What was found
DUE TO CORROSION BEYOND ACCEPTABLE LIMITS, 71 PERCENT MATERIAL LOSS, ON THE MAIN ENTRANCE DOOR LOWER TITANIUM STRIP. REPAIRED IAW ENGINEERING DRAWING F2MB222105A3 E01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DUE TO CORROSION BEYOND ACCEPTABLE LIMITS, 71 PERCENT MATERIAL LOSS, ON THE MAIN ENTRANCE DOOR LOWER TITANIUM STRIP. REPAIRED IAW ENGINEERING DRAWING F2MB222105A3 E01.