What was found
CRACK FUSELAGE THRESHOLD, FS 206.13 AND LBL 19.7 REPORT NO.FR-680A-0184-9951 REV - DATED 11/23/2021
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK FUSELAGE THRESHOLD, FS 206.13 AND LBL 19.7 REPORT NO.FR-680A-0184-9951 REV - DATED 11/23/2021