What was found
INSPECTION FOUND TWO .125 INCH CRACKS AT ONE FASTENER HEAD IN NLG CEILING PANEL AT BS 276, RBL 14. THE CRACKS WERE ROUTED 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 TWO .125 INCH CRACKS AT ONE FASTENER HEAD IN NLG CEILING PANEL AT BS 276, RBL 14. THE CRACKS WERE ROUTED OUT, A FILLER AND DOUBLER REPAIR WERE FABRICATED AND INSTALLED IAW SRM 51-40-2.