What was found
DURING SCHEDULED D CHECK, FOUND VERTICAL FIN ATTACH CLEVIS DRAG ANGLES CORRODED LT SIDE (2 EA). REMOVED AND REPLACED VERTICAL FIN DRAG ANGLES PER SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED D CHECK, FOUND VERTICAL FIN ATTACH CLEVIS DRAG ANGLES CORRODED LT SIDE (2 EA). REMOVED AND REPLACED VERTICAL FIN DRAG ANGLES PER SRM.