What was found
FUSELAGE SKIN GOUGED, 2 INCHES FWD OF FRAME 66 S26L. ACCOMPLISHED VISUAL INSPECTION NO CRACKS NOTED. BLENDED DAMAGED AREA IAW SRM 53-41-11. PERFORMED NDT, NO DEFECTS NOTED, INSTALLED RIVET WET.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN GOUGED, 2 INCHES FWD OF FRAME 66 S26L. ACCOMPLISHED VISUAL INSPECTION NO CRACKS NOTED. BLENDED DAMAGED AREA IAW SRM 53-41-11. PERFORMED NDT, NO DEFECTS NOTED, INSTALLED RIVET WET.