What was found
DURING ROUTINE VISUAL INSPECTION, CORROSION DAMAGE FOUND ON FUSELAGE SKIN LOCATED AT BS 435, SL1504. DAMAGE LENGTH IS 1.375", WIDTH IS .5", AND DEPTH IS .02".
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ROUTINE VISUAL INSPECTION, CORROSION DAMAGE FOUND ON FUSELAGE SKIN LOCATED AT BS 435, SL1504. DAMAGE LENGTH IS 1.375", WIDTH IS .5", AND DEPTH IS .02".