What was found
LT WING TE, MIDPOINT BETWEEN NR 1 O/B PYLON AND I/B NR 3 FLAP TRACK EVIDENCE OF CRACK AT RIVET HEAD TO EDGE LWR SKIN. REQUEST NDT TO CONFIRM. REMOVED FASTENER IAW A310 SRM 51-40-21, ROTO TESTED HOLE IAW NTM 51-10-00-01 NO CRACKS FOUND, FABRICATED REPAIR PARTS IAW EA6-5710-73485A DWG R57249152. INSTALLED REPAIR PARTS IAW EA6-5710-73485A DWGR 57249152. DOME SEALED FASTENER IAW A310 SRM 51-76-20, LEAK CHECK IAW AMM A310-28-11-00-5.