What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) On March 9, 2003 at approximately 1630 MST, the aircraft departed ffz on a local pleasure flight. After take-off and the landing gear had been retracted, the nose landing gear in transit indication light stayed illuminated. Viewing through an external mounted mirror, the nose gear appeared to be fully retracted. The flight continued and during a 3G maneuver an unusual noise was heard. A visual examination via the mirror showed that the nose gear was hanging out of the wheel well at about a 45 degree angle. Several attempts to obtain a down and locked landing gear indication failed. The pilot elected to land gear up at iwa. Minor aircraft damage. No injuries to the occupants. An investigation showed that the nose gear hydraulic actuator piston failed in the threaded area of the rod end bearing attachment.
As the FAA filed it
(-23) ON MARCH 9, 2003 AT APPROXIMATELY 1630 MST, THE AIRCRAFT DEPARTED FFZ ON A LOCAL PLEASURE FLIGHT. AFTER TAKE-OFF AND THE LANDING GEAR HAD BEEN RETRACTED, THE NOSE LANDING GEAR IN TRANSIT INDICATION LIGHT STAYED ILLUMINATED. VIEWING THROUGH AN EXTERNAL MOUNTED MIRROR, THE NOSE GEAR APPEARED TO BE FULLY RETRACTED. THE FLIGHT CONTINUED AND DURING A 3G MANEUVER AN UNUSUAL NOISE WAS HEARD. A VISUAL EXAMINATION VIA THE MIRROR SHOWED THAT THE NOSE GEAR WAS HANGING OUT OF THE WHEEL WELL AT ABOUT A 45 DEGREE ANGLE. SEVERAL ATTEMPTS TO OBTAIN A DOWN AND LOCKED LANDING GEAR INDICATION FAILED. THE PILOT ELECTED TO LAND GEAR UP AT IWA. MINOR AIRCRAFT DAMAGE. NO INJURIES TO THE OCCUPANTS. AN INVESTIGATION SHOWED THAT THE NOSE GEAR HYDRAULIC ACTUATOR PISTON FAILED IN THE THREADED AREA OF THE ROD END BEARING ATTACHMENT.