearreleaseofthewheeledlandinggearsystem,youadd36RINtotheprevioustotal.
15
Foreverynormalretraction/extensionofthewheeledlandinggearsystem,youadd1RINtotheprevioustotal.
16
Theexternalhoistliftisdenedasanunreelingandrecoveryofthecablewithaloadattachedtothehook,independent
ofthelengthofthecablethatisdeployed/recovered.Anunreeling/recoveryofthecablewithnoloadonthehookis
notconsideredtobealift.Anyoperationwherealoadof30pounds(14kg)orgreaterisappliedforoperation(i.e.,
unreelingorrecovery,cableconditioning)mustbeconsideredasonelift.
17
Theactuatormustbeoverhauledat2000RINand4000RIN.OverhaulistobeaccomplishedbyBeaverAerospace
only.ReturnactuatortoBellHelicopterT extron(BHT)perILGEN-04-98.
18
Whenoneorbothenginesarestarted,youadd1RINtotheprevioustotal.
Table2.InspectionLimitationsSchedule
NOMENCLATURE
PARTNUMBER
(1)
INSPECTIONINTERVAL
MAINROTOR
MainRotorYokeAssembly429-010-103-10150hours
(2)
NOTES:
1
Inspectionlimitationforthepartnumberlistedappliestoallsuccessivedashnumbersforthecomponent,unless
otherwisespecied.
2
RefertoFigure1forinspectiondetails.
Table3.CerticationMaintenanceRequirements
NOMENCLATURE
PARTNUMBER
(1)
INTERVAL
WHEELEDLANDINGGEAR
WheeledLandingGear
System
429-705-001-101800hoursor1year
(2)
KITS
Float/LifeRaftKit
429-706-069-1011600hours
(3)
Applicableto:ALL429-A-04-00-00-00A-288A-A
ECCNEAR99
10JAN2019-Issue1Page5