What was found
CORROSION ON ANGLE AND INTERNAL FUSELAGE SKIN ON RT SIDE OF VENTRAL STAIR CUTOUT, BS 1463 - 1480. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED ANGLE REPAIR IAW SRM 51-10-03, 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 ON RT SIDE OF VENTRAL STAIR CUTOUT, BS 1463 - 1480. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED ANGLE REPAIR IAW SRM 51-10-03, 51-30-02 AND DWG 9911991, REV K.