As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING LANDING GEAR RETRACTION TEST, IT WAS NOTED THAT THE NOSE WHEEL ASSY WOULD CONTACT THE RT NOSE GEAR DOOR, AFT HINGE DURING LANDING GEAR CYCLE. IT WAS ALSO NOTED THAT THE NOSE WHEEL ASSY WOULD CONTACT THE NOSE WHEEL WELL STRUCTURE WHEN FULLY RETRACTED. PRECISION MEASUREMENTS DETERMINED THAT THE NOSE STRUT ASSY TO ACFT STRUCTURE ATTACH POINTS WERE MISALIGNED.