What was found
DURING INSPECTION, FOUND FUSELAGE SKIN CRACKED BETWEEN 3 RIVET HOLES AT FS 344 BETWEEN STRINGERS 22L AND 23L. REPAIRED PER SRM 53-30-3 FIG 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, FOUND FUSELAGE SKIN CRACKED BETWEEN 3 RIVET HOLES AT FS 344 BETWEEN STRINGERS 22L AND 23L. REPAIRED PER SRM 53-30-3 FIG 1.