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Accidents · NTSB WPR24FA202 · Final report

Air Tractor INC AT-802A accident near Capitan, New Mexico, June 21, 2024

On June 21, 2024 at about 4:58 pm local time, a 2018 Air Tractor INC AT-802A, registered N331BS, was destroyed in an accident during enroute (cruise) near Capitan, New Mexico. It was a positioning flight under general aviation rules (Part 91). 1 person was killed. The weather was instrument conditions (cloud, fog or low visibility).

The NTSB's probable cause their words, unchanged

The pilot’s decision to continue the visual flight rules flight through an apparent visual corridor that rapidly narrowed due to rising terrain and mountain obscuration, resulting in momentary instrument meteorological conditions and the pilot’s subsequent controlled flight into the obscured terrain.

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

What the record shows

Date
June 21, 2024 · about 4:58 pm local time
Place
Capitan, New Mexico · map
Type
Accident
Injuries
1 person was killed.
Weather
instrument conditions (cloud, fog or low visibility)
Aircraft
Air Tractor INC AT-802A, built 2018 · all AT-802As on the register
Registration
N331BS · no longer on the register · serial 802A-0749
Damage
Destroyed
Flight
Positioning flight · general aviation rules (Part 91)

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

A flight of three fire-fighting airplanes was being repositioned on a visual flight rules flight from Texas to Oregon. The flight crews planned a refueling stop at an airport in New Mexico. Before reaching the airport, they saw “a light rain shower” ahead of them near the Capitan Mountains in New Mexico. The pilots of the first two airplanes maneuvered to avoid the weather, and the lead pilot directed the other two airplanes to turn 30° and climb to reacquire visual contact with one another. However, one of the pilots observed the accident airplane maneuvering about 2,000 ft below the other airplanes, and the accident pilot subsequently reported that he had a visual flight rules (VFR) corridor through the weather. The pilot likely elected to continue through the VFR corridor rather than climb with the other airplanes. Because the airplanes had been cruising at about 9,500 ft mean sea level (msl), the accident airplane was operating at about 7,500 ft msl in mountainous terrain where elevations in the Capitan Mountain Range exceeded 10,000 ft msl. After the first two airplanes landed at the planned refueling destination, the pilots realized that the accident airplane had not arrived and was missing. After the FAA issued an Alert Notice for the missing airplane, the wreckage was located about 9 miles east-northeast of the Capitan Mountains by another airplane. All required flight control surfaces of the airplane were found at the accident site. The ground scars, tree impact signatures, and wreckage impact fragment distribution indicated that the airplane impacted rising terrain in a near-level flight attitude at high forward velocity, consistent with controlled flight into terrain. Although the airplane was highly fragmented, postaccident examination of the airplane revealed no evidence of preimpact malfunctions or failures that would have precluded normal operation. The impact signatures on the propeller blades were consistent with high RPM and engine power at the time of impact. Weather information for the area indicated widespread mountain obscuration, low ceilings, and light rain near the accident site. The National Weather Service (NWS) had several AlRMETs that were current at the time of the accident for mountain obscuration in the area, and weather observations near the accident site reported instrument flight rules (IFR) and low IFR (LIFR) conditions. Satellite imagery, weather radar data, and model sounding data indicated extensive overcast clouds and saturated atmospheric conditions over the mountainous terrain surrounding the accident site. Although IFR and mountain obscuration conditions existed in the surrounding area, the available evidence suggests that the pilot was likely attempting to maintain visual meteorological conditions while maneuvering through an apparent VFR corridor. As the airplane approached the mountainous terrain, the apparent VFR corridor ahead likely deteriorated rapidly due to rising terrain and mountain obscuration. Given the airplane’s near-level, high-speed impact attitude, the pilot was likely unable to perceive and avoid the terrain in sufficient time to prevent the collision.

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. Controlled flight into terrain or object (CFIT) during maneuvering
  2. Loss of visual reference during maneuvering
  3. VFR encounter with IMC during enroute (cruise) defining event

The NTSB's findings

  • Personnel issues › Action/decision › Action › Incorrect action selection › Pilot
  • Personnel issues › Action/decision › Info processing/decision › Decision making/judgment › Pilot
  • Environmental issues › Physical environment › Terrain › Mountainous/hilly terrain › Awareness of condition
  • Environmental issues › Conditions/weather/phenomena › Ceiling/visibility/precip › Obscuration › Decision related to condition
  • Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Altitude › Not attained/maintained

Pilot

  • Certificate: commercial pilot
  • Ratings: single-engine land; single-engine sea; instrument: airplane; rotorcraft: unmanned (suas)
  • Flight time: 14,042 hours in all; 133 in this make and model; 14,042 as pilot in command
  • Medical certificate: Class 2 (with waivers/limitations)
  • Seat: sngl
  • Injury: fatal

The aircraft

  • Airframe total time: 1,243 hours
  • Last inspection: annual inspection, April 1, 2024
  • Seats: 2
  • Landing gear: fixed
  • Engine: P&W Canada PT6A-67AG (turboprop); 1,243 hours total
  • Operator: Coastal Air Strike

The flight

  • Departed from: E38 Alpine TX at 4:00 pm
  • Destination: GUP Gallup NM
  • Flight plan: none

Weather at the time

  • Light: daylight
  • Wind: from 130° at 11 knots
  • Visibility: 10 statute miles
  • Sky: broken clouds at 300 ft
  • Temperature: 63°F (17°C), dew point 63°F (17°C)
  • Altimeter: 30.39 inHg
  • Observation at 10:15 am from KSRR, 9 miles away

Weather report (METAR): KSRR 211615Z AUTO 13011KT 10SM BKN003 BKN007 17/17 A3039 RMK AO2

Injuries

FatalSeriousMinorNone
Flight crew1

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

12 documents, released by the NTSB on May 28, 2026. 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 Pilot/operator Aircraft Accident Report, NTSB Form 6120.1 PDF, 11 pages · our copy View Download
2 Memorandum for Records PDF, 8 pages · our copy View Download
3 Accident Site Summary Report PDF, 6 pages · our copy View Download
4 POH Excerpt PDF, 1 page · our copy View Download
5 Meteorology PDF, 10 pages · our copy View Download
6 Route of Flight Diagrams PDF, 1 page · our copy View Download
7 Logbook Excerpt PDF, 1 page · our copy View Download
8 FAA Ac 61-134 Excerpts PDF, 5 pages · our copy View Download
9 Pilot Training Records PDF, 4 pages · our copy View Download
10 Toxicological Report PDF, 1 page · our copy View Download
11 Party Member Form PDF, 2 pages · our copy View Download
12 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.