What was found
DURING C CHECK, BULGING OF THE FUSELAGE SKIN WAS NOTED AT STR 25RT, AFT OF BS 1166. FOUND STRINGER 25 RT CRACKED. CUTOUT STRINGER FROM BS 1175 TO 1183. INSTALLED STRINGER REPAIR PER SRM 53-10-3. NON ROUTINE 3790.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C CHECK, BULGING OF THE FUSELAGE SKIN WAS NOTED AT STR 25RT, AFT OF BS 1166. FOUND STRINGER 25 RT CRACKED. CUTOUT STRINGER FROM BS 1175 TO 1183. INSTALLED STRINGER REPAIR PER SRM 53-10-3. NON ROUTINE 3790.