What was found
FUSELAGE FRAME DAMAGED BY CHAFING. REPAIRED IAW ENGINEERING REPORT 6829-2, REV 1R DATED AUG 1, 2007.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME DAMAGED BY CHAFING. REPAIRED IAW ENGINEERING REPORT 6829-2, REV 1R DATED AUG 1, 2007.