As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAJOR REPAIR - FUSELAGE FRAME CRACKED AT F.S. 177.35 RT STRINGER 9 AT RELIEF HOLE. MAINTENANCE STOP DRILLED AND PATCHED AFFECTED AREAS I.A.W. BEECH SRM 51-70. PATCH DIMENSIONS 3 INCH BY 2.4 INCH. .080 2024 T3 . RII COMPLIED WITH PER TASKCARD 8.2.1.