What was found
DURING SCHEDULED C-10 CHECK, FOUND FUSELAGE TO WING FORWARD FAIRING ATTACH ANGLE CRACKED AT FS 476, LBL 59, WL 285. REPAIRED BY REPLACEMENT IAW SMP583 51-70.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED C-10 CHECK, FOUND FUSELAGE TO WING FORWARD FAIRING ATTACH ANGLE CRACKED AT FS 476, LBL 59, WL 285. REPAIRED BY REPLACEMENT IAW SMP583 51-70.