What was found
CRACK ON THE LT ANGLE THAT ATTACH FUSELAGE TO VERTICAL STABILIZER BS 1463. DAMAGED AREA WAS REPAIRED IAW DWG SR09530296, REV.A, HFC IAW SPM 06-10-01.001. NO CRACKS WERE FOUND AFTER TRIM OUT.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON THE LT ANGLE THAT ATTACH FUSELAGE TO VERTICAL STABILIZER BS 1463. DAMAGED AREA WAS REPAIRED IAW DWG SR09530296, REV.A, HFC IAW SPM 06-10-01.001. NO CRACKS WERE FOUND AFTER TRIM OUT.