What was found
UPON INSPECTION OF LAV TRUCK DAMAGE FOUND 2EA 1INCH LONG PUNCTURES THRU OUTER SKIN OF LAV SERVICE PANEL DOOR. REF SMC16 FOR DAMAGE REMOVED. REMOVE FUSELAGE SKIN FASTENERS REF SMC16 & PTT 3582009 & PTT 3582026. GOING TO REPLACE SKIN PER AIRBUS. REMOVED FASTENERS COMMON TO DAMAGED AREA AND CUT OUT DAMAGED SKIN. REMOVED SKIN AND HFEC INSPECTED HOLES. DRILLED NEW SKIN TO MATCH AIRCRAFT. COUNTERSINK AND FINAL TRIMMED NEW SKIN. SEALED SKIN PANEL AND INSTALLED ON AIRCRAFT WITH TEMP FASTENERS.