What was found
INSPECTION TYPE: C2, VERTICLE WEB IN COCKPIT SUBFLOOR IS CORRODED BEYOND LIMITS AT STA -80 LBL 50 AT FUSELAGE SKIN. REMOVED, FABRICATED AND REPLACED WEB/DOUBLER IAW DWG 5613785 AND SRM 51-1-20D, 51-1-21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION TYPE: C2, VERTICLE WEB IN COCKPIT SUBFLOOR IS CORRODED BEYOND LIMITS AT STA -80 LBL 50 AT FUSELAGE SKIN. REMOVED, FABRICATED AND REPLACED WEB/DOUBLER IAW DWG 5613785 AND SRM 51-1-20D, 51-1-21.