What was found
UPPER FUSELAGE COCKPIT FLOORBEAM WITH CORROSION AT STA 277 AND AT 12 INCHES LBL 0. REPAIRED IAW SRM 51-40-4 FIG 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UPPER FUSELAGE COCKPIT FLOORBEAM WITH CORROSION AT STA 277 AND AT 12 INCHES LBL 0. REPAIRED IAW SRM 51-40-4 FIG 1.