Avia Stroitel AC-5M accident near North Plains, Oregon, July 5, 2023
On July 5, 2023 at about 6:30 pm local time, a 2000 Avia Stroitel AC-5M (glider), an amateur-built aircraft,, registered N40233, was substantially damaged in an accident during maneuvering near North Plains, Oregon (North Plains Glider Port airport). It was a personal flight under general aviation rules (Part 91). 1 person was seriously injured. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The pilot’s failure to maintain control of the motor glider, which resulted in an inflight overstress separation of the right wing during a high-speed, high-wing-load spiral dive recovery. Contributing to the accident was the inadequately manufactured wing structure.
Source: NTSB aviation accident database, copy made October 4, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- July 5, 2023 · about 6:30 pm local time
- Place
- North Plains, Oregon · North Plains Glider Port · map
- Type
- Accident
- Injuries
- 1 person was seriously injured.
- Weather
- visual conditions (good weather)
- Aircraft
- Avia Stroitel AC-5M, built 2000, amateur-built · all AC-5Ms on the register
- Registration
- N40233 · registry record · serial 004
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The pilot stated the airspeed may have been too slow when he initiated a 30° - 45° right turn during his first flight in the foreign-manufactured experimental motor glider. The glider immediately entered a clockwise, tight spiraling dive. After several revolutions, he was able to arrest the rotation, but the motor glider’s high airspeed produced significant vibrations. He applied gentle aft pressure on the control stick to regain control, but an inflight separation of the right wing ensued. The pilot released the canopy, egressed about 500 ft above ground level (agl), and deployed his parachute. The motor glider impacted the ground, and the pilot’s parachute landing resulted in serious injury. Postaccident examination of the motor glider’s wing structure revealed that the right wing’s main spar fractured due to overstress from upward bending loads. No evidence of fatigue was observed with the fracture. However, the wing spar was likely weaker than expected due to wrinkles in the composite fiber reinforcement layers in the upper and lower caps at the critical location where the spar intersected the reinforced closeout rib at the inboard section of the wing. Since the overstress fractures showed no evidence of damage before separation from a progressive failure mechanism or impact, the loads on the right wing during the accident flight were likely higher than any previously applied loads. However, the extent and angle of the wrinkles in the reinforcement layers at the fracture location indicated that the load that produced the right wing failure in this accident was considerably less than the expected failure load for the design and was possibly lower than the expected maximum design operating load. However, without knowing the actual ratio between the design ultimate failure load and the maximum design operating load of the wing for this experimental foreign-made aircraft, it is uncertain whether the design maximum operating load was exceeded based solely on analysis of the lab findings.
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
- Aircraft structural failure during maneuvering
- Loss of control in flight during maneuvering defining event
- Aircraft maintenance event during prior to flight
The NTSB's findings
- Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
- Aircraft › Aircraft structures › Wing structure › Spar (on wing) › Capability exceeded
- Personnel issues › Experience/knowledge › Knowledge › Knowledge of equipment › Pilot
- Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Airspeed › Not attained/maintained
- Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Lateral/bank control › Not attained/maintained
- Organizational issues › Development › Manufacture/production › (general) › Manufacturer
Pilot
- Certificate: private
- Ratings: single-engine land; rotorcraft: glider
- Flight time: 240 hours in all; 0 in this make and model; 21 in the last 90 days; 3 in the last 30 days; 206 as pilot in command
- Last flight review: May 16, 2023
- Medical certificate: Class 2 (without waivers/limitations)
- Seat: sngl
- Injury: serious injuries
The aircraft
- Airframe total time: 96.5 hours
- Last inspection: condition inspection, June 7, 2023; 4 hours since
- Maximum gross weight: 660 lb
- Seats: 1
- Landing gear: fixed
- Engine: Zanzolterra MZ34/5 (piston); 13 hours total
The flight
- Departed from: 1OR4 North Plains OR at 6:19 pm
- Flight plan: none
Weather at the time
- Light: daylight
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 84°F (29°C), dew point 50°F (10°C)
- Altimeter: 29.90 inHg
- Observation at 10:53 am from KHIO, 5 miles away
Weather report (METAR): KHIO 051753Z 00000KT 10SM CLR 29/10 A2990 RMK AO2 SLP121 T02890100 10294 20144 58002
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
9 documents, released by the NTSB on May 8, 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.
| # | Document | What it is | |
|---|---|---|---|
| 1 | Pilot/operator Aircraft Accident Report, NTSB Form 6120.1 | PDF, 24 pages | View Download |
| 2 | Record of Conversation -pic | PDF, 2 pages | View Download |
| 3 | Record of Conversation -faa | PDF, 2 pages | View Download |
| 4 | Pilot Logbook | PDF, 17 pages | View Download |
| 5 | Motor Glider Logbook | PDF, 14 pages | View Download |
| 6 | Flight Manual Excerpts | PDF, 2 pages | View Download |
| 7 | Photographs | PDF, 7 pages | View Download |
| 8 | Materials Laboratory Factual Report 24-081 | PDF, 22 pages | View Download |
| 9 | Release of Aircraft Wreckage | PDF, 2 pages | View Download |
The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.
About this page
Everything above comes from the NTSB's public accident database: the narrative, probable cause and findings are the NTSB's own words, and the coded tables behind its report (pilot, aircraft, flight, weather, injuries, sequence of events) are written out in plain English. Pilots' ages, home towns and medical details are left out on purpose. The documents and photographs are the NTSB's docket, the folder of records gathered during the investigation, shown as the NTSB released them (the NTSB redacts some personal details first) and listed under the NTSB's own titles. This site's own text never names pilots, passengers or anyone else involved. A preliminary report describes what is known soon after the event and can change; the final report, with the probable cause, usually follows one to two years later and this page is refreshed when it does. Case number WPR23LA255.
