What was found
CLT - FOUND FUSELAGE SKIN CRACKED 2.25 INCH, FORWARD SERVICE DOOR CUTOUT LOWER AFT CORNER BS 330. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-01 FIG 202. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - FOUND FUSELAGE SKIN CRACKED 2.25 INCH, FORWARD SERVICE DOOR CUTOUT LOWER AFT CORNER BS 330. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-01 FIG 202. (M)