What was found
DURING ROUTINE C CHECK INSPECTION, LEFT FUSELAGE OVERWING EXIT HATCH LOWER SILL INNER CHORD CRACKED 0.250 INCH AT STA 883.5 REF. N/R 0250.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ROUTINE C CHECK INSPECTION, LEFT FUSELAGE OVERWING EXIT HATCH LOWER SILL INNER CHORD CRACKED 0.250 INCH AT STA 883.5 REF. N/R 0250.