What was found
RIGHT FUSELAGE HAS LAP SEAM CORROSION AND CRACK COMING OUT OF RIVET HOLE AT STA R170 LONGERON 20. INSTALLED DOUBLER PER NAC DRAWING NAC011 SCENARIO 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT FUSELAGE HAS LAP SEAM CORROSION AND CRACK COMING OUT OF RIVET HOLE AT STA R170 LONGERON 20. INSTALLED DOUBLER PER NAC DRAWING NAC011 SCENARIO 1.