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Accidents · NTSB ERA22FA320 · Final report

Amateur-built AA Nieuport 28 accident near Basehor, Kansas, July 18, 2022

On July 18, 2022 at about 3:00 pm local time, a 2016 amateur-built AA Nieuport 28, registered N6170, was destroyed in an accident during takeoff near Basehor, Kansas (Hoelting 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 incorrect installation of the left-wing strut, which resulted in a loss of airplane control during takeoff and a subsequent aerodynamic stall and spin from which the pilot could not recover.

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

What the record shows

Date
July 18, 2022 · about 3:00 pm local time
Place
Basehor, Kansas · Hoelting · map
Type
Accident
Injuries
1 person was killed.
Weather
visual conditions (good weather)
Aircraft
Amateur-built AA Nieuport 28, built 2016
Registration
N6170 · registry record · serial 001
Damage
Destroyed
Flight
Personal flight · general aviation rules (Part 91)

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

On the day of the accident, the pilot intended to fly the airplane for the first time since it had been repaired following a previous hard landing. The pilot, who was the builder of the experimental biplane, was taking off on a personal flight when the airplane veered to the left, lifted off the runway, and flew back toward the runway centerline. A witness noted that the airplane was going “very slow.” When the airplane reached an altitude of about 200 ft above ground level, the airplane started to make a slow left turn. The witness then observed the tail of the airplane drop down and the left wing roll, and the airplane subsequently spun to the ground. A postcrash fire ensued. About 2 years before the accident, the airplane was involved in a hard landing, which damaged the landing gear. The pilot subsequently repaired the landing gear, which would have included removal and reassembly of the wing struts. Postaccident examination of the airplane found that the left outer interplane strut was not correctly attached to the lower left wing compression strut. The bolt and nut were present through the outer interplane strut but had not been secured to the lower wing compression strut. The disconnected strut would have resulted in an out-of-rig condition and change the flight characteristics of the upper and lower left wings, potentially inducing drag while in flight. In this case, the upper and lower left wings would have each displayed different flight characteristics because the lower wing angle was pushed down and the upper wing was pushed up during the wire-tensioning process. The faster the airplane flew in the out-of-rig condition, the more pronounced the changed flight characteristics of the upper and lower left wings would have become. During the accident sequence, the pilot likely tried to slow the airplane to improve the changed flight characteristics, but the airplane’s critical angle of attack was exceeded and resulted in the airplane’s subsequent stall and spin to the ground.

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. Aerodynamic stall/spin during initial climb
  2. Loss of control in flight during takeoff defining event
  3. Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent
  4. Aircraft maintenance event during prior to flight

The NTSB's findings

  • Aircraft › Aircraft structures › Wing structure › Attach fittings (on wing) › Incorrect service/maintenance
  • Personnel issues › Task performance › Maintenance › Repair › Owner/builder

Pilot

  • Certificate: airline transport pilot
  • Ratings: multi-engine land; single-engine land; instructor: airplane multi-engine; instructor: airplane single-engine; instrument: airplane
  • Flight time: 9,525 hours in all; 999,999 in this make and model
  • Medical certificate: Class 3 (with waivers/limitations)
  • Seat: frt
  • Injury: fatal

The aircraft

  • Last inspection: inspection type not recorded
  • Maximum gross weight: 1,200 lb
  • Seats: 1
  • Landing gear: fixed
  • Engine: Lycoming 0-320 (piston); 0 hours total
  • Fire on the ground

The flight

  • Flight plan: none
  • Runway 18, 2,200 ft by 50 ft

Weather at the time

  • Light: daylight
  • Visibility: 10 statute miles
  • Sky: a few clouds at 4,000 ft
  • Temperature: 82°F (28°C), dew point 70°F (21°C)
  • Altimeter: 30.00 inHg
  • Observation at 9:53 am from KMCI, 15 miles away

Weather report (METAR): KMCI 181453Z 00000KT 10SM FEW040 28/21 A3000 RMK AO2 SLP147 T02780211 50002

Injuries

FatalSeriousMinorNone
Flight crew1

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

7 documents, released by the NTSB on January 30, 2024. 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 Memorandum for Record A�� Witness Interview Summary PDF, 1 page · our copy View Download
2 Wreckage Examination Summary - Kit Manufacturer PDF, 1 page · our copy View Download
3 Maintenance Records PDF, 1 page · our copy View Download
4 Investigative Photos PDF, 6 pages · our copy View Download
5 Wreckage Examination Summary PDF, 4 pages · our copy View Download
6 Toxicological Report PDF, 1 page · our copy View Download
7 Statement of Party Representatives to NTSB Investigation PDF, 2 pages · 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.