Pilot Debrief

BEECH 300 near Chinle, AZ — 2025-08-05

Investigation ongoingWPR25FA240
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Date
2025-08-05
Location
Chinle, AZ, USA
Airport
E91
Aircraft
BEECH 300
Registration
N534AW
Category
Airplane
Highest injury
Fatal
Fatalities
4

Probable cause

NTSB has not published a probable cause for this accident yet. Preliminary reports describe what happened; the cause is determined later, often 12–24 months after the event.

NTSB narrative

On August 5, 2025, about 1245 mountain daylight time, a Beech 300, N534AW, was destroyed when it was involved in an accident near Chinle, Arizona. The pilot, co-pilot and two medical crew members were fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 135 positioning flight. Automatic dependent surveillance-broadcast (ADS-B) data and air traffic control radar data showed that the airplane departed Albuquerque International Sunport Airport (ABQ) Albuquerque, New Mexico about 1155, climbed to 18,000 ft mean sea level (msl) and proceeded direct to Chinle Municipal Airport (E91) Chinle, Arizona. About 1229 the airplane began a descent and about 1239, the airplane entered the traffic pattern on the downwind leg for runway 36. About 1240, while about 6,600 ft, the airplane turned right and entered the base leg. The last radar data point recorded the airplane about 6,100 ft, and about 2.8 miles southeast of the runway 36 threshold. According to a witness, who was located about one quarter mile from the airport, he observed the airplane on a northbound heading over the runway while flying about 180 ft above ground level (agl). The left wing banked erratically multiple times and then leveled off, at which time the airplane pitched up. The left wing then dropped into a knife edge attitude, while the airplane descended to the ground and immediately erupted in flames. The airplane impacted open terrain about 990 ft west of runway 36 at an elevation of about 5,510 ft. A path of disturbed terrain and vegetation extended about 281 ft from the main wreckage and included multiple airframe components. A postaccident fire thermally damaged the fuselage and wings. A cockpit voice recorder was recovered from the airplane and shipped to the NTSB Vehicle Recorders Laboratory for download. The airplane was recovered to a secure facility for further examination.

Preliminary NTSB coding

  • Loss of control in flight · Approach-VFR go-around
  • Go-Around (VFR)
View NTSB preliminary report

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