What was found
INSPECTION FOUND A 3 INCH CRACK IN LOWER FUSELAGE SKIN AT STA 1050, STRINGER 27L. THE CRACKED AREA WAS CUT OUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND 51-40-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 3 INCH CRACK IN LOWER FUSELAGE SKIN AT STA 1050, STRINGER 27L. THE CRACKED AREA WAS CUT OUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND 51-40-5.