What was found
(CAN) DURING INSPECTION, CORROSION, DISBOND AND A 1.0" CRACK WERE FOUND ON THE LOWER FUSELAGE SKIN AT AN ANTENNA CUTOUT LOCATED BETWEEN STN. X167.00 - X182.00, AND BETWEEN STR. 32S AND 32P.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) DURING INSPECTION, CORROSION, DISBOND AND A 1.0" CRACK WERE FOUND ON THE LOWER FUSELAGE SKIN AT AN ANTENNA CUTOUT LOCATED BETWEEN STN. X167.00 - X182.00, AND BETWEEN STR. 32S AND 32P.