Amateur-built BUGATTI-DEMONGE 100P accident near Burns Flat, Oklahoma, August 6, 2016
On August 6, 2016 at about 1:20 pm local time, a 2015 amateur-built BUGATTI-DEMONGE 100P, registered N110PX, was destroyed in an accident during takeoff near Burns Flat, Oklahoma (Clinton-Sherman airport). It was a flight test 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 airspeed following an engine anomaly during the initial climb after takeoff, which resulted in the airplane exceeding its critical angle of attack and experiencing an aerodynamic stall. Contributing to the accident was an engine anomaly, the reason for which could not be identified during postaccident examination.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- August 6, 2016 · about 1:20 pm local time
- Place
- Burns Flat, Oklahoma · Clinton-Sherman · map
- Type
- Accident
- Injuries
- 1 person was killed.
- Weather
- visual conditions (good weather)
- Aircraft
- Amateur-built BUGATTI-DEMONGE 100P, built 2015
- Registration
- N110PX · no longer on the register · serial 002
- Damage
- Destroyed
- Flight
- Flight test · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The airline transport pilot departed from a 13,500 ft long runway with a right quartering headwind present on a local test flight in an experimental, amateur-built, twin-engine airplane, which was a replica of a 1930s-era air racer. During the initial climb after takeoff , the airplane entered a right bank followed by a left bank. The left bank increased, and the airplane entered a nose-low descent that continued until it impacted terrain in an inverted attitude. The airplane was equipped with several onboard cameras that captured video footage of the accident flight. The video revealed that the left/forward engine began surging after liftoff and reached its maximum operating speed (red line) twice during the short flight. Although the pilot attempted to control the forward engine rpm with the throttle lever, the throttle inputs had no apparent effect. Based on the design of the propeller drive train, it is a possibility that the forward engine clutch was slipping. The airplane's airspeed decreased below its design stall speed and the angle of attack increased; the airplane then rolled left and subsequently impacted the ground. A postaccident examination of the airplane did not reveal any preimpact flight control anomalies. Examination of the engines did not identify a reason for the surging of the forward engine or slipping of the clutch. The sequence of events as described by witness statements and the onboard video was consistent with a loss of airspeed following an engine anomaly and a subsequent aerodynamic stall. Toxicological testing revealed alcohols were present in samples taken during the autopsy. Given the putrefaction of the samples, it is likely that all detected alcohols were the result of postmortem production. Terrain from the accident site to one quarter mile north of the accident site was suitable for an emergency landing there.
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
- Powerplant sys/comp malf/fail during takeoff
- Loss of control in flight during takeoff defining event
- Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent
The NTSB's findings
- cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Airspeed › Not attained/maintained
- cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
- factor Aircraft › Aircraft power plant › (general) › (general) › Malfunction
- factor Not determined › Not determined › (general) › (general) › Unknown/Not determined
Pilot
- Certificate: airline transport pilot
- Ratings: multi-engine land; single-engine land; instructor: airplane multi-engine; instructor: airplane single-engine; instructor: instrument airplane; instrument: airplane
- Flight time: 10,700 hours in all
- Medical certificate: Class 2 (with waivers/limitations)
- Seat: sngl
- Injury: fatal
The aircraft
- Maximum gross weight: 2,939 lb
- Seats: 1
- Landing gear: retractable
- Engine 1: Suzuki 1300 cc (piston); 0 hours total
- Engine 2: Suzuki 1300 cc (piston); 0 hours total
- Fire on the ground
The flight
- Departed from: CSM Burns Flat OK at 1:20 pm
- Destination: CSM Burns Flat OK
- Flight plan: none
- Runway 35L, 13,503 ft by 150 ft
Weather at the time
- Light: daylight
- Wind: from 040° at 9 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 73°F (23°C), dew point 70°F (21°C)
- Altimeter: 30.05 inHg
- Observation at 12:53 pm from KCSM, 1 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
10 documents, released by the NTSB on November 22, 2017. 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 | Witness Statements | PDF, 7 pages | View Download |
| 2 | Onboard Image Recorder - Group Chairman's Factual Report | PDF, 11 pages | View Download |
| 3 | Attachment 1 to Onboard Image Recorder Factual Report (Shelf Item) | PDF, 1 page | View Download |
| 4 | Attachment 2 to Onboard Image Recoder Factual Report | data file | Download |
| 5 | Airplane Performance Study | PDF, 9 pages | View Download |
| 6 | Maps or Charts of Accident Area | PDF, 2 pages | View Download |
| 7 | Toxicological Report - Cami 201600172001 | PDF, 1 page | View Download |
| 8 | Miscellaneous Information - Cami Information for Detected Drugs | PDF, 3 pages | View Download |
| 9 | Photos | PDF, 16 pages | View Download |
| 10 | 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.
