What was found
RT AND LT OUTBOARD FLAP MID HINGE ATTACH HARDWARE CORRODED. INSTALLED NEW HARDWARE IAW CRJ200 AMM 57-53-02-400-803.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RT AND LT OUTBOARD FLAP MID HINGE ATTACH HARDWARE CORRODED. INSTALLED NEW HARDWARE IAW CRJ200 AMM 57-53-02-400-803.