# NTSB WPR16FA046: Aerostar S A YAK 52, N912EB, Alpine, WY, January 4, 2016

- Type: NTSB accident investigation
- Classification: Accident · Fatal · Field investigation · Final report
- Date: January 4, 2016, 16:15 local (23:15 UTC)
- Place: Alpine, WY
- Coordinates: 43.160884, -111.04104
- Nearby events: https://openairdocs.org/map.md?lat=43.1609&lon=-111.0410&mi=10
- Phase of flight: [Maneuvering](https://openairdocs.org/ntsb-phases/450) (OpenAirDocs' grouping)
- Defining event: [Maneuvering: Controlled flight into terr/obj (CFIT)](https://openairdocs.org/ntsb-events/120)
- Highest injury: Fatal
- Injuries: 2 fatal
- Status: Completed, report September 18, 2017
- Report: Approved by Office Director
- NTSB office: Western Pacific Region
- Parties: FAA FSDO
- NTSB case key (mKey): 92522
- NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=WPR16FA046
- NTSB report (PDF, downloads): https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/92522/pdf
- NTSB docket: https://data.ntsb.gov/Docket?ProjectID=92522
- Page: https://openairdocs.org/ntsb/WPR16FA046

## Probable cause

The pilot's failure to maintain clearance from snow-covered terrain in flat light conditions.

## Findings

NTSB's coded findings; those marked are part of the probable cause.

- [Attention/monitoring: monitoring environment](https://openairdocs.org/ntsb-findings/02021545): Personnel issues › Psychological · Pilot (probable cause); cases with it: [Aerostar S A YAK-52, 1 case](https://openairdocs.org/ntsb-findings/02021545/cases.md?model=1140003), [All aircraft, 809 cases](https://openairdocs.org/ntsb-findings/02021545/cases.md)
- [Performance/control parameters: altitude](https://openairdocs.org/ntsb-findings/01062012): Aircraft › Aircraft oper/perf/capability · Not attained/maintained (probable cause); cases with it: [Aerostar S A YAK-52, 3 cases](https://openairdocs.org/ntsb-findings/01062012/cases.md?model=1140003), [All aircraft, 1,310 cases](https://openairdocs.org/ntsb-findings/01062012/cases.md)
- [Light condition: flat light](https://openairdocs.org/ntsb-findings/03036025): Environmental issues › Conditions/weather/phenomena · Decision related to condition (probable cause); cases with it: [Aerostar S A YAK-52, 1 case](https://openairdocs.org/ntsb-findings/03036025/cases.md?model=1140003), [All aircraft, 42 cases](https://openairdocs.org/ntsb-findings/03036025/cases.md)
- [Terrain: snowy/icy terrain](https://openairdocs.org/ntsb-findings/03021030): Environmental issues › Physical environment · Awareness of condition (probable cause); cases with it: [Aerostar S A YAK-52, 1 case](https://openairdocs.org/ntsb-findings/03021030/cases.md?model=1140003), [All aircraft, 77 cases](https://openairdocs.org/ntsb-findings/03021030/cases.md)

## Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event best describes what happened.

- [Maneuvering: Controlled flight into terr/obj (CFIT)](https://openairdocs.org/ntsb-events/120) (defining event); cases with it: [Aerostar S A YAK-52, 1 case](https://openairdocs.org/ntsb-events/120/sequence.md?model=1140003), [All aircraft, 1,074 cases](https://openairdocs.org/ntsb-events/120/sequence.md)

## Analysis

The pilot was conducting a local aerobatic flight with a pilot-rated passenger occupying the rear seat (which was equipped with flight controls). The pilot's son was flying another airplane, returning to the home airport after a local sightseeing flight. The airport was at the southeast corner of a reservoir, which surrounded the airport on three sides (all but the east side). The accident site was located on flat, featureless, snow-covered terrain northwest of the airport. The son reported that, as he was flying north away from the airport over the west side of the reservoir, it was frozen over, and covered with snow. He stated that the surface was flat with no cracks, and the lighting was flat as well so that he had difficulty judging his height above the ground. As he continued north, the surface showed some cracks, which helped him with height visualization. About 7 miles north of the airport, he transitioned to the east side of the reservoir, and headed south toward the airport. The son's airplane was about 200 ft above ground level and several miles from the runway on final approach, when an exchange of radio transmissions led the son to believe that his father was going to pass by him. He never saw his father's airplane. An airplane witness had just taken off from the airport in another airplane; he saw the son's airplane on a 2-mile final approach and then saw a debris field forming as the accident airplane impacted the ground behind the son's airplane. Examination of the accident site and the wreckage indicated that the airplane impacted the ground at high speed in a near level attitude, consistent with controlled flight into terrain. No evidence of any preimpact mechanical malfunctions or anomalies was found. It is likely that, as a result of the flat light conditions described by the pilot's son, the pilot did not realize he was descending over the featureless, snow-covered terrain. The pilot had undiagnosed heart disease, which placed him at significant risk for sudden severe impairment/incapacitation from an acute cardiovascular event such as a heart attack, arrhythmia, or stroke. However, the operational evidence indicated that this crash was controlled flight into terrain with a pilot rated passenger in the rear seat who could have taken over in the event the pilot became severely impaired or incapacitated. As a result, it is unlikely the pilot's heart disease contributed to the accident.

## Factual narrative

The FAA pamphlet "Flying in Flat Light and White Out Conditions" states in part: Flat light is an optical illusion, also known as "sector or partial white out." It is not as severe as "white out" but the condition causes pilots to lose their depth-of-field and contrast in vision. Flat light conditions are usually accompanied by overcast skies inhibiting any good visual clues. Such conditions can occur anywhere in the world, primarily in snow covered areas but can occur in dust, sand, mud flats, or on glassy water. Flat light can completely obscure features of the terrain, creating an inability to distinguish distances and closure rates. As a result of this reflected light, it can give pilots the illusion of ascending or descending when actually flying level. Chapter 17 page 10 of the FAA's Pilot's Handbook of Aeronautical Knowledge discusses featureless terrain illusions. It states that an absence of surrounding ground features, as in an overwater approach, over darkened areas, or terrain made featureless by snow, can create an illusion that an aircraft is at a higher altitude than it actually is during a landing approach. This illusion, sometimes referred to as the "black hole approach," causes pilots to fly a lower approach than is desired. On January 4, 2016, about 1615 mountain standard time, an experimental Aerostar SA YAK-52, N912EB, collided with terrain while maneuvering near Alpine Airport, Alpine, Wyoming. The private pilot and the pilot-rated passenger sustained fatal injuries; the airplane was destroyed. The airplane was registered to and operated by Wyoming Wings LLC under the provisions of 14 Code of Federal Regulations Part 91. The local personal flight departed Alpine Airport about 1530. Visual meteorological conditions prevailed, and no flight plan had been filed. Family members reported that the accident airplane departed, and went to an area northwest of the airport where the pilot planned to perform aerobatic maneuvers. Two other airplanes, one flown by the accident passenger's father, and the other by the accident pilot's son, then departed on local sightseeing flights. The passenger's father returned to the airport, landed on runway 13, and turned the airplane toward the southwest on a taxiway as he prepared to depart on runway 31, which was standard practice at the airport when winds permitted. He saw the YAK performing aerobatics west of the airport and heard the accident pilot's son report on a 3-mile final straight in for runway 13. He departed runway 31, and immediately turned 90° to the west to clear the area for the landing traffic. As he reached pattern altitude, he saw the debris field forming on the snow-covered ground behind the accident pilot's son's airplane, which was on a 2-mile final approach. He flew over the site, and broadcast that the YAK was down. He made a couple of passes over the site before landing. He noted that the sky was slightly cloudy, and low light conditions were present. The accidentpilot's son stated that he departed after his father, and flew along the east side of a reservoir before turning south to overfly the family's home. He returned to the north and maneuvered to the west side of the reservoir. As he proceeded north, he descended over the reservoir, which was frozen over and covered with snow. He stated that the surface had no cracks, and the lighting was flat so that he had difficulty judging his height above the ground. As he continued north, the surface showed some cracks, which helped him with height visualization. About 7 miles north of the airport, he transitioned to the east side of the reservoir, and headed south toward the airport. He was about 5 miles from the airport, and made a radio call that he was going to land on runway 13. He saw the accident passenger's father's airplane take off and turn to the west. He was about 100 to 200 ft above the ground and over the reservoir about 3 miles from the airport when he heard his father in the YAK make a radio call indicating that the YAK was either going to join up or do a flyby. Because of that transmission, he decided to do a go-around and fly over the airport rather than land. He reported that he and his father had done formation flying, join ups, and flybys previously, and typically his father would break the maneuver off after the join up and low approach. He looked over his shoulder for the join up at his 4- and 7-o'clock positions, and listened for a radio call from his father. The call did not come, and he never saw the YAK. He then heard the accident passenger's father radio him, and realized that something was wrong. He proceeded to the area where the other airplane was circling, and saw a disturbance in the snow. He flew above the other airplane until it departed to land. An airport resident, who had heard the radio transmissions, went to his window, and was looking for the YAK to fly over. After hearing the conversations, he contacted the pilots in the air and notified the local emergency authorities. The Booneville County Coroner's Office, Idaho Falls, Idaho, completed an autopsy of the pilot, and the cause of death was reported as the effect of blunt force injuries. Examination of the body for natural disease during the autopsy was limited by the severity of the pilot's injuries but identified evidence of severe coronary artery disease with areas of up to 80% stenosis and microscopic evidence of damage to the heart muscle from previous ischemia. The FAA Bioaeronautical Sciences Research Laboratory, Oklahoma City, Oklahoma, performed toxicological testing of specimens from the pilot, which were negative for performance enhancing drugs or alcohol. The laboratory did not perform tests for carbon monoxide or cyanide. The drug valsartan was detected in liver and kidney. A review of medical records indicated that the 61-year-old male pilot, who was seated in the front seat, had reported to the FAA that he had high blood pressure, high cholesterol, and arecent diagnosis of diabetes. At time of his last medical exam, on May 24, 2014, he reported using valsartan for blood pressure, ezetimibe and simvastatin in combination as well as fenofibrate for high cholesterol, and metformin for diabetes. None of these medications carry warnings about performance impairment. His treating physician reported excellent control of his diabetes on his treatment regimen with a hemoglobin A1C of 6.6%. The 17-year-old female passenger, who was seated in the rear seat, had reported no medical conditions and no medications to the FAA during her only medical exam, dated May 21, 2014. No autopsy was performed and no specimens for toxicology analysis were obtained. The airport was at the southeast corner of the reservoir, which surrounded the airport on three sides (all but the east side). The accident site was located on flat, featureless, snow-covered terrain about 2 miles northwest of the airport, and near the extended centerline for the final approach to runway 13. The debris field was 578 ft long on a magnetic heading of 122°. The first identified point of contact was a crater, which measured about 15 ft long, 6 ft wide, and 2 ft deep. On the left side of the beginning of the crater was a piece of the left wing-tip and the pitot tube with about 1 ft buried in the soft dirt; a few feet farther into the crater was a piece of the left aileron. At the end of the crater was a separated propeller blade. The left wing fragmented into several pieces, and most of them were in the first half of the debris field. The inverted right wing was about 400 ft into the debris field along the debris path centerline. The main wreckage consisting of the fuselage and empennage was 500 ft into the debris field. The last major component was the separated engine, which was at the end of the debris field. The airplane was highly fragmented. All control surfaces and major components of the airplane were identified in the debris field. The airplane had flight controls for both the front and rear seat pilots. All identified disconnects in flight control push-pull tubes were angular and jagged; all identified disconnects in flight control cables were splayed. The propeller was separated from the engine crankshaft along with the crankshaft propeller flange. The spinner was crushed and exhibited thermal damage. Two of the three blades were separated from the propeller hub. The remaining propeller blade was melted outboard of the mid span point. The remaining portion of crankshaft exposed from the front of the engine case exhibited extensive spiral cracking throughout half of its respective circumference.

## Aircraft

- Registration: [N912EB](https://openairdocs.org/deregistered/N912EB-2017-12-21), registration cancelled 2017-12-21, S/N 832912, built 1983 (OpenAirDocs)
- Reported make and model: AEROSTAR S A YAK 52 (NO SERIES)
- Registry model: [Aerostar S A YAK-52](https://openairdocs.org/model/aerostar-s-a-yak-52) (registry code 1140003) (OpenAirDocs)
- Registry engine: [Vedeneyev M14P](https://openairdocs.org/engine/vedeneyev-m14p) (registry code 63601, reciprocating) (OpenAirDocs)
- Category: Airplane
- Serial number: 832912
- Year built: 1983
- Engines: VENDENYEV M14P reciprocating
- Damage: Destroyed
- Flight: Personal, Part 91
- Airworthiness certificate: Special, Experimental (Special)
- Last inspection: Condition, February 17, 2015
- Departed: K46U, Alpine, WY
- Destination: K46U, Alpine, WY

## Flight crew

As NTSB recorded them. NTSB leaves out names.

- Pilot; age 61; injuries: fatal; private; airplane ratings: single-engine land; instrument ratings: airplane; medical: class 3, with waivers/limitations; seat: front; restraint: 5-point; toxicology performed; flight hours: 2,250 total
- Pilot-rated passenger; age 17; injuries: fatal; private; airplane ratings: single-engine land; medical: class 3, without waivers/limitations; seat: rear; restraint: 5-point; flight hours: 250 total

## Weather

- Conditions: Visual (VMC), Day
- Wind: calm
- Visibility: 10 statute miles
- Lowest ceiling: none
- Temperature: 27 °F, dew point 18 °F
- Altimeter: 29.94 inHg
- Observed at: K46U, 2 nm away

## FAA reports on this event (1)

The FAA's own accident and incident reports, matched to the aircraft by N-number and date (OpenAirDocs).

- [Accident 20160104000289A](https://openairdocs.org/incident/20160104000289A), Jan 4, 2016: Aerostar S A YAK-52, Alpine, WY, Destroyed, 2 fatal. On 01/04/2016@1530 near Alpine airpark (46U) a yak 52 was conducting maneuvers that were described by witnesses as aerobatic (loops and rolls). A pilot and a…

## Docket (9 files)

The files NTSB released with the investigation on September 14, 2017, on NTSB's docket system: https://data.ntsb.gov/Docket?ProjectID=92522. 5.8 MB in all.

- Cockpit Display Factual Report (item 1, .PDF, 38 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40456176&FileExtension=.PDF&FileName=Cockpit%20Display%20Factual%20Report-Master.PDF
- NTSB Medical Officer Factual Report (item 2, .PDF, 503 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40456177&FileExtension=.PDF&FileName=NTSB%20Medical%20Officer%20Factual%20Report-Master.PDF
- Witness Statements (item 3, .PDF, 113 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40456178&FileExtension=.PDF&FileName=Witness%20Statements-Master.PDF
- Wreckage Diagrams (item 4, .PDF, 410 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40456179&FileExtension=.PDF&FileName=Wreckage%20Diagrams-Master.PDF
- NTSB On Site Wreckage Examination Report (item 5, .PDF, 12 photos, 1.6 MB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40456180&FileExtension=.PDF&FileName=NTSB%20On%20Site%20Wreckage%20Examination%20Report-Master.PDF
- NTSB Airframe and Engine Exam Report (item 6, .PDF, 11 photos, 1.8 MB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40456181&FileExtension=.PDF&FileName=NTSB%20Airframe%20and%20Engine%20Exam%20Report-Master.PDF
- Pilot Flight Time Information (item 7, .PDF, 626 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40456182&FileExtension=.PDF&FileName=Pilot%20Flight%20Time%20Information-Master.PDF
- Maintenance Condition Inspection (item 8, .PDF, 383 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40456183&FileExtension=.PDF&FileName=Maintenance%20Condition%20Inspection-Master.PDF
- Toxicological Report (item 9, .PDF, 344 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40456184&FileExtension=.PDF&FileName=Toxicological%20Report-Master.PDF

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

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