What was found
INSPECTION FOUND A 1 CRACK IN FUSELAGE SKIN AT STA 440 ABOVE STRINGER 25R. THE CRACKED AREA WAS CUT OUT AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-10-2 AND 53-30-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 CRACK IN FUSELAGE SKIN AT STA 440 ABOVE STRINGER 25R. THE CRACKED AREA WAS CUT OUT AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-10-2 AND 53-30-3.