What was found
FUSELAGE FRAME 28 CORROSION BETWEEN STRINGERS 21 LT & RT. CUT AWAY CORRODED FRAME PORTION & SPLICED IN NEW IAW ADAPTATION OF TSK-530000-300-840-A01 FOLLOWING ATR INSTRUCTION IAW EO ATR-53-57-2014.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME 28 CORROSION BETWEEN STRINGERS 21 LT & RT. CUT AWAY CORRODED FRAME PORTION & SPLICED IN NEW IAW ADAPTATION OF TSK-530000-300-840-A01 FOLLOWING ATR INSTRUCTION IAW EO ATR-53-57-2014.