As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CLOSE OUT PANEL ON AFT SIDE OF REAR SPAR CARRY THROUGH. TWO CRACKS IN LOWER BEND RADIUS. FIRST CRACK AT END OF CENTER STRINGER AND LOWER END OF ANGLE STRIP ATTACHED TO PANEL SKIN. SECOND CRACK IS FORWARD OF LEFT OF CENTER STRINGER IN BEND RADIUS OF PANEL. BOTH CRACKS WERE COVERED BY PRESSURE VESSEL SEALANT. (M)