What was found
INSPECTION FOUND A .75 INCH CRACK ON FUSELAGE SKIN LAP JOINT AT STA 720, STRINGER 26R. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-6 AND 53-30-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .75 INCH CRACK ON FUSELAGE SKIN LAP JOINT AT STA 720, STRINGER 26R. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-6 AND 53-30-3.