What was found
CRACKED FRAME, INTERNAL FUSELAGE STRUCTURE BS 333 AND BTWN STR 2L TO 2R. FRAME AT INTERNAL FUSELAGE STRUCTURE OVER BS 333 AND BTWN STRINGERS 2L TO 2R WAS REPLACED IAW SRM 51-42-06-001-001-A01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED FRAME, INTERNAL FUSELAGE STRUCTURE BS 333 AND BTWN STR 2L TO 2R. FRAME AT INTERNAL FUSELAGE STRUCTURE OVER BS 333 AND BTWN STRINGERS 2L TO 2R WAS REPLACED IAW SRM 51-42-06-001-001-A01.