What was found
INSPECTION TYPE:C3 HFEC & VISUAL INSP DETECTED A .225 INCH CRACK ON THE C-4 (D-PIT) LOWER FORWARD JAMB CORNER AS MARKED ON PART. REMOVED AND REPLACED FUSELAGE SKIN IAW SRM 51-1-20D, 51-1-21, 51-1-22, FS 1350 - 1490 L31R - L31L.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION TYPE:C3 HFEC & VISUAL INSP DETECTED A .225 INCH CRACK ON THE C-4 (D-PIT) LOWER FORWARD JAMB CORNER AS MARKED ON PART. REMOVED AND REPLACED FUSELAGE SKIN IAW SRM 51-1-20D, 51-1-21, 51-1-22, FS 1350 - 1490 L31R - L31L.