What was found
FOUND FUSELAGE SKIN CRACKED AT FORWARD GALLEY DOOR UPPER DOOR HINGE CUTOUT. TRIMMED OUT DAMAGE AREA TO MAINTAIN A MINIMUM RADIUS OF .70 INCH, HFEC INSPECTION AROUND CUTOUT AREA NO DEFECTS NOTED. FABRICATED AND INSTALLED .50 INCH 2024-T3 FILLER AND .063 INCH CRES DOUBLER WITH CHAMFERED EDGES, REMOVED ALL NICKS, BURRS, SCRATCHES, GOUGES AND SHARP EDGES FROM SKIN AND ALL REPAIR PARTS IAW SRM 53-30-3 FIG 20 AND ECO 3233. AIRCRAFT RETURNED TO SERVICE. (M)