What was found
INSPECTION FOUND A 3 INCH CRACK WITH CORROSION IN FUSELAGE TO FLOOR ANGLE AT STA 983 TO 996, LONGERON 19R. THE CORRODED SECTION WAS REMOVED, FILLER AND UPPER AND LOWER ANGLE DOUBLERS WERE INSTALLED IAW SRM 53-05, FIGURE 25, SHEET 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 3 INCH CRACK WITH CORROSION IN FUSELAGE TO FLOOR ANGLE AT STA 983 TO 996, LONGERON 19R. THE CORRODED SECTION WAS REMOVED, FILLER AND UPPER AND LOWER ANGLE DOUBLERS WERE INSTALLED IAW SRM 53-05, FIGURE 25, SHEET 1.