NTSB Prelim: Jackson Dennis RV-8 | 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-04.22.24

Airborne-Unlimited-04.16.24

Airborne-FlightTraining-04.17.24 Airborne-AffordableFlyers-04.18.24

Airborne-Unlimited-04.19.24

Join Us At 0900ET, Friday, 4/10, for the LIVE Morning Brief.
Watch It LIVE at
www.airborne-live.net

Wed, Aug 31, 2022

NTSB Prelim: Jackson Dennis RV-8

Relatives... Told Investigators The Pilot Would Often Conduct Low Altitude Flights And Perform Aerobatic Maneuvers Over The Relatives’ Home

Location: Scio, OR Accident Number: WPR22FA312
Date & Time: August 21, 2022, 14:03 Local Registration: N184DJ
Aircraft: Jackson Dennis RV-8 Injuries: 2 Fatal
Flight Conducted Under: Part 91: General aviation - Personal

On August 21, 2022, at 1403 Pacific daylight time, an experimental homebuilt Vans RV-8 airplane, N184DJ, was substantially damaged when it was involved in an accident near Scio, Oregon. The pilot and passenger were fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

Witnesses, including relatives of the pilot, told investigators the pilot would often conduct low altitude flights and perform aerobatic maneuvers over the relatives’ home. The relatives stated the pilot conducted three passes over their home prior to the accident and the airplane was mostly wings level during the first two passes. During the third pass the airplane flew over about 100 ft above the ground from north to south. The airplane then rolled like a barrel roll and  then descended out of sight behind trees and impacted the ground. One family member stated she thought the pilot started the maneuver lower than normal. The second family member said that something did not look right at the start of the maneuver, that the airplane was too low and that the maneuver was “really snappy looking,” not smooth like he had seen before. He also said the airplane was not wings level as it exited the maneuver. Both family members described hearing the engine running steady and did not hear anything abnormal before the accident.

Two other witnesses were outside their home about .4 miles west of the accident site and stated that on one of the passes before the accident the airplane flew over their home from west to east. During the pass one witness thought he heard the airplane wheels hit the tops of the trees near his home. The airplane then descended to about 5 feet above the ground and then pulled up steeply as it approached a hedge row before making the accident pass. One of the witnesses videoed the final portion of the accident pass. In the video, the airplane can be seen in a nose up attitude through distant trees, then descending towards the ground at about a 45° nose low attitude. The airplane engine can be heard running before the sound of impact is heard.

The airplane impacted in a grass field about .2 miles south of the relative’s home. The initial impact signatures were indicative of the airplane impacting in a nose low and right-wing low attitude. The right flap was separated from the wing and located about 50 ft from the initial impact point. The canopy was separated from the fuselage and was located about 150 ft from the initial impact point. The main wreckage was inverted and located about 250 ft and bearing 200° from the initial impact point. The right wing was mostly separated from the fuselage and was resting under the fuselage.

Both ailerons, elevators, and the rudder were accounted for and remained attached to the airplane. Flight control continuity was verified to all flight control surfaces from the cockpit and continuity was continuous for all flight controls except the right aileron. The right aileron control tube was fractured near the wing root consistent with impact damage. The propeller assembly had separated from the engine at the shaft and was located near the main wreckage. Both propeller blades exhibited leading edge gouges, chordwise scratches, and significant S-type bending and curling.

FMI: www.ntsb.gov

Advertisement

More News

ANN's Daily Aero-Term (04.26.24): DETRESFA (Distress Phrase)

DETRESFA (Distress Phrase) The code word used to designate an emergency phase wherein there is reasonable certainty that an aircraft and its occupants are threatened by grave and i>[...]

ANN's Daily Aero-Linx (04.26.24)

Aero Linx: The International Association of Missionary Aviation (IAMA) The International Association of Missionary Aviation (IAMA) is comprised of Mission organizations, flight sch>[...]

Airborne 04.22.24: Rotor X Worsens, Airport Fees 4 FNB?, USMC Drone Pilot

Also: EP Systems' Battery, Boeing SAF, Repeat TBM 960 Order, Japan Coast Guard H225 Buy Despite nearly 100 complaints totaling millions of dollars of potential fraud, combined with>[...]

Airborne 04.24.24: INTEGRAL E, Elixir USA, M700 RVSM

Also: Viasat-uAvionix, UL94 Fuel Investigation, AF Materiel Command, NTSB Safety Alert Norges Luftsportforbund chose Aura Aero's little 2-seater in electric trim for their next gli>[...]

Airborne-NextGen 04.23.24: UAVOS UVH 170, magni650 Engine, World eVTOL Directory

Also: Moya Delivery Drone, USMC Drone Pilot, Inversion RAY Reentry Vehicle, RapidFlight UAVOS has recently achieved a significant milestone in public safety and emergency services >[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

© 2007 - 2024 Web Development & Design by Pauli Systems, LC