What was found
CLT - FOUND FUSELAGE SKIN CRACKED .8 INCH, BETWEEN BS 727D AND E, BL 0. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER PER SRM 51-10-2, 51-20-01, 51-40-00 AND 53-00-01 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 .8 INCH, BETWEEN BS 727D AND E, BL 0. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER PER SRM 51-10-2, 51-20-01, 51-40-00 AND 53-00-01 FIG 202. (M)