What was found
CRACK ON AFT EDGE ANGLE BETWEEB BEAM NR 5 AND 6. THE ANGLE WAS REPLACED IAW SRM 51-41-01, 51-41-02, AND DWG 5914121 REV: AV.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON AFT EDGE ANGLE BETWEEB BEAM NR 5 AND 6. THE ANGLE WAS REPLACED IAW SRM 51-41-01, 51-41-02, AND DWG 5914121 REV: AV.