RENO, NV, USA
N115R
R&K SPECIAL 01
THE PILOT WAS FLYING HIS HOMEBUILT EXPERIMENTAL BIPLANE ON THE SMALL (3 MILE) RACE COURSE AT THE RENO NATIONAL AIR RACES. WITNESSES REPORTED THAT AFTER MAKING SEVERAL LAPS AT A HIGHER ALTITUDE, A DESCENT WAS MADE TO THE SAME ALTITUDE THAT PREVIOUS PILOTS HAD USE TO QUALIFY. THE AIRPLANE HAD 'ROUNDED' THE PYLONS & WAS FLYING DOWN THE EAST STRAIGHTAWAY, WHEN WITNESSES 'OBSERVED A SLIGHT ROLL, A ROLL CORRECTION AND IMMEDIATE PITCH DOWN . . .' ANOTHER WITNESS SAID 'PILOT WAGGLED WINGS AND PORPOISED TWICE, SECOND PORPOISE INTO GROUND.' THE PILOT SAID HE WAS FLYING WINGS LEVEL, FROM AN ALTITUDE OF APPROXIMATELY 50 FEET, WHEN THERE WAS A SLIGHT LEFT WING DROP FOLLOWED BY A SEVERE PITCH DOWN. HE CORRECTED BY LEVELING THE WINGS & 'LOCKING' THE STICK IN A PITCH UP POSITION, BUT REPORTEDLY, THE AIRPLANE STRUCK THE GROUND TAIL FIRST. NO PREIMPACT PART FAILURE OR MALFUNCTION WAS FOUND. THE PILOT INDICATED THAT HE MAY HAVE ENCOUNTERED SEVERE WINDSHEAR OR A WHIRLWIND. WAKE TURBULENCE FROM A PREVIOUS LAP WAS NEITHER RULED OUT NOR VERIFIED.
On September 14, 1993, about 1055 hours Pacific daylight time, a homebuilt experimental R and K Special airplane, N115R, collided with terrain while on a timing run at the Reno National Air Races, Reno, Nevada. The airplane was destroyed and the commercial rated pilot received serious injuries. The pilot stated that he made a slight roll correction prior to the airplane pitching down and contacting the ground. Crew witnesses stated that: "Racer number 6 was the last biplane flying in the practice/qualification session. The pilot made several laps at a higher altitude. He then descended to what appeared to be the same altitude the previous biplanes had used to qualify. As the pilot approached the start/finish line, they observed a slight roll, a roll correction, and an immediate pitch down at about 20 degrees with wings level to ground impact." The pilot reported that witnesses told him that the airplane hit the ground tail first. He also stated that information provided by other race pilots indicated that the airplane encountered a severe windshear/whirlwind. The aircraft was examined by an FAA airworthiness inspector who reported that no preimpact mechanical malfunctions or failures were evident.
THE PILOT'S LOSS OF CONTROL DUE TO AN UNDETERMINED ENCOUNTER WITH AN UNFAVORABLE WIND/AIR CONDITION IN THE FORM OF A DUST DEVIL, WINDSHEAR, OR WAKE TURBULENCE FROM A PREVIOUS LAP. A RELATED FACTOR IN THE ACCIDENT WAS: THE LOW ALTITUDE AT THE TIME OF THE ENCOUNTER, WHICH LIMITED THE TIME AVAILABLE FOR THE PILOT TO CORRECT THE LOSS OF CONTROL.
Source: NTSB Aviation Accident Database
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