What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) On February 3, 2006, at approximately 1737 MST, N88AA, a Cessna 182-R182, with privacy data omitted performing as pilot-in-command, experienced a nose gear collapse after landing on runway 34 at Bullhead international airport (ifp). The pilot privacy data omitted stated that the landing on runway 34 was normal and that after the aircraft cleared the runway and was on taxiway delta, the nose gear suddenly collapsed. Statements from ATC personnel in the tower support that there wasn't anything unusual about this landing. Inspection of the aircraft revealed that the rivets that attach the bracket at the aft end of the nose gear hydraulic actuator failed due to structural overload. The specific cause for the structural overload is not known. The smear pattern on the rivets was from aft to forward indicating the rivets failed when this bracket was pulled forward. This is the normal direction of travel fro gear retraction. There was no evidence to support that this damage was caused by a hard landing. The aircraft sustained substantial damage to the nose gear assembly, nose gear doors and fire wall structure. There were no injuries to the sole occupant.
As the FAA filed it
(-23) ON FEBRUARY 3, 2006, AT APPROXIMATELY 1737 MST, N88AA, A CESSNA 182-R182, WITH ^PRIVACY DATA OMITTED^ PERFORMING AS PILOT-IN-COMMAND, EXPERIENCED A NOSE GEAR COLLAPSE AFTER LANDING ON RUNWAY 34 AT BULLHEAD INTERNATIONAL AIRPORT (IFP). THE PILOT ^PRIVACY DATA^ STATED THAT THE LANDING ON RUNWAY 34 WAS NORMAL AND THAT AFTER THE AIRCRAFT CLEARED THE RUNWAY AND WAS ON TAXIWAY DELTA, THE NOSE GEAR SUDDENLY COLLAPSED. STATEMENTS FROM ATC PERSONNEL IN THE TOWER SUPPORT THAT THERE WASN'T ANYTHING UNUSUAL ABOUT THIS LANDING. INSPECTION OF THE AIRCRAFT REVEALED THAT THE RIVETS THAT ATTACH THE BRACKET AT THE AFT END OF THE NOSE GEAR HYDRAULIC ACTUATOR FAILED DUE TO STRUCTURAL OVERLOAD. THE SPECIFIC CAUSE FOR THE STRUCTURAL OVERLOAD IS NOT KNOWN. THE SMEAR PATTERN ON THE RIVETS WAS FROM AFT TO FORWARD INDICATING THE RIVETS FAILED WHEN THIS BRACKET WAS PULLED FORWARD. THIS IS THE NORMAL DIRECTION OF TRAVEL FRO GEAR RETRACTION. THERE WAS NO EVIDENCE TO SUPPORT THAT THIS DAMAGE WAS CAUSED BY A HARD LANDING. THE AIRCRAFT SUSTAINED SUBSTANTIAL DAMAGE TO THE NOSE GEAR ASSEMBLY, NOSE GEAR DOORS AND FIRE WALL STRUCTURE. THERE WERE NO INJURIES TO THE SOLE OCCUPANT.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.