NTSB Prelim: Trom Wayne Vans RV6A | 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

Tue, Oct 04, 2022

NTSB Prelim: Trom Wayne Vans RV6A

No Evidence The Pilot Declared An Emergency Or Made Any Radio Calls Prior To The Accident

Location: Aztec, AZ Accident Number: WPR22FA348
Date & Time: September 16, 2022, 13:30 Local Registration: N646RV
Aircraft: Trom Wayne Vans RV6A Injuries: 2 Fatal
Flight Conducted Under: Part 91: General aviation - Personal

On September 16, 2022, about 1330 mountain standard time (MST), a Vans RV-6A experimental airplane, N646RV, was destroyed when it crashed near Aztec, Arizona. The pilot and passenger were fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

According to family members, the pilot and passenger were conducting a cross-country flight from San Diego, California, to Nogales, Arizona. Automatic Dependent Surveillance – Broadcast (ADS-B) data indicated the flight departed Brown Field Municipal Airport (SDM) at 1209. The flight flew easterly, parallel to Interstate 8 (I-8), and maintained an altitude of about 7,300 ft mean sea level (msl) and 125 knots until it neared Aztec, Arizona. At 1331:19 airspeed and altitude began decreasing. The pilot subsequently maneuvered away from I-8 for about one mile and then turned east and south-east before the ADS-B data ended in the vicinity of the accident location at 1334:28 (figure 1). The airplane impacted desert terrain about one mile north of I-8 and was destroyed by postimpact fire. There was no evidence the pilot declared an emergency or made any radio calls prior to the accident.

The wreckage was examined on site. Portions of the wood propeller remained attached to the crankshaft flange. The Fractured propeller blade remnants showed little rotational deformation. Impact marks were identified on the engine starter housing. The marks matched the starter ring teeth and showed little or no rotational movement.

The engine was retained for further examination.

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