As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING RETRACTION TEST OF LANDING GEAR, NOSE STRUT PISTON WOULD NOT EXTEND COMPLETELY WITH AIRCRAFT ON JACKS. WHEEL WOULD CENTER 180 DEGREES FROM NORMAL CENTER. (WHEEL AND FORK ASSY WOULD CENTER BACKWARDS). LOWER BEARING, PN 1944E9A, MOUNTING FLANGE BOLT HOLES DRILLED 180 DEGREES OUT OF INDEX WITH BEARING CENTERING CAM LOBE. (X)