As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
*** SUPPLEMENTAL SDR *** FAULT: CRACK FOUND AT 10 O'CLOCK POSITION FACING AFT AT FR40 LOWER JUNCTION RH SIDE. APPLIED PROTECTION SURFACE ON FASTENERS HEAD IAW SRM 51-23-10. (8 OZ PAINT CUP #02-012-176) AND APPLIED CIC IAW EO: M-5100-2780-L ON STIFFENER AT FR 40 LOWER RADIUS RH SIDE. VERIFIED APPLIED PROTECTION ON SURFACE