N744TWRobinson Helicopter R44 II · 2005

On May 17, 2019, about 1034 mountain daylight time, a Robinson R44 helicopter, N744TW, was substantially damaged when it was involved in an accident near Alpine, Utah. The pilot and passenger sustained fatal injuries. The helicopter was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot’s mother stated that the pilot kept the helicopter at his home in Myton, Utah, and that he and his wife had planned to fly to South Valley Regional Airport (U42), West Jordan, Utah, to pick up a second passenger before proceeding to Phoenix, Arizona. She saw the helicopter depart at 0930 and stated that it was raining lightly at that time. At 1022, she received a text message from the passenger stating that they were “17 minutes out.” At 1025, she received a text stating that “the flight was smooth.” At 1027, she received a short video showing the helicopter above a thick cloud layer with no discernable horizon. Some of the cloud tops appeared above the helicopter, as seen in Figure 1.

Figure 1. Images recorded by a passenger.

Radar data provided by the Federal Aviation Administration (FAA) revealed a target correlated to the accident helicopter first appear on radar at 0956 at an altitude of 10,400 ft mean sea level (msl), on a heading of 309° about 44 miles west of the pilot’s residence. The helicopter continued generally on a west-northwest course, as shown in Figure 2. The airspeed initially varied from 37 to 88 knots ground speed but stabilized to about 85 knots for most of the flight. The helicopter climbed to 13,000 ft msl at 1007 and remained between 12,700 and 13,000 ft ft msl until about 1030, when it descended below 12,500 ft msl. At 1031, the helicopter began a right descending right turn that continued until radar contact was lost at 1033 at an altitude of 9,200 ft msl and groundspeed of 108 knots, about 1,650 ft from the accident site. The data revealed that the helicopter completed about 2 1/2 360° turns before radar contact was lost. (see Figure 3.)

Figure 2. Recorded radar targets showing the likely route of flight.

Figure 3. Radar targets showing the turning descent. Path lines show estimated track.

Review of the pilot's logbook revealed about 145.1 total hours of flight experience: about 30.5 hours in the Robinson R44 helicopter, and about 113.4 hours in the Robinson R22 helicopter. The logbook contained no entries for instrument flight training.

The pilot’s flight instructor stated that he had last provided instruction to the pilot about one year before the accident. The instructor followed a private pilot training syllabus that did not include instrument training. The instructor stated that they had done some instrument flight rules (IFR) training, and less than 5 hours “hood work” (with a view limiting device) because the pilot wanted to try it. He stated that they had discussed visual flight rules (VFR) cloud clearance requirements. The instructor stated that they may have done some unusual attitude recoveries.

The Robinson R44 Raven II helicopter, serial number 10702, was manufactured in 2005, and was approved for VFR flights in day and night conditions. The helicopter was not equipped with a supplemental oxygen system, nor were any supplemental oxygen provisions found at the accident site. A review of the maintenance records revealed that the last annual inspection was completed on January 13, 2019, and the associated entry stated, “Inspected avionics for security and basic electrical operation.” There were no instrument discrepancies recorded.

According to Leidos, the pilot did not have any contact with them or any other third-party vendors on the day or the day prior of the accident.

Roosevelt Municipal Airport (74V), Roosevelt, Utah, located about 5 miles north of the pilot’s residence, about the time of departure reported wind from 080° at 3 knots, 10 statute miles visibility, broken clouds at 7,500 ft above ground level (agl), temperature 10°C, dew point temperature 3°C, altimeter setting of 29.77 inches of mercury.

Reported weather at U42 about the time of the accident included wind from 080° at 4 knots, visibility of 10 statute miles or greater, scattered clouds at 1,900 feet agl, ceiling broken at 4,300 feet agl, overcast at 5,000 feet agl, temperature 7°C, dew point temperature of 5°C, altimeter setting of 29.83 inches of mercury.

AIRMET Sierra was issued at 0845 for moderate icing between the freezing level and 18,000 ft msl and mountain obscuration by clouds, precipitation, or mist, and was active for the accident location at the accident time. Weather radar imagery above the accident location between about 8,600 ft and 14,200 ft msl identified reflectivity consistent with light rain in an area that included the accident site. (see Figure 4.)

Figure 4. Weather radar imagery

Satellite imagery identified cloudy conditions over the accident site, with analysis indicating cloud tops of about 13,000 ft msl along the route of flight and a cloud top height of about 19,500 ft msl during the final portions of the flight, as shown in Figure 5.

Figure 5. Satellite imagery showing clouds.

The Robinson R44 Raven II helicopter, serial number 10702, was manufactured in 2005, and was approved for VFR flights in day and night conditions. The helicopter was not equipped with a supplemental oxygen system, nor were any supplemental oxygen provisions found at the accident site. A review of the maintenance records revealed that the last annual inspection was completed on January 13, 2019, and the associated entry stated, “Inspected avionics for security and basic electrical operation.” There were no instrument discrepancies recorded.

The debris field was about 7,656 ft msl elevation, oriented on a magnetic heading of 127° and was about 125 ft in length. The first piece of wreckage in the debris path was a small portion of a tail rotor blade. The empennage separated from the tail cone, and the tail cone separated from the fuselage. The fuselage came to rest on its right side, with the cabin portion of the fuselage fractured and lying on its left side. Both landing skids separated from the fuselage. The main rotor blades remained attached to the hub and were bowed down. The main rotor hub remained attached to the driveshaft, and the pylon remained attached to the transmission.

Fuel remaining at the time of the accident was estimated to be about 13 gallons, based on a fuel consumption estimate of 15 gallons per hour, the last recorded fuel purchase of 39 gallons and a subsequent flight time of 2.25 hours.

Examination of the recovered airframe, flight control system components, and engine revealed no mechanical malfunctions or anomalies that would have precluded normal operation.

The Pilot’s Handbook of Aeronautical Knowledge, FAA-H-8083-25B, states in part:

Under normal flight conditions, when there is a visual reference to the horizon and ground, the sensory system in the inner ear helps to identify the pitch, roll, and yaw movements of the aircraft. When visual contact with the horizon is lost, the vestibular system becomes unreliable. Without visual references outside the aircraft, there are many situations in which normal motions and forces create convincing illusions that are difficult to overcome…Unless a pilot has many hours of training in instrument flight, flight should be avoided in reduced visibility or at night when the horizon is not visible. A pilot can reduce susceptibility to disorienting illusions through training and awareness and learning to rely totally on flight instruments.

Be physically tuned for flight into reduced visibility. Ensure proper rest, adequate diet, and, if flying at night, allow for night adaptation. Remember that illness, medication, alcohol, fatigue, sleep loss, and mild hypoxia are likely to increase susceptibility to spatial disorientation.

The Pilot’s Operating Handbook for the R44 contains a Safety Notice (SN-18) which states in part:

Flying a helicopter in obscured visibility due to fog, snow, low ceiling, or even dark night can be fatal. Helicopters have less inherent stability and much faster roll and pitch rates than airplanes. Loss of the pilot’s outside visual reference, even for a moment, can result in disorientation, wrong control inputs, and an uncontrolled crash. This type of situation is likely to occur when a pilot attempts to fly through a partially obscured area and realizes too late that he is losing visibility.

Toxicology testing performed at two laboratories identified 300 ng/ml of amphetamine in blood obtained from the inferior vena cava; 346 ng/ml in heart blood and 4167 ng/ml in urine; phenylpropanolamine and oxycodone in heart blood and urine; oxymorphone, a metabolite of oxycodone in urine; and oxazepam in urine.