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Accidents · NTSB ANC22FA066 · Final report

Piper PA-12 accident near Arctic Village, Alaska, August 11, 2022

On August 11, 2022 at about 7:52 pm local time, a Piper PA-12, registered N3937M, was substantially damaged in an accident during initial climb near Arctic Village, Alaska. It was a personal flight under general aviation rules (Part 91). 1 person was killed. The weather was visual conditions (good weather).

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The NTSB's probable cause their words, unchanged

The pilot’s decision to depart in turbulent and gusting wind conditions, which resulted in a loss of control and impact with terrain.

Source: NTSB aviation accident database, copy made October 4, 2026. Docket and reports at the NTSB.

What the record shows

Date
August 11, 2022 · about 7:52 pm local time
Place
Arctic Village, Alaska · map
Type
Accident
Injuries
1 person was killed.
Weather
visual conditions (good weather)
Aircraft
Piper PA-12 · all PA-12s on the register
Registration
N3937M · registry record · serial 12-2825
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

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

The pilot was returning from a solo hunting trip when the accident occurred. There were no reported distress calls or radio communications from the pilot. The next day a pilot who was overflying the area spotted the airplane wreckage about 2 nautical miles (nm) west of a gravel airstrip. A review of the data from the accident pilot’s GPS revealed that the airplane departed the gravel strip to the south and then made a right turn into a mountain valley. The flight track continued west up the valley about 300 to 400 ft above ground level (agl) for about 2 nm, then made a sharp left turn and descended to the ground. The airplane impacted the ground in a nose-low attitude and came to rest upright. The forward fuselage and cockpit area were crushed upward and aft. Flight control continuity was confirmed from all flight control surfaces, through a few impact separations, to the cockpit controls. The flaps were partially extended. The pitch trim jackscrew was found in a full nose-up position. The propeller damage signatures were indicative of the engine operating at the time of impact. Examination of the airframe and engine did not reveal any preaccident mechanical malfunctions or failures that would have precluded normal operation. The engine data monitor data indicated the engine was operating normally with no anomalies noted. A postaccident weight calculation, including fuel, revealed the airplane was about 61 lbs over its maximum gross weight. The airplane's center of gravity could not be calculated since the exact location/station of the cargo could not be determined. The pilot who discovered the wreckage stated that, on the afternoon of the accident, there was significant wind shear in the area with sustained wind at least 20 kts and gusting to at least 30 kts. He stated that the wind gusts were violent, which made him park his airplane on an airstrip about 15 miles east of the gravel airstrip and wait for the wind to subside. He added that another pilot who flew northbound over the gravel strip a few hours after the accident time reported that the wind conditions were very turbulent. The circumstances of the accident were consistent with the pilot’s loss of control shortly after taking off into reported high gusting wind.

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. Loss of control in flight during initial climb defining event

The NTSB's findings

  • Environmental issues › Conditions/weather/phenomena › Wind › High wind › Contributed to outcome
  • Environmental issues › Conditions/weather/phenomena › Wind › Gusts › Contributed to outcome
  • Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Altitude › Not attained/maintained
  • Personnel issues › Action/decision › Info processing/decision › Decision making/judgment › Pilot
  • Aircraft › Aircraft oper/perf/capability › Aircraft capability › Maximum weight › Capability exceeded

Pilot

  • Certificate: private
  • Ratings: single-engine land
  • Flight time: 599.2 hours in all; 14.3 in the last 30 days
  • Last flight review: May 25, 2022
  • Medical certificate: Class 3 (with waivers/limitations)
  • Seat: frt
  • Injury: fatal

The aircraft

  • Last inspection: inspection type not recorded
  • Maximum gross weight: 1,750 lb
  • Seats: 3
  • Landing gear: fixed
  • Engine: Lycoming O-320-A2B (piston); 0 hours total

The flight

  • Departed from: Marsh Strip AK at 4:49 pm
  • Destination: PALR Chandalar Lake AK
  • Flight plan: none

Weather at the time

  • Light: daylight
  • Wind: at 20 knots, gusting 30
  • Temperature: 0°F (-18°C), dew point 0°F (-18°C)

Injuries

FatalSeriousMinorNone
Flig1

Other NTSB records under N3937M the same tail number, which may have belonged to a different aircraft at the time

2018-06-02GAA18CA320 · accident near Nulato, AK · substantial damage · no injuries

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 docket at the NTSB holds the report as a PDF and the investigation's photographs and documents. This site 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 ANC22FA066.