Cessna 172 N6929H

Summary

On 3 July 2020 at about 13:22 local time, a Cessna 172 registered N6929H, operated by Tyson Colby Brummett, was involved in an accident near Alpine, Utah, United States. 4 people were on board and 4 died. The aircraft was destroyed. The NTSB has published a probable cause for this accident; it is quoted in full below.

Date

3 July 2020 at 13:22

Classification

Accident

Location

Alpine, Utah, United States

Coordinates

40.4992, -111.6581

Aircraft

Cessna 172

Registration

N6929H

Category

Airplane

Year built

1975

Engines

1

Operator

Tyson Colby Brummett

Operating rule

Part 91: General Aviation

Purpose of flight

Personal

Phase of flight

Not recorded

Route

Salt Lake City → Salt Lake City

Aircraft damage

Destroyed

Weather

VMC

Light

Day

NTSB number

WPR20LA203

4 people died.

The pilot’s exceedance of the airplane’s critical angle-of-attack while maneuvering in a canyon, which resulted in a loss of airplane control.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

The pilot and three passengers departed the airport for a daytime personal flight in favorable weather conditions. Radar data indicated the airplane flew on a southbound heading for about 25 minutes, steadily climbing to an altitude of 6,200 feet, before turning to the northeast and flying over a lake. The airplane continued on a north/northeast heading and climbed to an altitude of 8,785 feet over the next 16 minutes. It disappeared off radar 4 minutes later after performing a 270º turn in a canyon. A witness in the area observed the airplane approach the canyon headed in a northwest direction and noted that he thought the airplane was too low to clear the terrain and depart the canyon. He observed the airplane enter a “tight, right banking turn” in the canyon. The airplane leveled off after turning about 180º, followed by a couple of left and right wing-tip oscillations before it entered a clockwise, corkscrew spin and disappeared from view in a vertical, nose-down attitude. The witness reported that the airplane’s engine was producing the same, constant sound until it started to vertically descend, and the noise started to oscillate. Examination of the airplane and engine revealed no preimpact mechanical anomalies, and damage to the crankshaft flange and propeller was consistent with the engine producing power at the time of impact. Additionally, autopsy and toxicology of the pilot did not reveal evidence of physiological impairment or incapacitation. The radar data, witness statement, and damage to the airplane were all consistent with a loss of control after the pilot exceeded the airplane’s critical angle-of-attack while maneuvering in the canyon.

Quoted verbatim from the NTSB record.