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Accidents · NTSB CEN19LA049 · Final report

Beech 58 accident near Sioux Falls, South Dakota, December 25, 2018

On December 25, 2018 at about 11:03 pm local time, a 1980 Beech 58, registered N6745V, was destroyed in an accident during approach (IFR final approach) near Sioux Falls, South Dakota (Joe Foss Field Airport). It was a personal flight under general aviation rules (Part 91). 2 people were killed. The weather was instrument conditions (cloud, fog or low visibility).

The NTSB's probable cause their words, unchanged

The pilot's failure to maintain adequate airspeed during the instrument approach which led to an aerodynamic stall.

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

What the record shows

Date
December 25, 2018 · about 11:03 pm local time
Place
Sioux Falls, South Dakota · Joe Foss Field Airport · map
Type
Accident
Injuries
2 people were killed.
Weather
instrument conditions (cloud, fog or low visibility)
Aircraft
Beech 58 P, built 1980 · all 58s on the register
Registration
N6745V · no longer on the register · serial TJ-272
Damage
Destroyed
Flight
Personal flight · general aviation rules (Part 91)

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

The pilot and passenger were on a cross-country flight and an instrument flight rules approach in instrument meteorological conditions. According to air traffic control transcripts, an air traffic controller at the destination airport cleared the flight for the RNAV approach for runway 33. According to ADS-B flight track data, the airplane then turned toward the final approach path just inside the initial approach fix at 3,100 ft mean sea level (msl) and 156 knots calibrated airspeed (KCAS). Subsequently, the airplane proceeded west of the final approach centerline, turned back through the centerline to the east, and then back to the west, resembling s-turns through the extended centerline. During the s-turns across the extended centerline, the controller cleared the airplane to land. Two minutes later, the airplane was about 3,000 ft msl and 78 KCAS, and then began to rapidly descend. According to a witness and video footage of the accident, the airplane descended in a steep, nosedown attitude. The witness added that it appeared that he then “saw airplane try to pull out of a dive” just before it impacted the ground. The airplane impacted trees and a building and then came to rest in a residential neighborhood about 200 ft south of the last radar location. The airplane was massively fragmented and a postimpact fire ensued. Impact and fire damage precluded a thorough examination and functional testing of the related airplane systems. Examination of both engines and propeller assemblies revealed signatures consistent with symmetric power development at the time of the accident. According to a family member of the pilot, 3 months before the accident, the pilot was en route at altitude when the airplane suddenly nosed over. According to a work order, 3 weeks before the accident, the autopilot was removed and repaired. The repair station owner reported that, after a flight 3 days before the accident, the pilot told him that he had no issues with the airplane and that the flight was uneventful. A review of the airplane’s flight track showed the pilot making S-turns across the approach course, which is consistent with the pilot hand-flying the approach, not a coupled autopilot approach. Therefore, it is unlikely that the pilot was flying the instrument approach using the autopilot system. Further, although the autopilot system could not be functionally tested due to impact and fire damage, it is unlikely that the autopilot system played a role in the accident if it was not in use. Therefore, based on the radar data, it is likely that the pilot failed to maintain adequate airspeed during the final approach, which resulted in the exceedance of the airplane’s critical angle of attack and a subsequent aerodynamic stall. Given the witness account and surveillance video, it is likely the pilot was attempting to recover from the stall but did not have adequate altitude to do so.

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. Aerodynamic stall/spin during approach (IFR final approach) defining event

The NTSB's findings

  • cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Airspeed › Not attained/maintained
  • Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
  • Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Angle of attack › Not attained/maintained

Pilot

  • Certificate: private
  • Ratings: multi-engine land; single-engine land; instrument: airplane
  • Flight time: 2,448.5 hours in all; 588.2 in this make and model; 6.4 in the last 30 days
  • Last flight review: November 21, 2016
  • Medical certificate: Class 3 (with waivers/limitations)
  • Seat: unk
  • Injury: fatal

The aircraft

  • Airframe total time: 5,585.7 hours
  • Last inspection: annual inspection, February 15, 2018
  • Landing gear: retractable
  • Engine 1: Teledyne Continental TSIO-520-WB (piston); 0 hours total
  • Engine 2: Teledyne Continental TSIO-520-WB (piston); 0 hours total
  • Fire on the ground

The flight

  • Departed from: GRR Grand Rapids MI at 7:07 pm
  • Destination: Y14 Tea SD
  • Flight plan: IFR

Weather at the time

  • Light: dusk
  • Wind: from 040° at 8 knots
  • Visibility: 10 statute miles
  • Sky: overcast at 800 ft
  • Temperature: 30°F (-1°C), dew point 27°F (-3°C)
  • Altimeter: 30.23 inHg
  • Observation at 10:56 pm from FSD, 5 miles away

Injuries

FatalSeriousMinorNone
Flight crew1
Passengers1

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

22 documents, released by the NTSB on December 3, 2020. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.

The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.

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.