What was found
THE TRAILING EDGE OF THE L/H INBOARD FLAP COVE SKIN WAS FOUND TO BE CRACKED ALONG THE RIVET LINE. AFTER DAMAGED MATERIAL WAS REMOVED, THE HOLE WAS ABOUT 8.5"X2.5" THIS AREA WAS FLUSH PATCHED PER CASA 212 SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
THE TRAILING EDGE OF THE L/H INBOARD FLAP COVE SKIN WAS FOUND TO BE CRACKED ALONG THE RIVET LINE. AFTER DAMAGED MATERIAL WAS REMOVED, THE HOLE WAS ABOUT 8.5"X2.5" THIS AREA WAS FLUSH PATCHED PER CASA 212 SRM.