What was found
INSPECTION FOUND A 1 INCH CRACK IN FRAME AT BS 520 ABOVE STRINGER 24L. THE CRACK WAS STOP DRILLED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-4. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN FRAME AT BS 520 ABOVE STRINGER 24L. THE CRACK WAS STOP DRILLED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-4. (M)