What was found
ANGLE CRACKED AT LEFT FR 26 STRINGER 4 (INTERNAL STRUCTURE). ANGLE REPLACED AT L/H FR 26 STRG 4 IAW SRM 51-25-01 AND 51-25-04.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ANGLE CRACKED AT LEFT FR 26 STRINGER 4 (INTERNAL STRUCTURE). ANGLE REPLACED AT L/H FR 26 STRG 4 IAW SRM 51-25-01 AND 51-25-04.