What was found
INSPECTION FOUND A 1.5 INCH CRACK AT FASTENER HOLE OF FRAME AT STA 400 LOWER LOBE. THE CRACKED AREA WAS REMOVED, A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.5 INCH CRACK AT FASTENER HOLE OF FRAME AT STA 400 LOWER LOBE. THE CRACKED AREA WAS REMOVED, A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-30-2.