What was found
INTERNAL FUSELAGE STA 859.5 AND STR 14R FRAME HAS CHAFFING MARK & 1EA RIVET HEAD CHAFED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FRAME STRAP PER DWG 145T8002-14 REV B AT STA 859.9 STR 14R.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INTERNAL FUSELAGE STA 859.5 AND STR 14R FRAME HAS CHAFFING MARK & 1EA RIVET HEAD CHAFED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FRAME STRAP PER DWG 145T8002-14 REV B AT STA 859.9 STR 14R.