STRUCTURALREPAIRMANUAL
Page235
53−00−13
Printed in Germany
Jul01/05
CAUTION: THISREPAIRMUSTBEINSPECTEDATDEFINEDINTERVALS.THEACCORDING
INSPECTIONINSTRUCTIONREFERENCEISIIR53−00−13−2−003−00ANDIS
DESCRIBEDINCHAPTERSTRUCTURALREPAIRINSPECTIONS(SRI)OFTHE
SRM.INFORMYOURPLANNINGDEPARTMENTANDPROVIDETHEMWITHTHE
NECESSARYINFORMATION.
CAUTION: OBEYTHEREPAIREFFECTIVITYPERWEIGHTVARIANTANDAIRCRAFTTYPE
GIVENINTABLE204.
D. StringerRepair−StringermadefromDAN51B,DAN58Bandcomparable
Therepairisapplicabletoformedandextrudedstringers−madefrom
DAN51B,DAN58B,A539−70014,D530−70044orF530−70060−whenastringeris
damagedoraskinrepairrequiresastringersplice.
NOTE: Therepairisapplicableonlyintheareasindicatedontherele
vantFigure.Therepaireffectivityofthisrepairisshownin
Table204.
AIRCRAFT
WEIGHTVARIANT
A340−2XX
000,001,002
A340−2XX
021
A340−3XX
000,001,002,003,004
A340−3XX
020,021,024,026,027,028,050,051,052
RepairEffectivityperWeightVariantandAircraftType
Table204
NOTE: RefertotheWeightVariantIdentificationListgiveninthe
IntroductionoftheSRM.ThisTableshowsallnecessaryinformation
relatedtotheweightvariantandtheirmaximumvaluesandthe
modificationassociatedtotheaircrafttype.
