As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
1/4 INCH DIAGONAL CRACK ( TOP L TO BOTTOM R) FOUND IN FUSELAGE SKIN AT FRAME 75 JUST ABOVE STRINGER 2L. 1" AREA OF PAINT REMOVED AND AREA DYE PEN'D FOR BETTER VISIBILITY AND LOCATION OF CRACK. AREA AROUND FLAW TAPED OFF.-C/A-REPAIRED CRACK IN FUSELAGE SKIN AT FR 75 JUST ABOVE STR 21L, IAW SRM 53-31-01 AND SRM 51-40-02.