Beech C23 accident near Lansing, West Virginia, September 26, 2021
On September 26, 2021 at about 2:09 pm local time, a 1977 Beech C23, registered N3342L, was substantially damaged in an accident during initial climb near Lansing, West Virginia (New River Gorge airport). It was a personal flight under general aviation rules (Part 91). 3 people were killed. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The pilot’s exceedance of the airplane’s critical angle of attack while maneuvering to avoid trees and terrain after takeoff, which resulted in an aerodynamic stall and loss of control. Also causal was the pilot’s decision to operate the airplane outside of its weight and balance limitations and his decision to continue the takeoff after two previous aborted takeoffs during which the airplane demonstrated reduced performance.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- September 26, 2021 · about 2:09 pm local time
- Place
- Lansing, West Virginia · New River Gorge · map
- Type
- Accident
- Injuries
- 3 people were killed.
- Weather
- visual conditions (good weather)
- Aircraft
- Beech C23, built 1977 · all C23s on the register
- Registration
- N3342L · no longer on the register · serial M-1902
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The pilot and two passengers were departing on the return flight following a weekend of camping. Three witnesses watched as the pilot initiated a takeoff from runway 22 (2,950 ft long), then aborted the takeoff. The pilot continued to the end of the runway, turned the airplane around, and initiated a takeoff from runway 04, which he also aborted. The airplane continued to the departure end of runway 04, turned around, and began another takeoff from runway 22. One of the witnesses reported that, “…he was going too fast to stop at the end of the runway but not fast enough to take off.” The airplane lifted off “maybe” 800 ft before the departure end of the runway, cleared trees at the departure end, and flew over a creek which ran below and perpendicular to the runway. The terrain on the opposite bank was higher than the runway and included mature trees. The airplane banked steeply left and disappeared below the trees. A witness estimated the airplane’s bank angle as 45° and said that the engine sound was smooth and continuous from engine start until the sound of impact. Postaccident examination of the airplane revealed no evidence of mechanical malfunctions or anomalies that would have precluded normal operation. The airplane had a useful load of about 862 lbs. The airplane’s weight and balance at the time of the accident was calculated using the known weights of the pilot, passengers, and baggage (a total of about 797 lbs) and estimates of the airplane’s fuel state at the time of the accident based on its likely fuel consumption during the 2.5-hour flight to the accident airport. The amount of fuel onboard at the time of the accident could not be determined; however, the airplane’s weight at the time of the accident would have exceeded its maximum gross weight with a center of gravity aft of the aft limit, even with only about 1 hour of fuel onboard. Toxicology testing revealed that the pilot had used cannabis; low concentrations of THC and its inactive metabolite, THC-COOH, were detected in his blood. Peak effects from using cannabis typically occur in the first couple of hours and concentrations typically fall below 5 ng/mL after three hours. Since THC is stored in fatty tissues and slowly released days and weeks after using cannabis, low concentrations can be detected long after use, especially in more chronic users. While the pilot’s pattern of cannabis use is unknown, given the low concentration of THC in his blood and none in his liver, it is unlikely that the pilot was under the influence of THC. Thus, while the pilot was found to have cannabis in his body, it is unlikely that the effects of the pilot’s use of cannabis contributed to this accident. One laboratory detected ethanol in the pilot’s pleural blood at 0.026 gm/dL; the other lab did not detect ethanol in his cavity blood. One would expect similar concentrations in both blood samples. The pilot’s internal organs had many lacerations, which can increase microbial spread and microbial production of ethanol. A concentration of 0.026 is close to the concentration where some minor effects from ethanol use can be observed. Given the differing and low level of ethanol and the condition of the body, it is likely that the identified ethanol was from sources other than ingestion. Thus, the identified ethanol did not contribute to this accident. The pilot’s decision to operate the airplane outside of its weight and balance limitations likely resulted in degraded performance and handling characteristics, including a longer ground roll during the takeoff, reduced climb performance, and instability due to the aft center of gravity. Given the previous two aborted takeoffs, it is likely that the pilot recognized the airplane’s poor takeoff performance; however, he chose to both attempt and continue a third takeoff. After becoming airborne, it is likely that the pilot was maneuvering to avoid trees at the end of the runway when he exceeded the airplane’s critical angle of attack, resulting in an aerodynamic stall and loss of airplane control.
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
- Aerodynamic stall/spin during initial climb defining event
The NTSB's findings
- Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Angle of attack › Capability exceeded
- Aircraft › Aircraft oper/perf/capability › Aircraft capability › Maximum weight › Capability exceeded
- Aircraft › Aircraft oper/perf/capability › Aircraft capability › CG/weight distribution › Capability exceeded
- Personnel issues › Action/decision › Info processing/decision › Decision making/judgment › Pilot
- Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
Pilot
- Certificate: private
- Ratings: single-engine land; instrument: airplane
- Flight time: 395.7 hours in all; 312.1 in this make and model
- Medical certificate: Class 3 (without waivers/limitations)
- Seat: left
- Injury: fatal
The aircraft
- Airframe total time: 3,533 hours
- Last inspection: annual inspection, December 3, 2020; 135.6 hours since
- Maximum gross weight: 2,450 lb
- Seats: 4
- Landing gear: fixed
- Engine: Lycoming O-360-A4K (piston); 0 hours total
The flight
- Destination: CPK Chesapeake VA
- Flight plan: none
- Runway 04/2, 2,950 ft by 24 ft
Weather at the time
- Light: daylight
- Wind: from 240° at 5 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 59°F (15°C), dew point 46°F (8°C)
- Altimeter: 30.20 inHg
- Observation at 10:51 am from KBKW, 18 miles away
Weather report (METAR): KBKW 261451Z AUTO 24005KT 10SM CLR 15/08 A3020 RMK AO2 SLP218 T01500078 53014 TSNO
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 | |||
| Passengers | 2 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
12 documents, released by the NTSB on March 1, 2023. 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.
| # | Document | What it is | |
|---|---|---|---|
| 1 | Memorandum for Record - Airport Owner | PDF, 2 pages | View Download |
| 2 | Memorandum for Record - Witness Airport Founder | PDF, 1 page | View Download |
| 3 | Witness Statements | PDF, 1 page | View Download |
| 4 | Memorandum for Record A�� Friend/ Former Owner of Accident Airplane | PDF, 2 pages | View Download |
| 5 | Memorandum for Record A�� Pilot's Partner | PDF, 1 page | View Download |
| 6 | Maintenance Records - Airframe Excerpts | PDF, 2 pages | View Download |
| 7 | Maintenance Records - Engine Annual Inspection | PDF, 1 page | View Download |
| 8 | Electronic Device Email Report | PDF, 1 page | View Download |
| 9 | Investigative Photographs | PDF, 6 pages | View Download |
| 10 | Aircraft Incident/accident Technical Report - Textron | PDF, 12 pages | View Download |
| 11 | Statement of Party Representatives to NTSB Investigation | PDF, 15 pages | View Download |
| 12 | Release of Aircraft Wreckage, NTSB Form 6120.15 | PDF, 1 page | View Download |
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.
