What was found
DURING INSPECTION CHECK, FOUND STRESS CORROSION CRACK ON RT WING UPPER EXTERIOR SURFACE STA XRS74 STRINGERS 9 TO 15. DAMAGE WILL BE REPAIRED IAW EWO ATI 57-038 AND FAA FORM 8110-3 MUST BE ISSUED APPROVING THIS REPAIR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION CHECK, FOUND STRESS CORROSION CRACK ON RT WING UPPER EXTERIOR SURFACE STA XRS74 STRINGERS 9 TO 15. DAMAGE WILL BE REPAIRED IAW EWO ATI 57-038 AND FAA FORM 8110-3 MUST BE ISSUED APPROVING THIS REPAIR.