What was found
FRAME 25 IS CRACKED AT RT FLOOR SILL (BACKSIDE) BETWEEN STRINGER 15 AND 16L. PERFORMED REPAIR OF FRAME 25 AT FLOOR SILL IAW SRM 53-00-04, REPAIR 14.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FRAME 25 IS CRACKED AT RT FLOOR SILL (BACKSIDE) BETWEEN STRINGER 15 AND 16L. PERFORMED REPAIR OF FRAME 25 AT FLOOR SILL IAW SRM 53-00-04, REPAIR 14.