What was found
R2 DOOR CUTOUT A HAS CORROSION ON THE OUTSIDE SKIN OF THE FUSELAGE BETWEEN FR66 AND FR68 REPAIRED R2 DOOR CUTOUT EXT SKIN BELOW THE DOOR BETWEEN FR66 AND FR68 IAW ECRA 5341-01159 PART 1, ACCOMPLISH THE INITIAL INSPECTION REQUIREMENTS AT THE FUSELAGE SKIN AT FR66-FR68 UNDERNEATH SCUFFPLATE AS PER PART 2 OF ECRA 5341-01159 ON OR BEFORE THE AC REACHES 121,300FC. PLANNING TO CONTACT ENGINEERING FATER 115,300FC BUT BEFORE 116,300FC REPAIR PERFORMED PER PART 1 OF ECRA 5341-01159. ACCOMPLISH THE INITIAL INSPECTION REQUIREMENTS AT THE FUSELAGE SKIN AT FR66-68 UNDERNEATH SCUFF PLATE AS PER PART 2 OF EC/RA 5341-01159 ON OR BEFORE THE AIRCRAFT REACHES 121,300 TOTAL AIRCRAFT FLIGHT CYCLES. PLANNING TO CONTACT ENGINEERING AFTER 115,300 TOTAL AIRCRAFT FLIGHT CYCLES BUT BEFORE 116,300 TOTAL AIRCRAFT FLIGHT CYCLES. PART 2 INSPECTIONS TO BE DETERMINED BY EG.