As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CNTR WING INSP REAR SPAR INTERNAL ANGLE/TEE FITTING FR44 LT SIDE MID HOLE WITH CRACK SIGNAL. COMPLIED WITH EA:6-5710-T0343040 PT1 REPAIRED CENTER WING REAR SPAR RIB1 INTERNAL ANGLE/TEE FITTING AT FR44 LH SIDE MID HOLE(#35A). CATEGORY "B" REPAIR.FIRST INSPECTION IS 6560FC/18380FH WHICHEVER COMES FIRST AFTER REPAIR EMBODIED.INTERNAL INSPECTION IS 6560FC/18380FH WHICHEVER COMES FIRST .INSPECTION METHOD IS ROTATIVE PROBE INSPECTION AS PER NTM51-10-01 AFTER FASTENER AND BUSHES REMOVAL. MAJOR REPAIR IAW FEDEX GMM6-2-100