What was found
CRACK DAMAGE TO THE AFT UPPER FRAME ANGLE (PN: 350A21-1262.21) IN THE CARGO BAY WAS IDENTIFIED AT APPROXIMATELY FS 198” MEASURING APPROXIMATELY 0.125”.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK DAMAGE TO THE AFT UPPER FRAME ANGLE (PN: 350A21-1262.21) IN THE CARGO BAY WAS IDENTIFIED AT APPROXIMATELY FS 198” MEASURING APPROXIMATELY 0.125”.