What was found
FUSELAGE CRACKED AT STA 1022, 1.1/2" ABOVE LT LONGERON 8R. CRACK LENGTH 5/8". CRACK VERIFIED WITH EDDY CURRENT. ENDS OF CRACK MARKED. REPAIR IN WORK.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE CRACKED AT STA 1022, 1.1/2" ABOVE LT LONGERON 8R. CRACK LENGTH 5/8". CRACK VERIFIED WITH EDDY CURRENT. ENDS OF CRACK MARKED. REPAIR IN WORK.