What was found
DURING HMV INSPECTIONS IT WAS NOTED THAT THE FUSELAGE SKIN WAS CRACKED AT STRINGER 1 BETWEEN FS 1090 AND FS 1110. THIS DAMAGED WAS REPAIRED PER ER/A 333417-14 AND APPROVED BY FAA 8110-3 FORM, DER DESIGNATION DERY-635273-NM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING HMV INSPECTIONS IT WAS NOTED THAT THE FUSELAGE SKIN WAS CRACKED AT STRINGER 1 BETWEEN FS 1090 AND FS 1110. THIS DAMAGED WAS REPAIRED PER ER/A 333417-14 AND APPROVED BY FAA 8110-3 FORM, DER DESIGNATION DERY-635273-NM.