What was found
DURING REPETITIVE INSPECTION OF A/D 2000-20-08 ON LEFT FRONT PAX ENTRANCE DOOR LOWER FORWARD CORNER, VISUALLY DETECTED FUSELAGE SKIN CRACK EXTENDING OUTWARD FROM DOOR RADIUS 1.5 INCH.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING REPETITIVE INSPECTION OF A/D 2000-20-08 ON LEFT FRONT PAX ENTRANCE DOOR LOWER FORWARD CORNER, VISUALLY DETECTED FUSELAGE SKIN CRACK EXTENDING OUTWARD FROM DOOR RADIUS 1.5 INCH.