As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK ON CUSP WEB AT STA Y=256 AND X=-54 AT CAB PAX (CPAX). CUSP WEB WAS REPAIRED PER SRM 53-00-55-2R-4- FIG 221. HFEC WAS ACCOMPLISHED ON CUSP WEB, TRIM OUT AREA WAS FOUND AT STA Y=256 AND X=-49 AT CAB PAX AND NO CRACK INDICATION WAS FOUND PER NDTSPM PART 6. 06-10-01.001.