N91BV

HISTORY OF FLIGHT

On October 4, 2011, about 1315 mountain daylight time, an experimental Vaughn Pulsar airplane, N91BV, impacted the terrain about one-half mile south of the departure end of Runway 16, at South Valley Regional Airport, West Jordon, Utah. Both the certified flight instructor and his passenger received fatal injuries, and the airplane, which had been purchased earlier that day by the passenger, sustained substantial damage. The pilot of the 14 Code of Federal Regulations Part 91 personal flight was departing South Valley Regional Airport in visual meteorological conditions, with an intended destination of Nephi, Utah. No flight plan had been filed.

According to the previous owner, the individual who he sold the airplane to on the day of the accident had come to see it about two weeks earlier. Although the airplane was not flown at that time, the owner, accompanied by the potential buyer, started it up, taxied it along the taxiway, performed an engine run-up check, and then taxied it back to the hangar. Reportedly, the engine ran well on that day, and subsequently, the potential buyer advised the owner that he was going to purchase the airplane. The buyer also told the owner that he would have to make arrangements for someone else to come pick up the airplane because he was not a rated pilot. He later advised the owner that he and a flight instructor would come pick up the airplane, and that the flight instructor would later be using the airplane to give him the instruction necessary to earn his Sport Pilot license.

According to the previous owner, who knew the gross weight limitations of the airplane, when the purchaser called to advise him that he and the flight instructor would be picking up the airplane together, he asked him what their approximate weights were. Reportedly, the purchaser said that they were each in the 180 to 190 pound range. But, when the buyer and the flight instructor arrived on the day of the accident, it appeared to the owner that the weight of the flight instructor was higher than he had been told. He therefor advised the new owner and the flight instructor that they may be near the maximum gross weight limit of the airplane, and told them they should not add any more fuel to the 9 gallons already onboard. The seller also handed the instructor pilot a copy of the weight and balance sheet, so that he could perform an accurate gross weight calculation. Then, after giving the new owner the keys to the airplane and a box full of airplane associated paperwork, the seller spent a little time talking to both individuals about the airplane and its systems. He then left the airport to go back to work. He was not there when the new owner and the instructor pilot entered the airplane to prepare for departure.

Although the investigation did not find any witnesses who observed the two individuals again until they taxied out for takeoff, no records where found at the airport of any additional fuel being added prior to departure. The next time the airplane and its occupants were spotted was about 5 minutes before they took off, when the airplane was seen taxiing to the northern end of runway 16. There, according to witnesses, the pilot stopped in the run-up area before taking off, but it is unknown whether an engine run-up check was completed. The pilot then taxied onto runway 16, where he initiated the takeoff roll.

When the instructor pilot was taxiing out for takeoff, the airplane passed near a flight instructor who had seen it fly before, and who had a friend who had expressed a possible interest in purchasing the airplane. After the airplane taxied by, the flight instructor went inside a nearby building to advise his friend that it appeared the airplane was taxiing out for takeoff. Then the flight instructor and his friend went back outside for the specific purpose of watching the airplane takeoff. According to that flight instructor, when it came by their location, which was about half way down the 5,860 foot runway, the airplane had already lifted off the runway, and its engine sounded to them like it was making full power. At that point the airplane was just above the runway surface and still appeared to be in ground effect. It was reportedly just barely climbing, and was in a repeated porpoising sequence; whereupon each time the airplane’s nose was raised, it would climb only a few feet before the pilot lowered it again to near a level flight attitude. As the airplane neared the departure end of the runway, another flight instructor, who was waiting to takeoff next, transmitted over the radio, “Experimental aircraft on departure, are you having technical difficulties?” To that transmission, the accident pilot responded, “No, it’s just a weak aircraft.” The porpoising sequence then continued until the airplane reached a point about one-half mile off the end of the runway about 75 feet above ground level (agl). It then appeared that the pilot established a shallow right turn, followed soon thereafter by an increase of the bank angle to near 90 degrees and a drop of the nose to about 45 degrees below the horizon. The airplane then made a rapid descent into the terrain.

PESONNELL INFORMATION

The pilot was a 28 year old male, who held both a commercial pilot certificate and a certified flight instructor certificate. His pilot ratings were for single-engine land airplanes and multi-engine land airplanes, and he held an airplane instrument rating. His instructor ratings were for instruction in single-engine airplanes, multi-engine airplanes, and instrument instruction in airplanes. His last airman’s medical, a Class 1 without waivers or limitations, was completed on September 16, 2011. Based upon information provided by his airman’s medical, it is estimated that he had accumulated a total of about 2,100 hours of flight time. It is not known if he had accumulated any flight time in the make and model of airplane involved in the accident.

AIRCRAFT INFORMATION

The airplane was a 1992 kit-built experimental Vaughn Pulsar with a total engine and airframe time of about 250 hours. Its engine was a Rotax 582 Mod 90 of 65 horsepower, with a model 3M23 fixed-pitch composite propeller. Its last recorded 100 hour inspection was signed off on June 30, 2011. Its original maximum allowable gross weight was 870 pounds, but an undated pen and ink notation on the original weight and balance sheet indicated that the maximum allowable gross weight had been increased to 1,000 pounds as per information from Aero Designs (the kit manufacturer). The investigation also discovered a weight and balance calculation sheet from an earlier undated dual instructional flight which listed the actual total ramp weight for that fight as 963 pounds, and the maximum allowable gross weight as 1,000 pounds.

METEOROLOGICAL INFORMATION

About 20 minutes prior to the accident, the 1253 recorded aviation surface weather observation (METAR) at Salt Lake City International Airport (KSLC), which is located about 10 miles north of South Valley Regional Airport, indicated a wind from 200 degrees at 14 knots gusting to 19 knots, 10 miles visibility, few clouds at 6,000 feet, scattered towering cumulus clouds with bases at 9,000 feet, scattered clouds at 20,000 feet, a temperature of 23 degrees C, a dew point of 08 degrees C, and an altimeter setting of 29.86 inches.

The KSLC special METAR taken at 1338, approximately 25 minutes after the accident, indicated a wind varying in direction from 200 degrees to 270 degrees at 09 knots gusting to 21 knots, 10 miles visibility, thunderstorms with light rain, few cumulonimbus clouds with bases at 4,300 feet, scattered clouds at 7,000 feet, a broken layer at 10,000 feet, a broken layer at 20,000 feet, a temperature of 22 degrees C, a dew point of 08 degrees C, and an altimeter setting of 29.83 inches. The METAR also included the remark that the peak wind since the last METAR had been from 170 degrees at 27 knots at 1311. It further remarked that there was occasional lightening in clouds to the southwest and west, and that there were thunderstorms to the west and southwest moving north.

According to the flight instructor who made the aforementioned radio transmission and then took off as soon as he saw the airplane descend into the terrain, the Automated Weather Observation System (AWOS) information being transmitted at the time of the accident indicated a wind from 150 degrees at 12 knots gusting to 18 knots, a visibility of 10 miles, scattered clouds at 10,000 feet, a temperature of 23 degrees C, a dew point of 7 degrees C, and an altimeter setting of 29.88 inches. He also remarked that during his takeoff, and while he was overhead the accident site, the air was smooth, without a single bump or downdraft.

The flight instructor, who with his friend, had watched the takeoff from the ground, reported that he had been working around the airport since 0700, and had witnessed multiple small rain cells move through the area. But, he further reported that at the time of the accident, there was no cell over the airport or the accident area, and that the wind was nearly steady about 15 knots (varying about 1 to 3 knots), and almost directly down the runway. He did observe one rain cell to the southwest, but he did not believe that it had resulted in any wind gusts or microburst activity in the area of the airport at the time of the accident.

Based upon a field elevation of 4,670 feet, a temperature of 23 degrees C, a dew point of 8 degrees C, and an altimeter setting of 29.83 inches, the density altitude at the time of takeoff was calculated to be 6,790 feet.

COMMUNICATIONS

The only known radio communication between an occupant of the accident airplane and someone else, was what appeared to be the instructor pilot’s res...