aircraft. All permanent repairs must be structural,procedures for all levels of maintenance. Informationrestore load-carrying capabilities, meet aerodynamiccontained in the SRM includes damagesmoothness requirements, and meet the environ-classifications, inspection procedures, typical repairmental durability requirements of the aircraft. Seeprocedures, and tool and material lists. Damagefigure 14-26. Repairable damage is divided intoexceeding any of these classifications requireseveral classifications. The aircraft’s structural repairengineering disposition. The examples listed belowmanual (SRM) provides the approved repairmay vary somewhat, depending upon the type ofFigure 14-26.—Example of repairable damage on composite material.14-25
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