What was found
(CAN) FUSELAGE TO WING ATTACH FITTINGS AT FUSELAGE STRINGER 3 WERE CHAFED BY FLAP SECONDARY DRIVE CABLE SHEATHS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) FUSELAGE TO WING ATTACH FITTINGS AT FUSELAGE STRINGER 3 WERE CHAFED BY FLAP SECONDARY DRIVE CABLE SHEATHS.