What was found
RT IB T/E AFT FLAP IMPACT DAMAGE 195" FROM IB END AND 4" FROM TE OF LE PANEL 3.5" OF DELAMINATION AND 2" BY 1" CRACK.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RT IB T/E AFT FLAP IMPACT DAMAGE 195" FROM IB END AND 4" FROM TE OF LE PANEL 3.5" OF DELAMINATION AND 2" BY 1" CRACK.