Beech BE-23 accident near Rolla, Missouri, December 18, 2000
On December 18, 2000, a Beech BE-23, registered N2324J, was destroyed in an accident near Rolla, Missouri. It was a business 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 inadequate preflight during the pre-buy inspection, the pilot's incapacitation due to carbon monoxide, and the fractured muffler.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- December 18, 2000
- Place
- Rolla, Missouri · map
- Type
- Accident
- Injuries
- 1 person was killed.
- Weather
- visual conditions (good weather)
- Aircraft
- Beech BE-23
- Registration
- N2324J · no longer on the register · serial M275
- Damage
- Destroyed
- Flight
- Business flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The pilot conducted a pre-buy inspection of the airplane that lasted approximately 30 minutes. The pilot departed SUS in the PA-23 at 1700. Two pilots in a Cessna 182 departed SUS 5-7 minutes later. Both airplanes had the same route of flight with Odessa, TX, as their destination airport. The Cessna 182 encountered no problems along the route of flight. Between 1800 and 1821, the PA-23's flight track became erratic in heading and altitude. The radar data indicated the airplane's altitude started descending from 8,500 feet msl at 1809 to an altitude of 2,000 feet msl recorded at 1821, which was the last radar return recorded. Between 1809 and 1821, the radar data indicated the airplane's flight path was a series of inconstant descending turns that took the airplane in an easterly direction. The last radar return was approximately .5 nautical mile from the accident site. The airplane impacted the ground in a steep nose down attitude. The leading edges of the left and right wings exhibited leading edge crush. Cable continuity was confirmed to the flight controls. The propeller blades exhibited "S" bending, leading edge gouges and chordwise scratching. Broken tree branches and limbs were found that exhibited prop slashes and gray paint transfer. A toxicology test was performed but a carbon monoxide test could not be performed due to an inadequate blood sample. The NTSB Materials Laboratory examined the muffler and heater muff assembly and reported that a microscopic examination of the muffler portion revealed the internal wall exhibited oxidation damage. The report stated, "Many areas of the muffler fracture showed oxidation damage that penetrated through the wall. The oxidation damage areas on the fracture appeared black, consistent with a pre-existing fracture that was exposed to the environment for an extended period of time." The report stated, "By visual estimate, the total combined length of the oxidation damage areas that penetrated through the wall was at least 20% of the circumference of the body of the muffler." The report stated, "The examination of the fractures from the heat exchanger collector tube showed evidence of minor tinting which is consistent with short-term (post crash) exposure to heat." It stated, "The outer layer of the tube had a decaburized layer, typical of steel exposed to high temperature and the environment for an extended period of time. The fracture surface of the heater muff exhibited no evidence of tinting."
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
Pilot
- Certificate: commercial pilot
- Ratings: multi-engine land; single-engine land; instructor: airplane multi-engine; instructor: airplane single-engine; instrument: airplane
- Flight time: 2,426 hours in all; 2,401 as pilot in command
- Medical certificate: Class 2 (valid medical--w/ waivers/lim.)
- Seat: left
The aircraft
- Airframe total time: 2,082 hours
- Last inspection: annual inspection, August 16, 2000; 6 hours since
- Maximum gross weight: 2,300 lb
- Seats: 4
- Landing gear: fixed
- Engine: Lycoming O-320-D2B (piston); 0 hours total
The flight
- Departed from: SUS Chesterfield MO at 11:00 pm
- Destination: Tulsa OK
- Flight plan: none
- Runway 0
Weather at the time
- Light: night, dark
- Wind: from 220° at 7 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 55°F (13°C), dew point 37°F (3°C)
- Altimeter: 30.00 inHg
- Observation at 11:53 pm from VIH, 12 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Crew | 1 |
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.
