As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
R/H FR.68 STGR.22, FRAME WEB HORIZONTAL FLANGE LOWER SURFACE RADIUS CRACKED APROX' 1.5 INCH IN LENTHG AT I/B SIDE REQUESTING REPAIR DISPOSITION ADITIONAL ENGENIRING DOCUMENTATION IS REQUIRED. C/A: C/W ALLSTEPS OF PRI 616556-14AD REVD AWAITING ENGINEERING C/W ALL STEP OF PRI 615556-14D REV 1. AWAITING FINAL ERA VERIFIED THAT PRI AND ERA # 616556-14AD REV ORIGINAL MATCH. (LP: 0252794)