NTSB Prelim: John M Corneal Sub-Sonex | Aero-News Network
Aero-News Network
RSS icon RSS feed
podcast icon MP3 podcast
Subscribe Aero-News e-mail Newsletter Subscribe

Airborne Unlimited -- Most Recent Daily Episodes

Episode Date

Airborne-Monday

Airborne-Tuesday

Airborne-Wednesday Airborne-Thursday

Airborne-Friday

Airborne On YouTube

Airborne-Unlimited-12.08.25

AirborneNextGen-
12.02.25

Airborne-Unlimited-12.03.25

Airborne-FltTraining-12.04.25

AirborneUnlimited-12.05.25

AFE 2025 LIVE MOSAIC Town Hall (Archived): www.airborne-live.net

Thu, Jun 17, 2021

NTSB Prelim: John M Corneal Sub-Sonex

One Witness Saw The Airplane Flying Inverted

Location: Shreveport, LA Accident Number: CEN21FA230
Date & Time: May 23, 2021, 14:47 Local Registration: N465JC
Aircraft: John M Corneal Sub-Sonex Injuries: 1 Fatal
Flight Conducted Under: Part 91: General aviation - Personal

On May 23, 2021 about 1447 central daylight time (CDT), a Sub-Sonex JSX-2 experimental amateur built jet airplane, N465JC, was destroyed when it impacted a small recreational lake (Cross Lake) near Shreveport, Louisiana. The pilot sustained fatal injuries. The personal flight was being conducted under the provisions of Title 14 Federal Code of Regulations Part 91.

The intent of the flight was to fly over Cross Lake after departing Shreveport Regional Airport (SHV). Automatic Dependent Surveillance Broadcast (ADS-B) track data indicated the airplane departed runway (RWY) 24 at SHV, about 1439:00. The airplane made a right turn to the northeast and proceeded to fly over Cross Lake. The ADS-B track data showed the airplane maneuvering low-level over the lake until track data was lost at about 1446:14.

The last track data showed the airplane at 625 ft MSL, 142 knots ground speed, heading 100 degrees over Cross Lake. Several witnesses described the airplane’s low-level flight over the lake, and their observations were consistent with the ADS-B data. One witness saw the airplane flying inverted. He saw the airplane nose down and impact the water in a near vertical attitude. There were no radio or distress calls heard from the pilot.

Examination of the wreckage did not show any pre-impact anomalies with the flight controls or control surfaces. A ballistic recovery system (BRS) was installed. The BRS cockpit deployment lever was found in the stowed position. The airplane was equipped with a Garmin GX3, and the unit was retained for download. The engine had a full authority digital engine control (FADEC) installed. The FADEC unit was retained for download.

FMI: www.ntsb.gov

Advertisement

More News

NTSB Final Report: Patriot Aircraft LLC CX1900A

After Draining Both Wing Fuel Tanks, A Significant Amount Of Water Was Observed In The Right Wing Fuel Tank Analysis: The pilot, who was also the owner of the experimental amateur->[...]

Aero-News: Quote of the Day (12.06.25)

“Airbus apologises for any challenges and delays caused to passengers and airlines by this event. The Company thanks its customers, the authorities, its employees and all rel>[...]

ANN's Daily Aero-Term (12.06.25): High Speed Taxiway

High Speed Taxiway A long radius taxiway designed and provided with lighting or marking to define the path of aircraft, traveling at high speed (up to 60 knots), from the runway ce>[...]

ANN's Daily Aero-Linx (12.06.25)

Aero Linx: Taylorcraft Foundation, Inc. The Taylorcraft Foundation is exclusively organized for charitable, educational & scientific activities and will preserve the history an>[...]

Airborne-NextGen 12.02.25: Honda eVTOL, Arctus High-Alt UAS, Samson Patent

Also: USAF Reaper Accident, Baikonur Damage, Horizon eVTOL IFR/FIKI, New Glenn Update Honda has outlined its clearest timeline yet for its entry into the world of electric vertical>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

© 2007 - 2025 Web Development & Design by Pauli Systems, LC