WPR25FA240
2025-08-05 · Chinle, Arizona, United States · Fatal · 1 aircraft · Status: In work
Airport E91
Current FAA registration · N534AW
- Make / Model
- BEECH 300
- Year of manufacture
- 1988 · 37 years old at event
- Engine
- P&W CANADA PT6A-60A (1050 hp)
- Seats / Engines
- 19 seats · 2 engines
- Last airworthiness date
- 20241002
- ADS-B equipped
- Yes — Mode-S A6BF5E
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual 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. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2025_WPR25FA240.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
Matched on aircraft type. All research papers
- NASA NTRS 2019 · Reprint (Version printed in journal) Deep stall characteristics of MU-300
The deep stall characteristics of the MU-300 Diamond aircraft are described. The MU-300 obtained type certification from the FAA in 1981, and from Canada, West Germany, and England in 1983.
- NASA NTRS 2019 · Technical Memorandum (TM) Reporter Concerns in 300 Mode-Related Incident Reports from NASA's Aviation Safety Reporting System
A model has been developed which represents prominent reporter concerns expressed in the narratives of 300 mode-related incident reports from NASA's Aviation Safety Reporting System (ASRS).
- NTSB Aircraft Accident Reports 2021 · Accident report Crash of Atlas Air Flight 3591, Boeing 767-300 (N1217A)
Atlas Air 3591 crashed into Trinity Bay, Texas, February 23, 2019. Investigation of the in-flight loss-of-control crash of Atlas Air 3591 into Trinity Bay, Texas.
- NASA NTRS 2014 · Presentation 300 FT Runway Visual Range (RVR) Experiment Review
- arXiv 2026 · arXiv preprint Quantifying the Reality Gap for RL-Based UAV Placement at mmWave and Sub-THz
Reinforcement learning (RL) policies for unmanned aerial vehicle (UAV) placement in mmWave and sub-terahertz networks are typically trained on simplified analytical channels.
- arXiv 2026 · arXiv preprint Multi-Domain Physics-Based MDO of Multirotor UAVs: A Deterministic Framework for Discrete COTS Sizing
Multirotor Unmanned Aerial Vehicle (UAV) design is governed by a tightly coupled system of non-linear equations spanning structural mechanics, electrochemistry, aerodynamics, and kinematics.