What was found
CORROSION LT WING SKIN AREA BETWEEN WS 150 & WS558. REMOVED CORROSION AND SENT MEASURMENTS TO FLIGHT VEHICLE CONSULTING FOR EVALUATION. BLENDED AREAS WERE FOUND TO BE IN LIMITS IAW FVC DWG 57-13170-1 WITH 8110-3 APPROVAL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION LT WING SKIN AREA BETWEEN WS 150 & WS558. REMOVED CORROSION AND SENT MEASURMENTS TO FLIGHT VEHICLE CONSULTING FOR EVALUATION. BLENDED AREAS WERE FOUND TO BE IN LIMITS IAW FVC DWG 57-13170-1 WITH 8110-3 APPROVAL.