What was found
INSPECTION FOUND A .375 INCH CRACK AT FASTENER HOLE IN TOP LEFT PANEL AT BS 273.5, LBL 14.5. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-40-2, 51-20-4 AND MM 51-20-11.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .375 INCH CRACK AT FASTENER HOLE IN TOP LEFT PANEL AT BS 273.5, LBL 14.5. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-40-2, 51-20-4 AND MM 51-20-11.