What was found
INSPECTION FOUND A .125 INCH CRACK AT TWO EACH FASTENER HEADS IN NLG CEILING PANEL AT BS 285, LBL 4. THE CRACKED AREA WAS CUT OUT, A FILLER AND DOUBLER REPAIR WERE FABRICATED AND INSTALLED IAW SRM 51-40-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .125 INCH CRACK AT TWO EACH FASTENER HEADS IN NLG CEILING PANEL AT BS 285, LBL 4. THE CRACKED AREA WAS CUT OUT, A FILLER AND DOUBLER REPAIR WERE FABRICATED AND INSTALLED IAW SRM 51-40-2.