What was found
CRACK FOUND ON FUSELAGE FRAME WEB AT SUPPORT BRACKET INBOARD AND OUTBOARD ATTACH RIVET AND INBOARD FRAME RADIUS AT STA 400 BETWEEN STRINGERS 8R AND 9R
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK FOUND ON FUSELAGE FRAME WEB AT SUPPORT BRACKET INBOARD AND OUTBOARD ATTACH RIVET AND INBOARD FRAME RADIUS AT STA 400 BETWEEN STRINGERS 8R AND 9R