What was found
DURING C-CHECK FUSELAGE CRACKED AT DENT FRAME 17-18, STRINGER 21L-21R VERIFIED WITH EDDY CURRENT. MX PERFORMED REPAIR AT FRAME 17-18, STRINGER 21L-21R IAW EC5320-01802. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK FUSELAGE CRACKED AT DENT FRAME 17-18, STRINGER 21L-21R VERIFIED WITH EDDY CURRENT. MX PERFORMED REPAIR AT FRAME 17-18, STRINGER 21L-21R IAW EC5320-01802. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.