What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) Just after landing at saint simon airport (ssi) Georgia, the nose gear collapsed. The BE-60 nose gear rotates 90 degrees to the aircraft's longitudinal axis before it is retracted into the nose wheel well and returns to the normal position upon extension. All three landing gear down and locked lights were illuminated indicating that all landing gear were safely extended. Upon touch down the nose gear collapsed because it did not rotate the required 90 degrees to re-align with the aircraft longitudinal axis and the ensuing side loading on the wheel and tire assembly caused the nose gear to collapse. During the investigation, and after consult with Beech technical representatives, it is determined that the gear straightener which interfaces with the rotating cam to align the wheel and tire assembly with the runway during the extension phase had been damaged and failed to return the wheel and tire assembly into proper position for landing. Photographs and schematics indicate the extent of damage to the gear straightening device and cam assembly. Investigation did not support that any pilot actions contributed to this event.
As the FAA filed it
(-23) JUST AFTER LANDING AT SAINT SIMON AIRPORT (SSI) GEORGIA, THE NOSE GEAR COLLAPSED. THE BE-60 NOSE GEAR ROTATES 90 DEGREES TO THE AIRCRAFT'S LONGITUDINAL AXIS BEFORE IT IS RETRACTED INTO THE NOSE WHEEL WELL AND RETURNS TO THE NORMAL POSITION UPON EXTENSION. ALL THREE LANDING GEAR DOWN AND LOCKED LIGHTS WERE ILLUMINATED INDICATING THAT ALL LANDING GEAR WERE SAFELY EXTENDED. UPON TOUCH DOWN THE NOSE GEAR COLLAPSED BECAUSE IT DID NOT ROTATE THE REQUIRED 90 DEGREES TO RE-ALIGN WITH THE AIRCRAFT LONGITUDINAL AXIS AND THE ENSUING SIDE LOADING ON THE WHEEL AND TIRE ASSEMBLY CAUSED THE NOSE GEAR TO COLLAPSE. DURING THE INVESTIGATION, AND AFTER CONSULT WITH BEECH TECHNICAL REPRESENTATIVES, IT IS DETERMINED THAT THE GEAR STRAIGHTENER WHICH INTERFACES WITH THE ROTATING CAM TO ALIGN THE WHEEL AND TIRE ASSEMBLY WITH THE RUNWAY DURING THE EXTENSION PHASE HAD BEEN DAMAGED AND FAILED TO RETURN THE WHEEL AND TIRE ASSEMBLY INTO PROPER POSITION FOR LANDING. PHOTOGRAPHS AND SCHEMATICS INDICATE THE EXTENT OF DAMAGE TO THE GEAR STRAIGHTENING DEVICE AND CAM ASSEMBLY. INVESTIGATION DID NOT SUPPORT THAT ANY PILOT ACTIONS CONTRIBUTED TO THIS EVENT.