What was found
DURING ROUTINE C CHECK INSPECTION, RIGHT FUSELAGE OVERWING EXIT HATCH LOWER SILL INNER CHORD CRACKED 0.200 INCH AT STA 883.5. REF N/R 0251
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ROUTINE C CHECK INSPECTION, RIGHT FUSELAGE OVERWING EXIT HATCH LOWER SILL INNER CHORD CRACKED 0.200 INCH AT STA 883.5. REF N/R 0251