What was found
CLT - INSPECTION VISUALLY FOUND A 2 INCH CRACK LOCATED AT UPPER FLANGE OF FUSELAGE FRAME STA 500 ATTACH TO RT TRANSITION ANGLE. INSTALLED FILLER AND DOUBLER AND RIVET INSTALLATION PER BOEING SRM 51-40-3. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - INSPECTION VISUALLY FOUND A 2 INCH CRACK LOCATED AT UPPER FLANGE OF FUSELAGE FRAME STA 500 ATTACH TO RT TRANSITION ANGLE. INSTALLED FILLER AND DOUBLER AND RIVET INSTALLATION PER BOEING SRM 51-40-3. (X)