What was found
CRACKED ANGLE TO ATTACH TOP FUSELAGE TO VERTICAL STAB RT SIDE STA Y=1405 AND Y=1437 APPROXIMATELY, H1L1-SM, CARD 168, ZONE 100. ANGLE WAS REPLACE IAW DWG 5912188, REV BD AND SRM 51-30-5. RETAIN FOR RECORDS BY PRIMARY STRUCTURE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED ANGLE TO ATTACH TOP FUSELAGE TO VERTICAL STAB RT SIDE STA Y=1405 AND Y=1437 APPROXIMATELY, H1L1-SM, CARD 168, ZONE 100. ANGLE WAS REPLACE IAW DWG 5912188, REV BD AND SRM 51-30-5. RETAIN FOR RECORDS BY PRIMARY STRUCTURE.