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Accidents · NTSB WPR20LA001 · Final report

Buckeye BREEZE accident near Moore, Utah, October 5, 2019

On October 5, 2019 at about 5:40 pm local time, a 2002 Buckeye BREEZE (powered parachute), registered N582UT, was substantially damaged in an accident during initial climb near Moore, Utah. It was a personal flight under general aviation rules (Part 91). 1 person was killed. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The pilot’s improper preflight inspection and detection of a pinch point in the steering line, which resulted in a loss of control in flight and impact with terrain.

Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.

What the record shows

Date
October 5, 2019 · about 5:40 pm local time
Place
Moore, Utah · map
Type
Accident
Injuries
1 person was killed.
Weather
visual conditions (good weather)
Aircraft
Buckeye BREEZE No Series, built 2002 · all BREEZEs on the register
Registration
N582UT · registry record · serial 2137
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

The NTSB's narrative final · quoted from the NTSB record

The pilot flew to a landmark in his powered parachute aircraft with a group of four other powered parachute aircraft. After landing and spending some time at the landmark, the pilot and the group then returned to their aircraft to depart. The first two aircraft departed the area and circled above the takeoff area while they waited for the other aircraft to depart. Each of the pilots had established communications on a common radio frequency that they used to announce their position and intentions. The accident aircraft lifted off the ground about 200 ft and immediately entered a steep left bank angle. The pilot reported over the radio that he was experiencing a problem, and a member of the group advised him to land. While still in a steep left turn, the aircraft made about one and a half revolutions near the departure area then began a steady descent from a low altitude. The aircraft impacted the ground and came to rest on its right side. A postaccident photograph showed the left steering line draped over a bracket that attached the light beacon to the aircraft frame. A technical expert described how the steering line could have become wrapped around the bracket by moving the riser that was positioned above it. This would have created a pinch point and prevented the line from being moved in any direction, thus inhibiting the pilot’s ability to steer the aircraft. As there were no other mechanical anomalies with the aircraft, the pinch point in the steering line was likely the problem the pilot reported during the accident flight. It is unknown if the pilot performed any preflight inspection of the aircraft before departing on the accident flight. However, had he performed a thorough inspection of the steering lines and pulled them taut as discussed in the Federal Aviation Administration’s guidance, it is likely that he would have detected the pinch point and prevented the in-flight loss of control. Thus, the pilot’s improper preflight inspection and failure to ensure the continuity of the aircraft steering lines resulted in a loss of control in flight and impact with terrain.

The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.

The factual record from the NTSB's investigation tables, in plain English

What happened, in order

  1. Flight control sys malf/fail during initial climb defining event
  2. Collision with terrain or object (not controlled flight into terrain) during emergency descent

The NTSB's findings

  • Personnel issues › Task performance › Inspection › Preflight inspection › Pilot
  • Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Lateral/bank control › Malfunction
  • Aircraft › Aircraft systems › Flight control system › (general) › Malfunction

Pilot

  • Certificate: private
  • Ratings: single-engine land
  • Flight time: 300 hours in all; 104 in this make and model
  • Last flight review: October 4, 2019
  • Medical certificate: Sport Pilot
  • Seat: frt
  • Injury: fatal

The aircraft

  • Last inspection: condition inspection, November 15, 2018; 4 hours since
  • Maximum gross weight: 1,000 lb
  • Seats: 2
  • Landing gear: fixed
  • Engine: Rotax 582 (piston); 0 hours total

The flight

  • Departed from: Moore UT at 5:40 pm
  • Destination: 69V Huntington UT
  • Flight plan: none

Weather at the time

  • Light: daylight
  • Wind: from 170° at 4 knots
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 55°F (13°C), dew point 5°F (-15°C)
  • Altimeter: 30.28 inHg
  • Observation at 5:53 pm from PUC, 39 miles away

Injuries

FatalSeriousMinorNone
Flight crew1

Documents from the investigation the NTSB's docket: the evidence folder behind the report

The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the docket at the NTSB.

Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.