What was found
INSPECTION FOUND A 2 AND 1.2 CRACK IN FUSELAGE SKIN AT STA 1143, LONGERON 14 AND 16R. THE CRACKS WERE STOP DRILLED AND REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, PAGE 9.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 AND 1.2 CRACK IN FUSELAGE SKIN AT STA 1143, LONGERON 14 AND 16R. THE CRACKS WERE STOP DRILLED AND REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, PAGE 9.