What was found
CLT - FOUND .25 INCH CRACK, FUSELAGE SKIN UPPER CORNER L1 WINDOW. INSTALLED DOUBLER PER 53-30-3. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - FOUND .25 INCH CRACK, FUSELAGE SKIN UPPER CORNER L1 WINDOW. INSTALLED DOUBLER PER 53-30-3. (M)