What was found
CORROSION ON ANGLE AND INTERNAL FUSELAGE SKIN AT LT SIDE OF VENTRAL STAIRS CUTOUT BS 1463-1480. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW ANGLE IAW SRM 51-30-02 AND DWG 9911991, REV K.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON ANGLE AND INTERNAL FUSELAGE SKIN AT LT SIDE OF VENTRAL STAIRS CUTOUT BS 1463-1480. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW ANGLE IAW SRM 51-30-02 AND DWG 9911991, REV K.