What was found
LT FUSELAGE FRAME DAMAGED BY CHAFING. REPAIRED IAW ENGINEERING REPORT 6593-1, REV IR DATED 5 MAR 07..
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT FUSELAGE FRAME DAMAGED BY CHAFING. REPAIRED IAW ENGINEERING REPORT 6593-1, REV IR DATED 5 MAR 07..