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STRUCTURALREPAIRMANUAL
Page218
53−00−13
Printed in Germany
Jul01/04
CAUTION: THISREPAIRMUSTBEINSPECTEDATDEFINEDINTERVALS.THEACCORDING
INSPECTIONINSTRUCTIONREFERENCEISIIR53−00−13−2−002−00ANDIS
DESCRIBEDINCHAPTERSTRUCTURALREPAIRINSPECTIONS(SRI)OFTHE
SRM.INFORMYOURPLANNINGDEPARTMENTANDPROVIDETHEMWITHTHE
NECESSARYINFORMATION.
CAUTION: OBEYTHEREPAIREFFECTIVITYPERWEIGHTVARIANTANDAIRCRAFTTYPE
GIVENINTABLE203.
C. StringerOuterFlangeRepair
Therepairisapplicabletoformedandextrudedstringersasfollows:
− ifastringerouterflangeisdamagedoraskinrepairrequiresa
stringerouterflangecutout(Figure203)
− iftheouterflangeofthestringeriscorroded(Figure204).
NOTE: Therepairisapplicableonlyintheareasindicatedontherele
vantFigure.Therepaireffectivityofthisrepairisshownin
Table
AIRCRAFT
WEIGHTVARIANT
A340−2XX
000,001,002,
A340−2XX
021
A340−3XX
000,001,002,003,004
A340−3XX
020,021,024,026,027
RepairEffectivityperWeightVariantandAircraftType
Table203
NOTE: RefertotheWeightVariantIdentificationListgiveninthe
IntroductionoftheSRM.ThisTableshowsallnecessaryinformation
relatedtotheweightvariantandtheirmaximumvaluesandthe
modificationassociatedtotheaircrafttype.