Amateur-built SMYTH SIDEWINDER accident near Boulder, Colorado, November 27, 2013
On November 27, 2013 at about 4:50 pm local time, a 1981 amateur-built SMYTH SIDEWINDER, registered N3786A, was destroyed in an accident during maneuvering near Boulder, Colorado. 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 abrupt maneuver, which exceeded the structural limits of the left wing and resulted in its in-flight separation.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- November 27, 2013 · about 4:50 pm local time
- Place
- Boulder, Colorado · map
- Type
- Accident
- Injuries
- 1 person was killed.
- Weather
- visual conditions (good weather)
- Aircraft
- Amateur-built SMYTH SIDEWINDER, built 1981
- Registration
- N3786A · no longer on the register · serial 212581
- Damage
- Destroyed
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
Radar data showed that, during the first 15 minutes of the cross-country flight, the experimental, amateur-built, airplane had a normal departure and climbout. However, the airplane then suddenly turned and rapidly descended. A witness reported that he heard a loud sound, looked up, and saw the airplane falling out of the sky. Another witness reported seeing flocks of migrating birds in the area about the time of the accident. No radio calls or distress transmissions were received from the pilot. The airplane's left wing was found about 1,156 ft from the main wreckage. Examination of the engine and flight controls did not reveal any mechanical anomalies that might have contributed to the accident. Examination of the left wing revealed no evidence of preexisting conditions that would have contributed to its separation. The wing's left lower spar cap was fractured about 8 inches outboard of the attachment point through the two rivet holes immediately outboard of the wing-to-fuselage fittings. There was no obvious deformation of the lower spar cap members in the fracture area. The upper spar cap members were fractured between 10 and 12 inches outboard of the attachment point with significant S-type bending of the members in the fracture area. The upper shear bolt remained intact and installed, but the lug portion of the fuselage fitting was fractured. The fracture faces on the upper and lower spar cap members all had a dull, angled, grainy appearance consistent with overstress separation. The lack of deformation of the lower spar cap members, the bending deformation of the upper spar cap members, and the appearance of the fracture faces on the individual members are consistent with a tension overload failure of the lower spar cap and compression overload failure of the upper spar cap. The evidence is consistent with the separation of the left wing due to a positive overload condition. Although flocks of migrating birds were seen in the area about the time of the accident, no evidence was found indicating that an in-flight bird strike occurred. However, it is likely that the pilot made an abrupt maneuver, possibly to avoid birds, which resulted in excessive g forces on the wing structure and led to its separation. An autopsy of the pilot did not reveal any medical conditions that might have contributed to the accident.
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
- Part(s) separation from AC during maneuvering defining event
The NTSB's findings
- cause Aircraft › Aircraft structures › Wing structure › Spar (on wing) › Failure
- cause Aircraft › Aircraft structures › Wing structure › Spar (on wing) › Capability exceeded
- cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › (general) › Not attained/maintained
- cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
Pilot
- Certificate: private
- Ratings: single-engine land
- Flight time: 1,977 hours in all; 900 in this make and model; 31 in the last 90 days
- Medical certificate: Class 3 (with waivers/limitations)
- Seat: sngl
- Injury: fatal
The aircraft
- Airframe total time: 1,909 hours
- Last inspection: continuous airworthiness programme, May 24, 2013
- Maximum gross weight: 1,600 lb
- Seats: 1
- Landing gear: fixed
- Engine: Lycoming O-320 (piston); 1,906 hours total
The flight
- Departed from: BJC Broomfield CO at 4:30 pm
- Destination: FNL Loveland CO
- Flight plan: none
Weather at the time
- Light: daylight
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 57°F (14°C), dew point 36°F (2°C)
- Altimeter: 30.04 inHg
- Observation at 3:59 pm from BDU, 25 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the 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.
