What was found
INSPECTION FOUND A 3 BY 5 INCH AREA OF FUSELAGE SKIN DENTED AT BS 890, LT SIDE, TOP OF WINDOW BELT. THE DENTED AREA WAS CUT OUT, DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-2, 51-10-2 AND SRM 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 3 BY 5 INCH AREA OF FUSELAGE SKIN DENTED AT BS 890, LT SIDE, TOP OF WINDOW BELT. THE DENTED AREA WAS CUT OUT, DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-2, 51-10-2 AND SRM 51-30-2.