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 2 PLACES. CRACK 1 IS JUST FWD OF FRAME 75 & JUST ABOVE STRINGER 2L, CRACK IS APPROX 1.25" LONG. CRACK 2 IS AT THE FIRST FASTENER BELOW STRINGER 2L ON FRAME 75, CRACK IS 1/4" LONG. PERFORMED REPAIR AT LT UPPER FUSELAGE SKIN CRACK FWD OF FRAME 75 ABOVE STRINGER 2L & ON FRAME 75 BELOW STRINGER 2L IAW ERS-EM-53MR-2099.