What was found
FOUND THE LT COCKPIT FLOORBEAM ANGLE TO BE CRACKED AT FS 278. R & R THE SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01, SRM TR-53-005 & DWG CC670-33199, REV B.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND THE LT COCKPIT FLOORBEAM ANGLE TO BE CRACKED AT FS 278. R & R THE SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01, SRM TR-53-005 & DWG CC670-33199, REV B.