HN-196 Inspect landing gear/struts 10/01/84 6. Connect with the definitive source for global and local news. Farmer said he kicked out the front window and escaped. Coroner on the basis of family request and that Mr. Allison was an organ donor. high fence. and free of metal deposits. He stated that at that point, the ride became very violent, and he became scared. arm nuts 6/15/90 3. altitude of about 50 feet. A licensed airplane pilot, Allison had received his helicopter rating a year before the crash. Although a licenced airplane pilot, Allison had only received his helicopter rating about a year before the crash. The tail rotor pedals were found with the left pedal fully depressed. On Tuesday, the National Transportation Safety Board completed its investigation of the helicoptor accident that killed NASCAR Winston Cup driver Davey Allison. engine. 134. Then the ride became very violent, said Farmer. The tail rotor drive John Corley, a flight instructor for Southeastern Helicopters in Saluda, S.C., who gave Allison the 2.8 hours of training, told the NTSB that Allison demonstrated ″about average″ pilot skills for someone who had not flown a helicopter in six months and had limited experience. A request was made of the investigator for the part and the report for further analysis, however, neither have been offered. The bulkhead torque tube was fractured from the mounts on both sides of the airframe. 1. west side of the racetrack are the stands and race car pit area. A FACTOR RELATED There were the aircraft began to rotate in a counter clockwise direction. long control tube through the tailboom was fractured near sta. Allison had been attempting to land the 2,500-pound helicopter in a parking lot at the speedway when it suddenly rose and began to spin out of control, witnesses said. his(Mr. Allison's) residence and park it until after the race at Talladega. In the race car pit area, there are hours of operation. oscillate from side to side and then climbed to an altitude of approximately 25 feet. He received his helicopter Aviation Insurance Managers Attached to this Report.). COLLECTIVE STICK HOUSING, COLLECTIVE PUSH-PULL ROD & ROD END FROM The metallurgical report stated fatigue as the failure method of the part. door upward across the pilot's door. occupants. The aircraft records were released to Mr. David Fair of the Federal Aviation Administration John Corley Attached to this Report. He stated that at no Both left skid struts were fractured. The Talladega Super Speedway is not a certificated airport. There was some crushing of the left door and the canopy THE HELICOPTER PILOT HAD ATTAINED 9 HOURS OF FLIGHT TIME IN THIS MAKE As a result of having trained on the Robinson R-22, Allison also had a propensity to make his approaches too fast and shallow, Corley said. large stock car racing complex consisting of several thousand acres of open land. The aircraft then banked sharply to the The pilot’s throttle was in the full open position, it said. WASHINGTON (AP) _ A federal investigation of a helicopter accident that killed NASCAR driver Davey Allison found he had less than three hours of training on the chopper he crashed at Talladega Superspeedway in Alabama last July. The cyclic controls were in place. 85 and progressing to sta. turn to the right approximately 30 degrees, and then rapidly ascended to a height above the power There was tube housing aft lugs were fractured. The west end of the area is bounded by a power line approximately 26 feet high. The tail rotor transmission was (sprag) clutch at the engine output assembly operated properly in both directions. helicopter prior to conducting any flights with passengers. with the fractures in the tailboom. to leading edge. HN-188 Install sleeve on tail rotor output shaft 5/21/83 9. ″I did not want to release his belt because he would fall. The accelerate time At that point, the aircraft began to The lateral and longitudinal control tubes under the cockpit seats We would like to show you a description here but the site won’t allow us. The aircraft records do not indicate that the following Mandatory Service Notices had been Information. meteorological conditions existed at the time, and no flight plan had been filed for the personal flight. He blade was fractured at sta. The red blade had a uniform up and aft 70 degree bend starting a 50 foot hover to approximately one foot above the terrain. 255 concurrent THE PILOT'S POOR IN-FLIGHT DECISION TO LAND DOWNWIND IN A CONFINED housing. main transmission. (See Insurance Quotation from The oil cooler drive belt The pilot's tail rotor pedal stems were fractured just above the bulkhead torque tube. Michael Stucker | Andrill Schlumberger, Sugar Land, Texas stucker@sugar-land.anadrill.slb.com | You don't want to know Anadrill's opinion. request was made of the investigator for the part and the report for further analysis, however, neither The 142 were separated from the blade. There was crushing of the airframe from station (sta.) compartment was intact. aircraft. 122. in Talladega, Alabama. barbed wire which was wrapped around the link and hub, and the bearing had pulled out of the The main rotor pitch line poles. received. Allison was hanging upside down in his seat belt, unconscious, Farmer said. He stated that at the completion of The lateral and longitudinal trim actuators were The green pitch housing was upper mast. ″I saw sky. UNCONFINED AREAS WERE LOCATED NEARBY. (BEFORE IMPACT). The stationary and rotating swashplates were intact and attached to the The Media Parking Lot is an asphalt paved area approximately 168 The green pitch housing was destroyed, and the damper assembly was fractured. The overrunning EXAMINATION OF THE AIRCRAFT DID NOT HN-198.1 Corrosion The Hughes 369HS is a five place utility category helicopter powered by an Allison Model 250-C20 1993. One company who offered a quotation, Allison, 32, who had owned the helicopter less than a month, died of massive head injuries. The aircraft wreckage was released to Davey Allison Racing Enterprises, Incorporated on August 5, 1993. David Carl Allison (February 25, 1961 – July 13, 1993) was an American NASCAR driver. 124. The main rotor turned freely in both directions, but did not turn the transmission. had been fractured. Allison's flight instructor stated that during the flight training in the 369HS, take-off and landings, rating in July of 1992, and had accumulated approximately 54 hours of flight time in helicopters. (See Record of Interview of Mr. Red Farmer by FAA Inspector Jerry Yates.). Both skid tubes The green rotor blade had aft and up spar bend at sta. indication of where he braced his feet during the event. Located on the roots remained attached to the hub and did not show significant damage at the root end. But 45 of the 54 hours of helicopter flight time he had logged when he died were in the smaller and slower Robinson R-22 helicopter, the NTSB said. The main transmission turned freely in both directions when turned with the input shaft. were separated from the aircraft, but remained primarily undamaged. A preliminary report of the crash will be released by the NTSB in about a week. The report said a metallurgical examination of the fractured main rotor drive shaft showed that the break was consistent with a violent crash. destroyed. time during the training, had they practiced down wind landings. bent aft at sta. Inspection of the fuel lines did not reveal any vacuum leaks. He said Allison tended to hover at about 25 feet instead of the recommended height of 3 feet. The pilot, Mr. David C. Allison, was employed as a race car driver. accumulated during training for his helicopter rating in a Robinson R-22. called the Media Parking Lot. Allison, 32, who had owned the helicopter less than a month, died of massive head injuries. Although Allison had logged 54 hours total flight time in helicopters, he’d had only 2.8 hours of instruction in the Hughes 369HS helicopter before the accident last July 12, according to the National Transportation Safety Board. Farmer told an investigator this had been his first ride in a helicopter, so he was not sure what to expect. attached to the transmission, and the tail rotor hub and fork bolt were still in place and not fractured. blade end of the link. CONFINED AREA OF THE TALLADEGA SUPER SPEEDWAY, ALTHOUGH OPEN & OF HIS FEET DURING THE EVENT. HN-213 Replace particle separator door 12/18/87 4. All four blade PROPERLY COMPENSATE FOR THE TAILWIND CONDITION. was intact and attached to the airframe, but the Plexiglass was broken and the door was buckled in TO THE ACCIDENT WAS: THE PILOT'S LACK OF TOTAL EXPERIENCE IN THE TYPE POWER LINES. The tail rotor swashplate and pitch links were attached. strap 11/23/83. inches from the tip. would make an appointment with the flight instructor to complete a thorough check out in the Hughes 369HS, which are 275 horse power (HP) at take off, and 240 HP at normal cruise. THE HELICOPTER THEN ASCENDED TO A HEIGHT OF ABOUT 25 FEET, THEN IT The pilots throttle on the Pieces of the aircraft were found as much New York Times News Service THE BALTIMORE SUN Davey Allison, the 1992 Daytona 500 winner and a member of one of stock-car racing's most prominent families, died … The blue pitch link was damaged by a strand of Visual HELICOPTER DURING THE EVENT; HOWEVER, HE DID NOT RECALL THE POSITION 78.5 to sta. upward bend at sta. would have required Mr. Allison to complete 25 hours of flight training in the Hughes 369HS prior to Why Supercars now needs a new "human salt harvester", Bottas: Hamilton's strategy freedom at Imola not unfair, Mercedes didn't believe sensors over Bottas's debris strike, Premier slams "reckless" Adelaide 500 return deal, Magnussen explains gearbox issue that caused headache, Penske's challenge at Phoenix? The forward canopies and cabin overhead canopies were all fractured. no unusual noises or restrictions observed in the transmission, and the magnetic chip plug was clean The part was a section of the co-pilot housing lug which 104, and progressing to sta. The main rotor blades all exhibited lead lag bending and spanwise torsional twisting. 256. attached to the aft tail boom fitting and turned freely. An investigator representing the pilot's family presented a section of the co-pilot's collective, and a head mixer assembly and the stationary swashplate. feet in length and 105 feet in width. numerous locations. The flight departed Birmingham, Alabama about 1415. assembly. METALLURGICAL EXAM OF FRACTURES ON THE COLLECTIVE STICK, The 'A' frame assembly (sta. HN-224 Replacement of tail rotor pitch The white ,red, and blue main rotor damper assemblies were attached to the pitch damaged following a collision with terrain during a landing attempt at the Talladega Super Speedway HN-235 Engine air inlet inspection/rework 3/20/93 2. The main rotor driveshaft was torsionally fractured just above the spline section in the The helicopter began to climb, Farmer said. swashplate attach point. engine specifications, but exceeded power plant limitations for the 250-C20 installation in the swashplate and red pitch link were both functional. and a large piece of the blade was located lodged in the top of the chain link fence between the Metallurgical examination of the fractured main rotor drive shaft showed that the fracture was The pilot's collective stick was fractured at the housing mount, and the copilot's collective torque The Talladega Super Speedway is a 8. He (See Record of Conversation With Mr. collision. The aft left skid tube was fractured just below the step THE SITE WAS 168 FEET LONG & The craft hovered at about 6 inches to a foot above the ground, then Allison attempted to turn to the right and the helicopter ″shot up very quickly,″ he said. An Aircraft Bill of Sale dated June 21, 1993, showed the aircraft was purchased from Stevens He said they approached the parking lot at a normal angle. REVEAL ANY PREIMPACT MALFUNCTION OF THE TAIL ROTOR SYSTEM. The section of tail rotor drive shaft from sta. The aft cargo or passenger The NTSB blamed Allison's inexperience for his "poor inflight decision to land downwind in a confined area that was surrounded by high obstructions."
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