Airbus A340-200, Руководство по ремонту конструкций, Страница: 15 / 40

STRUCTURALREPAIRMANUAL
Page219
53−00−13
Printed in Germany
Jul01/04
(1) RepairMaterials
ITEM NOMENCLATURE QTY MATERIAL/REMARKS
1 Coupling − RefertoFigure203or204
2 FillerorShim − RefertoFigure203or204
− 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(RefertoFigure203and/or204)
(a) Removeallfastenersasnecessaryfortherepair.
(b) Reworkthedamagedpartofstringerouterflangeanddeburrthe
edges.
NOTE: Makesurenottodamagetheadjacentstructure.
(c) Ifthereiscorrosion(RefertoFigure204):
1 Examinetherepairareaandremoveallsignsofcorrosion(Re
fertoChapter51−74−00.
2 Checkremainingthicknessoftheareafromwhichthecorrosion
hasbeenremoved.Ifthethicknessislessthan0.8mm(0.03
in.)cutouttheouterflange.
(d) Preparetherepairpartsanddeburrtheedges(Refertothe
relevantFigure).