What was found
CORROSION ON FRAME CONNECTION , C80, P`36 REPAIR PERFORMED BY REPLACEMENT OF CORRODED SECTIONS (A539-87426-212/-211) AND INSTALLING BOLTS NAS 6603-5 INSTEAD OF RIVETS, APPROVED BY EA 6-5319-99170 AND RAS/DAHAM/4020596/2006 ISSUE A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON FRAME CONNECTION , C80, P`36 REPAIR PERFORMED BY REPLACEMENT OF CORRODED SECTIONS (A539-87426-212/-211) AND INSTALLING BOLTS NAS 6603-5 INSTEAD OF RIVETS, APPROVED BY EA 6-5319-99170 AND RAS/DAHAM/4020596/2006 ISSUE A.