What was found
LEFT NOSE SECTION OF AIRCRAFT WAS STRUCK BY WINGTIP OF TAXIING AIRCRAFT CAUSING DAMAGE TO THAT SECTION. COMPLIED WITH NETJETS RFTS 114245 REV.0. PERFORMED 10X DETAILED VISUAL INSPECTION (DVI) ON THE INTERNAL AND EXTERNAL FUSELAGE SKIN AND ADJACENT STRUCTURE PER AC43.13-1 B, CHAPTER 5 SECTION 2 TO VERIFY THERE IS NO CRACKS, DAMAGED FASTENERS, OR ADDITIONAL DAMAGE OTHER THAN WHAT HAS BEEN PREVIOUSLY REPORTED, NO ADDITIONAL DISCREPANCIES WERE NOTED. APPLIED REPAIR ADHESIVE TO INNER STRUCTURE DISBOND AND ALLOWED ADHESIVE TO CURE PER MANUFACTURERS INSTRUCTIONS. PICTURE(S) OF TEMP REPAIR PROVIDED TO MCC.