What was found
RT INLET INTERNAL PRIMARY PARTS REQUIRED FABRICATION AND INSTALLED, BUTTSTRAP SUPPORT BRACKETS, ANGLE , AND INNER ANGLE DUE TO CRACKING AND LOOSE RIVETS CAUSED GOUGING.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RT INLET INTERNAL PRIMARY PARTS REQUIRED FABRICATION AND INSTALLED, BUTTSTRAP SUPPORT BRACKETS, ANGLE , AND INNER ANGLE DUE TO CRACKING AND LOOSE RIVETS CAUSED GOUGING.