What was found
R1 MAIN ENTRY DOOR HAS A 2 INCH LONG CRACK IN THE LOWER FORWARD VERTICAL CHORD RADIUS AT STA 446 BETWEEN WL 200 & 208.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
R1 MAIN ENTRY DOOR HAS A 2 INCH LONG CRACK IN THE LOWER FORWARD VERTICAL CHORD RADIUS AT STA 446 BETWEEN WL 200 & 208.