On October 11, 2007, about 1642 eastern daylight time, a Piper PA-46-310P, N383SA, registered to and operated by Striking Flight Services, Inc., experienced collapse of the nose landing gear during the landing roll at Dekalb-Peachtree Airport (PDK), Atlanta, Georgia. Visual meteorological conditions prevailed at the time and an instrument flight rules flight plan was filed for the 14 Code of Federal Regulations (CFR) Part 91 business flight, from Augusta Regional Airport at Bush Field (AGS), Augusta, Georgia, to PDK. The airplane was substantially damaged and the certificated private pilot and two passengers were not injured. The flight originated about 1545, from AGS. The pilot stated that he listened to the automated terminal information service (ATIS) when the flight was near the destination airport, which indicated the wind was from 330 degrees at 14 knots, with gusts to 16 knots. The flight proceeded to the destination airport where he entered the traffic pattern for runway 2R. He lowered the landing gear using the normal gear extension system during the downwind leg, turned onto base leg, then onto final leg, and while on final approach, requested a wind check with PDK air traffic control tower (ATCT). The tower controller advised that the wind was from 320 degrees at 6 knots. The flight was cleared to land, and the airplane touched down first on the main landing gears, followed by the nose landing gear. The airplane then "...began to pull to the left violently and uncontrollably for no apparent reason." He applied right rudder input but the airplane traveled off the left side of the runway onto grass, and came to rest upright in a nose-low attitude, with the nose landing gear collapsed. A surface observation weather report taken at PDK at 1653, or approximately 11 minutes after the accident, indicated the wind was from 310 degrees at 11 knots, with gusts to 17 knots. The damage to the airplane was initially reported to National Transportation Safety Board as being minor; however, subsequent inspection of it by a manufacturer representative revealed damage to the right wing main spar. At the time of the inspection by the representative (1 week after the occurrence), the nose landing gear assembly was removed. The airplane and runway were examined by a Federal Aviation Administration (FAA) airworthiness inspector. With respect to the airplane, the nose landing gear was collapsed and displaced to the left, and a lug of the nose landing gear trunnion was fractured. The nose landing gear was removed from the airplane, and the fractured lug was later submitted to the Safety Board's Materials Laboratory, Washington, DC. No other discrepancies associated with the nose landing gear steering system were reported. The right side of the nose landing gear wheel displayed coarse scratches consistent with runway contact. Inspection of the approach end of runway 2R revealed two parallel black colored arching skid marks, which continued off the runway onto grass near taxiway F. The precise origin of the skid marks could not be determined. The observed marks were consistent with being made by the nose and right main landing gear tires, and were located left of the runway centerline. The mark associated with the nose landing gear tire was darker in color. The inspector examined the skid mark associated with the nose landing gear and estimated it was approximately 70 degrees from being centered, or aligned. Examination of the fractured right hand lug of the nose landing gear trunnion, by personnel from the Safety Board's Materials Laboratory, revealed it was fractured in two places. The first fracture was located through the lug at a thread hole and the second fracture was approximately 90 degrees around the lug. The observed deformation and fracture patterns at the threaded hole were consistent with tensile overstress separation, while those at the other fracture location were typical of bending fracture. By design, the nose landing gear assembly extends forward pivoting about the trunnion mount. Located above the trunnion mount is a steering horn and rub block which are connected through the trunnion to the lower strut and tire. The steering horn, rub block, lower strut, and tire rotate 90 degrees clockwise during landing gear extension, positioning the tire parallel to the longitudinal axis of the airplane when it is down and locked. The rub block contacts a portion of the tubular engine mount during extension and causes the 90-degree clockwise rotation of the lower strut. Once extended, the nose wheel steering and rudder are interconnected. According to the aircraft maintenance manual, there are two mechanical reasons why the nose landing gear tire would fail to straighten during landing gear extension. The first reason is due to incorrect rigging of the nose gear steering, and the second is that the steering arm roller is sheared at the top of the nose landing gear strut. Due to the damage to the nose landing gear trunnion, no determination could be made as to whether the rigging of the nose gear steering was correct. As previously reported, the FAA inspector did not report any discrepancies associated with the nose landing gear steering. An operational issue associated with rudder input at nose landing gear touchdown can also result in the nose wheel not being aligned with the runway as the nose landing gear contacts it. The pilot did not report having rudder input applied at touchdown. The airplane was last inspected in accordance with an annual inspection on November 6, 2006, using the manufacturer's maintenance manual. The airplane total time at that time was 4,258.9 hours. The airplane had accumulated 244.7 hours since the inspection, at the time of the accident.