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Accidents · NTSB DCA26LA285 · Final report

Leigh Aerosystems CORP E100 accident near Douglas, Arizona, June 26, 2026

On June 26, 2026 at about 6:40 pm local time, a 2024 Leigh Aerosystems CORP E100 (powered-lift aircraft), registered N1224E, was substantially damaged in an accident during landing near Douglas, Arizona (Bisbee Douglas Intl airport). It was a flight test under general aviation rules (Part 91). No one was hurt; 1 person was on board or involved. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

Degraded engine and propeller performance during hot and high-density altitude operations, which resulted in a high descent rate and subsequent hard landing.

Source: NTSB aviation accident database, copy made November 2, 2026. Docket and reports at the NTSB.

What the record shows

Date
June 26, 2026 · about 6:40 pm local time · cases in 2026
Place
Douglas, Arizona · Bisbee Douglas Intl · cases near this airport · map
Type
Accident
Injuries
No one was hurt; 1 person was on board or involved.
Weather
visual conditions (good weather)
Aircraft
Leigh Aerosystems CORP E100, built 2024
Registration
N1224E · registry record · serial AV2
Damage
Substantial damage
Flight
Flight test · general aviation rules (Part 91)

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

On June 26, 2026, about 1140 Pacific daylight time, an experimental Leigh Aerosystems E100 unmanned aircraft system (UAS) experienced a hard landing at Bisbee Douglas International Airport, Douglas, Arizona. At the time of the accident, the aircraft was operated by a remote pilot as a flight test under the provisions of Title 14 Code of Federal Regulations Part 91 and a Federal Aviation Administration (FAA) Certificate of Authorization (COA). The aircraft sustained substantial damage and there were no injuries to ground personnel. Figure 1. Leigh Aerosystems E100 UAS. (Source: Northrop Grumman) According to the remote pilot, the intent of the flight was to test the aircraft’s hover capabilities and develop performance data for hot day conditions. The aircraft performed controlled flight up to a planned altitude of about 40 ft above ground level but then began to descend at a rate faster than planned. The aircraft subsequently experienced a hard landing about 10-15 ft from its takeoff location, resulting in the right spar and wing separating from the fuselage. The aircraft was subsequently shut down. Postaccident analysis by the operator of the flight test found that the high-density altitude (about 7,500 ft) at the time of the flight degraded both engine and propeller performance, which limited the maneuverability and controllability of the aircraft.

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. Hard landing during landing defining event

The NTSB's findings

  • Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Descent rate › Not attained/maintained
  • Environmental issues › Conditions/weather/phenomena › Temp/humidity/pressure › High density altitude › Effect on operation

Pilot

  • Medical certificate: Class 2 (without waivers/limitations)
  • Seat: none
  • Injury: no injuries

The aircraft

  • Airframe total time: 3.4 hours
  • Last inspection: condition inspection, June 26, 2026
  • Maximum gross weight: 330 lb
  • Seats: 0
  • Landing gear: fixed
  • Engine: Desert Acf DA-215 (piston); 0 hours total
  • Operator: Northrop Grumman Systems CORP

The flight

  • Flight plan: none
  • Runway 17/3, 6,430 ft by 100 ft

Weather at the time

  • Light: daylight
  • Wind: from 190° at 11 knots, gusting 20
  • Visibility: 10 statute miles
  • Sky: a few clouds at 9,000 ft
  • Temperature: 97°F (36°C), dew point 52°F (11°C)
  • Altimeter: 30.08 inHg
  • Observation at 11:56 am from KDUG, 1 miles away

Weather report (METAR): METAR KDUG 261856Z AUTO 19011G20KT 10SM FEW090 36/11 A3008 RMK AO2 SLP103 T03560106 TSNO=

Injuries

FatalSeriousMinorNone
Flight crew1

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

1 document, released by the NTSB on October 22, 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.

The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.

Connections how this case links to the rest of the register

Aircraft
Place

The whole map of how records connect · these connections as data: /graph/accident/DCA26LA285.json.

The bigger picture in Aviation Analytics: accidents over time since 1982, by model, by phase of flight and conditions, by place and on the map.

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 does not name anyone involved, its policy at this time. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.