What was found
CRACK ON CUSP WEB BTW STA Y=655 TO Y=674 AND X=54 TO X=60 AT CAB PAX (CPAX). CUSP WEB WAS REPAIRED PER SRM 53-00-55-2R-4 FIG 206. HFEC INSPECTION WAS PERFORMED ON CUSP WEB AFT CUT OUT. NO CRACKS WERE FOUND PER NDT SPM 06-10-01.001.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON CUSP WEB BTW STA Y=655 TO Y=674 AND X=54 TO X=60 AT CAB PAX (CPAX). CUSP WEB WAS REPAIRED PER SRM 53-00-55-2R-4 FIG 206. HFEC INSPECTION WAS PERFORMED ON CUSP WEB AFT CUT OUT. NO CRACKS WERE FOUND PER NDT SPM 06-10-01.001.