Airbus A340-200, Руководство по ремонту конструкций, Страница: 35 / 40

STRUCTURALREPAIRMANUAL
Page252
53−00−13
Printed in Germany
Jul01/05
(1) RepairMaterials
ITEM NOMENCLATURE QTY MATERIAL/REMARKS
1or2 Coupling − RefertoFigure209
− Sealant AR MaterialNo.09−013(Referto
Chapter51−35−00)
− CleaningAgent AR MaterialNo.11−003or11−004
(RefertoChapter51−35−00)
− Pretreatmentforpainting
(Chemicalconversioncoat
ing) AR MaterialNo.13−002(Referto
Chapter51−35−00)
− Storagepreservation(Cor
rosionpreventivetemporary
protectivecompound) AR MaterialNo.15−005A(Referto
Chapter51−35−00)
− Storagepreservation(Cor
rosionpreventivetemporary
protectivecompound) AR MaterialNo.15−007(Referto
Chapter51−35−00)
− StructurePaint(Polyure
thaneprimer) AR MaterialNo.16−001(Referto
Chapter51−35−00)
− StructurePaint(Polyure
thanetopcoat,grey) AR MaterialNo.16−002(Referto
Chapter51−35−00)
− StructurePaint(Washprim
er) AR MaterialNo.16−020(Referto
Chapter51−35−00)
− StructurePaint(flexible
polyurethane) AR MaterialNo.16−021(Referto
Chapter51−35−00)
(2) RepairInstruction(RefertoFigure209)
(a) Removeallfastenerasnecessaryfortherepair.
CAUTION: IFTHECOMPLETEDAMAGEDSTRINGERSECTIONMUSTBECUTOUT,
USEAPLASTICWEDGETOCAREFULLYREMOVETHESECTIONAWAY
FROMTHESKIN.PLACEAMETALSHEETBETWEENSTRINGERAND
SKINTOAVOIDDAMAGETOTHESTRUCTUREDURINGTHECUTOUT
ACTION.
CAUTION: IFYOUMUSTHEATTHEREPAIRAREATOHELPSEPARATETHE
STRINGERCUTOUTFROMTHESKIN,DONOTUSEATEMPERATURE
MORETHAN130C
° (266.0F ° )
(b) Cutoutthedamagedsectionofthestringeranddeburrthe
edges.
(c) Preparetherepairpartstosuitthedamagedareaanddeburr,
refertoFigure209.
(d) Attachtherepairpartsintheircorrectposition.Transferdrill
existingfastenerholesfromtheouterflangetotherepair
parts.Markanddrilladditionalholes.
NOTE: UsetransitionfitforHi−Lokfastenerinstallation(Refer
toChapter51−44−11).