What was found
CRACK FOUND ON FUSELAGE FRAME WEB AT SUPPORT BRACKET INBOARD AND OUTBOARD ATTACH RIVETS AT STA 380 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 RIVETS AT STA 380 BETWEEN STRINGERS 8R AND 9R