Beech 35-C33 accident near Pulaski, Tennessee, December 7, 2023
On December 7, 2023 at about 5:03 pm local time, a 1965 Beech 35-C33, registered N5891J, was destroyed in an accident during enroute (cruise) near Pulaski, Tennessee. It was a personal flight under general aviation rules (Part 91). 2 people were killed. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The pilot’s failure to maintain airplane control, which resulted in pilot-induced oscillations and a subsequent loss of control 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
- December 7, 2023 · about 5:03 pm local time
- Place
- Pulaski, Tennessee · map
- Type
- Accident
- Injuries
- 2 people were killed.
- Weather
- visual conditions (good weather)
- Aircraft
- Beech 35-C33, built 1965 · all 35-C33s on the register
- Registration
- N5891J · registry record · serial CD-919
- Damage
- Destroyed
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
After departure on a 430-nautical mile (nm) cross-country flight, initial controller-pilot communications and headings were unremarkable. However, as the airplane climbed through 6,500 ft mean sea level (msl) and became established enroute, a performance study of ADS-B data showed that the airplane’s altitude and airspeed began to vary as the airplane repeatedly descended and climbed with fluctuating airspeeds. These oscillations became increasingly more severe over about 25 minutes, with altitude deviations up to 1,500 ft and significant fluctuations in airspeed. An air traffic controller advised the pilot that the airplane was left of course; although the pilot acknowledged the controller, the deviations continued to worsen and the pilot stopped responding to radio calls. Faint emergency transmissions were later received from the pilot and passenger as the airplane continued to descend. During the final portion of the flight, the airplane exceeded a descent rate of 10,000 ft per minute with a groundspeed of about 228 knots before terrain impact. The increasing altitude and heading deviations, loss of communication, and rapid uncontrolled descent were consistent with a loss of airplane control. Flight instructors who had flown with the pilot before the accident indicated that she routinely demonstrated poor manual aircraft handling and struggled with cockpit automation, including autopilot and trim use. The pilot’s training history showed that she had demonstrated difficulty maintaining situational awareness, suggesting the high-performance airplane she had purchased about 1.5 years before the accident was beyond her level of pilot proficiency, something explicitly noted by one of the instructors who had flown with her. Postaccident examination of the airplane wreckage did not reveal evidence of any anomalies or mechanical irregularities that would have precluded normal operation, though the degree of fragmentation and fire damage precluded a complete evaluation of the airplane’s flight controls and autopilot system. Given the airplane’s heading was stable during the initial portion of the flight, it is likely that the pilot had been using the autopilot. Based on the pilot’s reported misunderstanding of that system, including, but not limited to the autopilot’s pitch inputs and the requirement for manual pitch trim application, it is possible that the pilot inadvertently mis-trimmed the airplane, which resulted in oscillations that were exacerbated by the pilot’s application of force on the control yoke. These kinds of pilot-induced oscillations can occur when manual yoke or pitch trim inputs are in conflict with the autopilot's pitch control inputs, leading to delayed, or out-of-sync, corrections, rather than a smooth, constant altitude hold. The airplane’s vertical profile as evidenced by the ADS-B data, was consistent with these kinds of pilot-induced oscillations. As the oscillations became stronger, the pilot may have ultimately been unable to control the airplane’s pitch, even with the autopilot disengaged, resulting in the loss of airplane control. Toxicology results indicated that the pilot had used a combination of medications that may be used to treat conditions such as anxiety and depression, which may have performance-impairing effects. However, no details about any associated underlying conditions were available from reviewed records. Additionally, the medications trazodone, alprazolam, and buspirone may cause psychomotor and cognitive impairment such as slowed reaction time, diminished situational awareness, and sedation. However, due to the extent of the pilot’s injuries, measurement of drug levels was limited to tissue specimens only, preventing reliable comparison to antemortem reference ranges in blood. Overall, the pilot may have been experiencing impairing effects of medication use or an associated underlying condition at the time of the accident, and such effects may have diminished her ability to render effective control inputs. However, available medical and circumstantial evidence was insufficient to establish whether such effects contributed to the accident, particularly given the pilot’s demonstrated baseline proficiency in the high-performance airplane.
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
- Loss of control in flight during enroute (cruise) defining event
- Collision with terrain or object (not controlled flight into terrain) during enroute (descent)
The NTSB's findings
- Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Pitch control › Not attained/maintained
- Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
Pilot
- Certificate: private
- Ratings: single-engine land
- Flight time: 390 hours in all; 200 in this make and model
- Medical certificate: Class 3 (with waivers/limitations)
- Seat: left
- Injury: fatal
Passenger
- Seat: rgt
- Injury: fatal
The aircraft
- Airframe total time: 3,449 hours
- Last inspection: annual inspection, May 11, 2023
- Maximum gross weight: 3,050 lb
- Seats: 4
- Landing gear: retractable
- Engine: Continental IO-470-N (piston); 0 hours total
- Fire on the ground
The flight
- Departed from: DKX Knoxville TN at 2:48 pm
- Destination: SUZ Benton AR
- Flight plan: none
Weather at the time
- Light: daylight
- Wind: from 190° at 9 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 54°F (12°C), dew point 32°F (0°C)
- Altimeter: 30.19 inHg
- Observation at 11:15 am from LUG, 16 miles away
Weather report (METAR): KLUG 071715Z AUTO 19009KT 10SM CLR 12/M00 A3019 RMK A01
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 | |||
| Passengers | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
20 documents, released by the NTSB on February 19, 2026. 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.
Other NTSB records under N5891J the same tail number, which may have belonged to a different aircraft at the time
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.
