What was found
HORIZONTAL STIFFENER CRACKED AT END FASTENER ON UPPER SKIN SURFACE INSIDE ACCESS PANEL 8204 18 INCHES OTBD OF FUSELAGE APPROX STA 860.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
HORIZONTAL STIFFENER CRACKED AT END FASTENER ON UPPER SKIN SURFACE INSIDE ACCESS PANEL 8204 18 INCHES OTBD OF FUSELAGE APPROX STA 860.