As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT UPPER FUSELAGE SKIN CRACKED IN 2 PLACES. CRACK 1 IS JUST AFT OF FRAME 75 & ABOVE STRINGER 2L. CRACK IS APPROX 3/8" LONG. CRACK 2 IS AT THE FIRST FASTENER AFT OF FRAME 75 ON STRINGER 2L, CRACK IS APPROX 1/4". FABRICATED & INSTALLED REPAIR PARTS FOR LT FRAME 75 IAW ERS-EM-53MR-2066. SEE TURN OVER FOR DETAILS.