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Accidents · NTSB WPR24FA182 · Final report

Vans Aircraft INC RV-12 accident near Auburn, Washington, June 6, 2024

On June 6, 2024 at about 7:00 pm local time, a 2021 Vans Aircraft INC RV-12, an amateur-built aircraft,, registered N412JN, was substantially damaged in an accident during approach (VFR pattern downwind) near Auburn, Washington (Auburn Municipal airport). It was a personal flight 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 improper installation of the control stick pushrod assemblies, which resulted in separation of the left pushrod and a total loss of roll control during flight. Contributing to the accident was the failure to detect the installation error during the airplane’s construction, inspection, and subsequent maintenance.

Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.

What the record shows

Date
June 6, 2024 · about 7:00 pm local time
Place
Auburn, Washington · Auburn Municipal · map
Type
Accident
Injuries
1 person was killed.
Weather
visual conditions (good weather)
Aircraft
Vans Aircraft INC RV-12, built 2021, amateur-built
Registration
N412JN · registry record · serial 120577
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

The NTSB's narrative final · quoted from the NTSB record

While returning to the airport from a routine pleasure flight, the pilot of the experimental light-sport airplane reported a total flight control failure while maneuvering to land. Data from the onboard electronic flight instrument system and witness statements indicated that after turning from the crosswind to the downwind leg, the airplane entered an uncontrolled descending left turn consistent with a spin or spiral, culminating in a collision with a warehouse roof about 0.75 mile from the runway threshold. Postaccident examination revealed that the left side (where the pilot was operating the airplane) control stick pushrod had become disconnected from the flaperon mixer bellcrank due to improper installation during construction. Both left and right pushrod rod-end eyebolt bearings had been installed in reverse orientation. The improper installation allowed the pushrod to gradually unscrew from its eyebolt, ultimately resulting in complete separation of the left pushrod. This condition rendered the primary roll control system on the pilot’s side ineffective. The aircraft was equipped with an autopilot system featuring a “Level” mode capable of providing roll control independent of the cockpit control sticks. Prompt activation of this feature—or use of the rudder to counteract the developing roll—would likely have allowed the pilot to retain some degree of control. Similarly, the pilot would have been able to fully control the airplane if he had reached to his right and used the other control stick. However, given the sudden onset and rapid progression of the event, it is unlikely the pilot had sufficient time or situational awareness to identify and employ these options before the airplane entered an unusual attitude and became uncontrollable. The pilot's autopsy identified heart disease, including severe coronary artery disease of a single coronary artery and mild thickening of the left cardiac ventricle. Although the pilot’s heart disease was associated with an increased risk of sudden impairment or incapacitation from a cardiac event, the circumstances of the accident were not consistent with a sudden medical event and it is unlikely that the pilot’s heart disease contributed to the accident. The improper assembly error was traced to the original construction of the airplane and was visible in build photographs taken in 2019. The oversight persisted through final inspection and three years of subsequent operation. The airplane kit manufacturer later issued a service bulletin addressing correct installation of the pushrods.

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

  1. Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent
  2. Loss of control in flight during approach (VFR pattern downwind)
  3. Flight control sys malf/fail during approach (VFR pattern downwind) defining event

The NTSB's findings

  • Aircraft › Aircraft systems › Flight control system › Aileron control system › Incorrect service/maintenance
  • Aircraft › Aircraft systems › Flight control system › Aileron control system › Failure
  • Personnel issues › Action/decision › Info processing/decision › Identification/recognition › Owner/builder
  • Personnel issues › Task performance › Maintenance › Installation › Owner/builder
  • Personnel issues › Task performance › Inspection › Scheduled/routine inspection › Pilot

Pilot

  • Certificate: private
  • Ratings: single-engine land; instructor: airplane single-engine; instrument: airplane
  • Flight time: 270.7 hours in all; 79.7 in this make and model
  • Last flight review: February 3, 2024
  • Medical certificate: BasicMed (with waivers/limitations)
  • Seat: left
  • Injury: fatal

The aircraft

  • Airframe total time: 97.2 hours
  • Last inspection: condition inspection, April 14, 2024; 3.4 hours since
  • Maximum gross weight: 1,320 lb
  • Seats: 2
  • Landing gear: fixed
  • Engine: Rotax 912 ULS2-01 (piston); 100 hours total

The flight

  • Departed from: S50 Auburn WA at 6:08 pm
  • Destination: S50 Auburn WA
  • Flight plan: none
  • Runway 35, 3,842 ft by 75 ft

Weather at the time

  • Light: daylight
  • Wind: from 020° at 7 knots
  • Visibility: 10 statute miles
  • Sky: broken clouds at 25,000 ft; clear
  • Temperature: 64°F (18°C), dew point 46°F (8°C)
  • Altimeter: 30.12 inHg
  • Observation at 11:53 am from KSEA, 9 miles away

Weather report (METAR): KSEA 061853Z 02007KT 10SM BKN250 18/08 A3012 RMK AO2 SLP206 T01830083

Injuries

FatalSeriousMinorNone
Flight crew1

Documents from the investigation the NTSB's docket: the evidence folder behind the report

13 documents, released by the NTSB on November 14, 2025. 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.

#DocumentWhat it is
1 Flight Control Examination Report PDF, 15 pages · our copy View Download
2 Dynon Skyview EFIS Data data file · our copy Download
3 S50 Ctaf - Courtesy Liveatc.net audio · our copy View Download
4 Security Video - Courtesy Skills Inc. MOV file · our copy Download
5 Witness Statements PDF, 2 pages · our copy View Download
6 Pilot Logbook Excerpts PDF, 15 pages · our copy View Download
7 Maintenance Logbook Excerpts PDF, 12 pages · our copy View Download
8 Medical Factual Memorandum for Record PDF, 2 pages · our copy View Download
9 Toxicological Report PDF, 1 page · our copy View Download
10 Vans Aircraft SB-00102 PDF, 4 pages · our copy View Download
11 Statement of Party Representatives to NTSB Investigation PDF, 1 page · our copy View Download
12 Evidence Control Forms PDF, 4 pages · our copy View Download
13 Release of Aircraft Wreckage, NTSB Form 6120.15 PDF, 1 page · our copy View Download

The same docket at the NTSB.

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.