What was found
TOP OF FUSELAGE STA 640, LAP SEAM CORRODED AND SKIN CRACKED BETWEEN L-4 AND L5. REMOVED CORRODED AND DAMAGED AREA. FABRICATED AND INSTALLED FILLER AND DOUBLER PER NAC DRAWING NAC011 REV 32.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TOP OF FUSELAGE STA 640, LAP SEAM CORRODED AND SKIN CRACKED BETWEEN L-4 AND L5. REMOVED CORRODED AND DAMAGED AREA. FABRICATED AND INSTALLED FILLER AND DOUBLER PER NAC DRAWING NAC011 REV 32.