What was found
DURING THE CURRENT C1 CHECK AT PEMCO-TPA, CORROSION WAS FOUND AROUND THE LH SIDE FRAME FITTING (PICKLEFORK). THE PICKLEFORK WAS REMOVED AND FOUND TO BE CORRODED BEYOND REPAIR, SO IT WAS REPLACED. THE SURFACE OF THE REAR SPAR WEB COMMON TO THE PICKLEFORK WAS ALSO FOUND TO HAVE CORROSION. THE CORROSION WAS BLENDED AND GRID MAPPED FOR REMAINING THICKNESS. THERE ARE NO REPAIRS IN THE SRM SO FLIGHT VEHICLES CONSULTING, INC., WAS CONTACTED FOR AN FAA-DER APPROVED REPAIR. THE PURPOSE OF THIS REA IS TO AUTHORIZE AND DOCUMENT ACCOMPLISHMENT OF REF /A/, WHICH IS AN FAA-DER APPROVED REPAIR. C/W ABX REA-5350-66010-00. AIRCRAFT RETURNED TO SERVICE AFTER C1 CHECK COMPLETION.