What was found
FORWARD BILGE FUSELAGE CIRCUMFERENTIAL FRAME HAS CORROSION ON UPPER CHORD AT STA 820, LBL 45.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FORWARD BILGE FUSELAGE CIRCUMFERENTIAL FRAME HAS CORROSION ON UPPER CHORD AT STA 820, LBL 45.