The U.S. aircraft register, updated daily
Accidents · NTSB CEN23FA113 · Final report

Beech B200 accident near Little Rock, Arkansas, February 22, 2023

On February 22, 2023 at about 5:56 pm local time, a 1983 Beech B200, registered N55PC, was destroyed in an accident during initial climb near Little Rock, Arkansas (Bill And Hillary Clinton Inter airport). It was a business flight under general aviation rules (Part 91). 5 people were killed. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The loss of control during initial climb for undetermined reasons. Contributing to the accident were the sudden wind shifts during the initial climb.

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

What the record shows

Date
February 22, 2023 · about 5:56 pm local time
Place
Little Rock, Arkansas · Bill And Hillary Clinton Inter · map
Type
Accident
Injuries
5 people were killed.
Weather
visual conditions (good weather)
Aircraft
Beech B200, built 1983 · all B200s on the register
Registration
N55PC · registry record · serial BB-1170
Damage
Destroyed
Flight
Business flight · general aviation rules (Part 91)

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

The pilot and four passengers were departing in the multi-engine turbopropeller-powered airplane when the accident occurred. Surveillance video indicated that the takeoff and initial climb appeared normal, however, the airplane than began to lose airspeed and altitude until the airplane entered a left roll and descended toward the ground. Just after the airplane went out of sight, the camera recorded a rising plume of smoke about 1 mile from of the departure end of the runway. Shortly after the plume of smoke appeared, the camera appeared to shake from wind, and recorded blowing debris and heavy rain on the ramp where the camera was located. Just before and during takeoff, the camera showed that the ramp was dry with no rain or noticeable wind. No radio or distress calls were heard from the pilot. Several witnesses saw the airplane’s takeoff and initial climb and they described the airplane as struggling to climb and reported that it entered a steep bank and descent toward the ground shortly after takeoff. The witnesses characterized the weather conditions as stormy and windy, with a weather front passing through the area. The wreckage of the airplane was found amidst heavily wooded terrain adjacent to a factory about 1 mile south of the departure end of runway 18 and a post-impact fire consumed most of the airplane. Detailed examinations of the airframe, engines, flight controls, and propellers did not reveal any pre-impact mechanical anomalies that would have precluded normal operations. Both engines and propellers exhibited evidence of rotation at the time of impact, and several large diameter tree branches at the accident site were found cut consistent with propeller blade strikes, also indicating that the engines were producing power at the time of impact. A performance study indicated that the airplane climbed to a maximum altitude of about 386 ft above ground level before it began to descend. Review of airplane performance from previous takeoffs from the same runway indicated that the airplane’s climb performance during the accident initial climb takeoff was diminished. The reason for the diminished performance could not be determined. Review of weather information indicated that the airplane departed about the time a line of extreme intensity precipitation was approaching, and weather reporting equipment at the airport indicated a wind shift associated with this oncoming line of precipitation. A wind shear alert was active in the control tower advising of 15 to 20 kt gains about 1 mile from the runway. Based on the observation weather data, it is likely that, during the initial climb, the airplane encountered wind with magnitudes between 20 and 30 kts that likely varied in direction about 50°, from a quartering headwind to a crosswind condition. In the minutes following the accident time, this wind continued to shift to a quartering tailwind condition for the departure runway and increased in magnitude to 30 to 40 kts. There was no evidence to suggest that the airplane encountered a microburst or downdraft. Based on available information, the performance study could not conclude why the airplane had diminished performance during the initial climb after takeoff. Although there was diminished performance during the initial climb, it could not be attributed to a airframe, engine, or system anomaly. Although the weather was deteriorating at the time of the accident, and there were wind shifts in the area, a weather study determined that the wind shifts likely contributed to, but did not cause the accident. The pilot’s autopsy was limited by injury but identified severe coronary artery disease. Within the limits of the autopsy, there was no evidence that a medical event contributed to the accident. The pilot’s toxicology testing detected a low level of ethanol in cavity blood only; however, the small amount of ethanol may have been produced postmortem. It is unlikely that the effects of ethanol contributed to the accident.

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. Windshear or thunderstorm during initial climb
  2. Unknown or undetermined during initial climb
  3. Loss of control in flight during initial climb defining event
  4. Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent

The NTSB's findings

  • Aircraft › Aircraft oper/perf/capability › Performance/control parameters › (general) › Unknown/Not determined
  • Environmental issues › Conditions/weather/phenomena › Wind › Sudden wind shift › Contributed to outcome

Pilot

  • Certificate: flight instructor, commercial pilot
  • Ratings: multi-engine land; single-engine sea; instructor: airplane multi-engine; instructor: airplane single-engine; instructor: instrument airplane; instrument: airplane
  • Flight time: 10,196 hours in all; 195 in this make and model; 40 in the last 90 days; 10 in the last 30 days
  • Last flight review: July 18, 2022
  • Medical certificate: Class 1 (with waivers/limitations)
  • Seat: left
  • Injury: fatal

The aircraft

  • Airframe total time: 10,784 hours
  • Last inspection: 100-hour inspection, July 22, 2022
  • Seats: 7
  • Landing gear: retractable
  • Engine 1: P&W PT6A-42 (Righ (turboprop); 10,607 hours total
  • Engine 2: P&W PT6A-42 (Left (turboprop); 10,498 hours total
  • Fire on the ground

The flight

  • Departed from: LIT Little Rock AR at 5:55 pm
  • Destination: CMH Columbus OH
  • Flight plan: IFR

Weather at the time

  • Light: daylight
  • Wind: from 300° at 22 knots, gusting 40
  • Visibility: 2 statute miles
  • Sky: overcast at 4,700 ft; scat at 3,600 ft
  • Temperature: 66°F (19°C), dew point 55°F (13°C)
  • Altimeter: 29.68 inHg
  • Observation at 12:02 pm from KLIT, 1 miles away

Weather report (METAR): KLIT 221802Z 30022G40KT 2SM -RA SCT036 OVC047 19/13 A2968 RMK AO2 PK WND 30040/1759 WSHFT 1748 RAB00 PRESRR P0000 T01890128

Injuries

FatalSeriousMinorNone
Flight crew1
Passengers4

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

33 documents, released by the NTSB on February 13, 2025. 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.

#DocumentWhat it is
1 NTSB Form 6120 Pilot Operator Report CEN23FA113 PDF, 11 pages · our copy View Download
2 Weather radar Image CEN23FA113 PDF, 1 page · our copy View Download
3 ADS-B Data Table CEN23FA113 data file · our copy Download
4 ADS-B Data Plot 1 CEN23FA113 PDF, 1 page · our copy View Download
5 ADS-B Data Plot 2 CEN23FA113 PDF, 1 page · our copy View Download
6 ADS-B Data Plot 3 CEN23FA113 PDF, 1 page · our copy View Download
7 Memorandum for the Record Site and Wreckage Examination CEN23FA113 PDF, 3 pages · our copy View Download
8 Memorandum for the Record Engine Examinations CEN23FA113 PDF, 4 pages · our copy View Download
9 Memorandum for the Record Propeller Examinations CEN23FA113 PDF, 5 pages · our copy View Download
10 Overhead Accident Area Diagram CEN23FA113 PDF, 1 page · our copy View Download
11 Overhead Image and Diagram of Accident Site CEN23FA113 PDF, 1 page · our copy View Download
12 Investigation Photographs CEN23FA113 PDF, 8 pages · our copy View Download
13 Signature Aero Ramp Security Video CEN23FA113 video View Download
14 I-440 Dashcam Video CEN23FA113 MOV file · our copy Download
15 3M Factory Security Camera Video CEN23FA113 video · our copy View Download
16 Witness Statements CEN23FA113 PDF, 4 pages · our copy View Download
17 Phenom 300 Pilot Statement CEN23FA113 PDF, 1 page · our copy View Download
18 Aircraft Performance Study PDF, 31 pages · our copy View Download
19 FAA ADS-B Data 2023-02-22 data file · our copy Download
20 FAA ADS-B Data 2023-02-15 data file · our copy Download
21 FAA ADS-B Data 2023-02-19 data file · our copy Download
22 Meteorology Specialist's Factual Report PDF, 25 pages · our copy View Download
23 Attachment 1 to the Meteorology Specialist's Factual Report PDF, 10 pages · our copy View Download
24 Attachment 2 to the Meteorology Specialist's Factual Report PDF, 368 pages · our copy View Download
25 Attachment 3 to the Meteorology Specialist's Factual Report PDF, 85 pages · our copy View Download
26 Maintenance Logbook Summary and Excerpts CEN23FA113 PDF, 32 pages View Download
27 Fuel Documents N55PC CEN23FA113 PDF, 4 pages · our copy View Download
28 NTSB ATC Voice Transcription Report CEN23FA113 PDF, 3 pages · our copy View Download
29 Pilot Toxicology Report CEN23FA113 PDF, 1 page · our copy View Download
30 Medical Factual Memorandum for Record PDF, 3 pages · our copy View Download
31 Certificate of Party Representative Hartzell CEN23FA113 PDF, 1 page · our copy View Download
32 Certificate of Party Representative Textron CEN23FA113 PDF, 1 page · our copy View Download
33 NTSB Release of Wreckage CEN23FA113 PDF, 2 pages · our copy View Download

The same 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.