What was found
INSPECTION FOUND A 5.25 INCH CRACK IN FUSELAGE SKIN AT STA 510 BETWEEN STRINGER 25 AND 26R. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. THE DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-30-8 AND 51-30-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 5.25 INCH CRACK IN FUSELAGE SKIN AT STA 510 BETWEEN STRINGER 25 AND 26R. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. THE DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-30-8 AND 51-30-3.