What was found
ATTACH ANGLE CRACKED ON TOP FUSELAGE TO VERTICAL STAB LT AT STA 15230.225 REPAIRED IAW SRM 55.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ATTACH ANGLE CRACKED ON TOP FUSELAGE TO VERTICAL STAB LT AT STA 15230.225 REPAIRED IAW SRM 55.