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Accidents · NTSB CEN24FA095 · Final report

Cirrus Design CORP SR22 accident near Little Rock, Arkansas, January 21, 2024

On January 21, 2024 at about 7:20 pm local time, a 2008 Cirrus Design CORP SR22, registered N255JP, was destroyed in an accident during initial climb near Little Rock, Arkansas (Bill And Hillary Clinton Ntl/A airport). 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 failure to maintain airplane control after a partial loss of engine power during initial climb. Contributing to the accident was the pilot’s failure to follow airplane flight manual procedures and limitations for the turbocharged engine, which resulted in a loss of engine power due to cold weather effects on the turbocharger control system.

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

What the record shows

Date
January 21, 2024 · about 7:20 pm local time
Place
Little Rock, Arkansas · Bill And Hillary Clinton Ntl/A · map
Type
Accident
Injuries
1 person was killed.
Weather
visual conditions (good weather)
Aircraft
Cirrus Design CORP SR22, built 2008
Registration
N255JP · registry record · serial 3084
Damage
Destroyed
Flight
Personal flight · general aviation rules (Part 91)

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

The pilot planned on flying the airplane on a personal cross-country flight. The air temperature at the departure airport was about 28°F when the pilot attempted to start the airplane engine for the flight. There were an excessive number of engine start attempts by the pilot, which he attributed to the cold weather and flooding the engine. Once he started the engine, he immediately taxied the airplane without allowing the engine to warm up. Recorded data showed that an engine run-up was not performed as prescribed in the airplane’s before takeoff checklist. Recorded data also showed the engine oil reached its minimum temperature limit about 11 minutes after engine start, which was about 2 minutes before the start of takeoff. During the departure climb, the engine manifold pressure exceeded its maximum limitation, the fuel flow entered its caution range, and oil pressure was near its upper normal range limit, all of which were indicative of the viscous effects of cold oil, which induced an excessively rich mixture. The pilot then reported that the engine lost power, and recorded data showed that engine power and airspeed gradually decreased. The airplane then entered an aerodynamic stall, descended, and impacted an area next to the departure runway. Postaccident examination of the airplane did not reveal any anomalies that would have precluded normal operation. The engine had been modified through a supplemental type certificate (STC) with the installation of a turbocharging system. There was no change in engine oil temperature limits with the installation of the turbocharger but there were changes in fuel flow and oil pressure limits. The STC flight manual supplement stated that if manifold pressure exceeded normal limits, engine throttle should be reduced. The supplement further stated that engine parameters should read in the green during takeoff and noted that manifold pressure may temporarily increase with an associated increase in fuel flow due to cooler oil temperatures. The pilot completed training in the airplane about 10 days before the accident, during which he accumulated 10 hours of flight time. The pilot’s total experience flying airplanes powered by turbocharged engines was unable to be determined. The pilot’s postmortem toxicology results indicate that he had used the sedating antihistamine medication diphenhydramine. The level of diphenhydramine in postmortem heart blood was low. Based on this result, it is unclear whether the pilot was experiencing any impairing effects of his diphenhydramine use at the time of the accident or during earlier flight-related activities. The pilot’s high HbA1c indicates that he had uncontrolled diabetes, which was not identified at his last aviation medical examination. Additionally, the pilot had a history of high blood pressure that was associated with some increased cardiovascular risk, and his autopsy results indicate the presence of at least mild cardiovascular disease. However, neither the toxicological nor the autopsy evidence provide any clear, specific indication that the pilot was significantly impaired by his medical conditions.

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. Loss of control in flight during initial climb defining event
  2. Loss of engine power (partial) during initial climb

The NTSB's findings

  • Personnel issues › Action/decision › Action › Lack of action › Pilot
  • Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Powerplant parameters › Not attained/maintained
  • Environmental issues › Conditions/weather/phenomena › Temp/humidity/pressure › Low temperature › Effect on equipment
  • Personnel issues › Experience/knowledge › Knowledge › Knowledge of equipment › Other
  • Aircraft › Aircraft oper/perf/capability › Performance/control parameters › (general) › Not attained/maintained
  • Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot

Pilot

  • Certificate: airline transport pilot, commercial pilot
  • Ratings: multi-engine land; single-engine land; instrument: airplane
  • Flight time: 22,000 hours in all; 15.2 in this make and model; 100 in the last 90 days
  • Medical certificate: Class 2 (with waivers/limitations)
  • Seat: left
  • Injury: fatal

The aircraft

  • Airframe total time: 853.7 hours
  • Last inspection: annual inspection, May 9, 2023
  • Maximum gross weight: 3,400 lb
  • Seats: 4
  • Landing gear: fixed
  • Engine: Teledyne Continental Motors IO-550-N (piston); 854 hours total
  • Fire on the ground

The flight

  • Departed from: KLIT Little Rock AR at 7:15 pm
  • Destination: VDF Tampa FL
  • Flight plan: IFR
  • Runway 04L/, 8,273 ft by 150 ft

Weather at the time

  • Light: daylight
  • Wind: from 120° at 6 knots
  • Visibility: 10 statute miles
  • Sky: scat at 16,000 ft
  • Temperature: 28°F (-2°C), dew point 10°F (-12°C)
  • Altimeter: 30.56 inHg
  • Observation at 12:53 pm from LIT, 45 miles away

Weather report (METAR): KLIT 211853Z 12006KT 10SM SCT160 SCT250 M02/M12 A3056 RMK AO2 SLP353 T10171122 $

Injuries

FatalSeriousMinorNone
Flight crew1

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

19 documents, released by the NTSB on November 14, 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 Surveillance Video - Attempted Battery Starts video View Download
2 Surveillance Video - After Takeoff video · our copy View Download
3 Surveillance Video - Taxiway M View of Impact video · our copy View Download
4 Flight Instructor Statement PDF, 4 pages · our copy View Download
5 Witness Statement PDF, 1 page · our copy View Download
6 radar Data data file · our copy Download
7 Recorded Flight Data Specialist's Factual Report PDF, 13 pages · our copy View Download
8 Recorded Flight Data Specialist's Factual Report Attachment 1 data file · our copy Download
9 Recorded Flight Data Specialist's Factual Report Attachment 2 data file · our copy Download
10 On Scene Investigation Summary PDF, 7 pages · our copy View Download
11 Aircraft Examination Summary PDF, 9 pages · our copy View Download
12 Cirrus SR22 Flight Manual Limitations Excerpt PDF, 2 pages · our copy View Download
13 Cirrus SR22 Flight Manual Before Takeoff Checklist PDF, 2 pages · our copy View Download
14 Tornado Alley Flight Manual Supplement PDF, 44 pages · our copy View Download
15 Continental Service Bulletin M67-12 PDF, 1 page · our copy View Download
16 Maintenance Records PDF, 7 pages · our copy View Download
17 Pilot's Insurance Application PDF, 3 pages · our copy View Download
18 Reports from Federal Agencies - FAA Toxicology PDF, 2 pages · our copy View Download
19 Release of Aircraft Wreckage, NTSB Form 6120.15 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.