What was found
PUNCTURE DAMAGE BETWEEN FS1031 AND FS1047 JUST BELOW STGR 22L. C/W PERMANENT REPAIR IAW STS EA72-2020-082 INSTRUCTIONS. AIRCRAFT WEIGHT & BALANCE NOT AFFECTED PER PSA WEIGHT & BALANCE MANUAL. FAA FORM 337 SUBMITTED. WITNESSED NAT REVEAL LVL II NDT OF AMERICAN TESTING SERVICES PERFORM HFEC OF TRIM OUT EDGES. NO INDICATIONS NOTED. HFEC INSPECTION OF EXISTING FASTENER HOLES COMPLETED BY AMERICAN TESTING SERVICE. FOUND ACCEPTABLE INDICATIONS AT THIS TIME. HFEC INSPECTION OF REPAIR DOUBLER. FOUND ACCEPTABLE CONDITION AT THIS TIME.