What was found
C1 CRACKED APPROX .5 ON LONG 14 UPPER FLANGE 2ND CANTED FRAME FROM STA 1766 INSIDE MAIN CABIN RT SIDE WALL. REMOVED DAMAGED SECTION OF LONGERON, FABRICATED, AND INSTALLED IAW DC-8 SRM 53-2-2 FIG 10.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
C1 CRACKED APPROX .5 ON LONG 14 UPPER FLANGE 2ND CANTED FRAME FROM STA 1766 INSIDE MAIN CABIN RT SIDE WALL. REMOVED DAMAGED SECTION OF LONGERON, FABRICATED, AND INSTALLED IAW DC-8 SRM 53-2-2 FIG 10.