NTSB CAROL · Event
Event CEN25FA346
Registry · N888MT
FAA Aircraft Registry record.
Make / Model
CESSNA 340A
Year of manufacture
1979 · 46 years old at event
Engine
CONT MOTOR TSIO-520 SER (300 hp)
Seats / Engines
6 seats · 2 engines
Last airworthiness date
20000616
ADS-B equipped
Yes — Mode-S AC3CB2
Registrant of record
SPELTS MARK WARREN TRUSTEE
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
On August 27, 2025, about 1158 central daylight time, a Cessna 340A, N888MT, was substantially damaged when it was involved in an accident near Kearney, Missouri. The pilot and passenger were fatally injured. The airplane operated as a Title 14 Code of Federal Regulations Part 91 personal flight. ADS-B data showed that the airplane departed the Washington Regional Airport (KFYG), Washington, Missouri, about 1057, and cruised at 4,500 ft mean sea level towards the Midwest National Air Center Airport (KGPH), Mosby, Missouri. About 25 miles from the airport, the airplane descended and entered the traffic pattern for a left base turn. The airplane’s altitude was lower than normal for a standard traffic pattern and continued to descend. An eyewitness who lived near the accident site reported that the airplane appeared to be low and slow. The airplane’s left wing dipped down momentarily, returned wings level, then the left wing dipped again, and the airplane rolled left until it collided with terrain. Figure 1 ADS-B and Accident Site The airplane impacted an uncultivated soybean field about 0.6 miles from the approach end of runway 18. The initial impact point consisted of ground scars consistent with the left wing and airplane nose. A divot in the ground made by the right engine contained the right propeller assembly which had fractured at the crankshaft. The debris field was about 95 ft long, orientated along a 225° magnetic heading. The main wreckage consisted of the remainder of the airplane, to include the fuselage, empennage, tail section, both wings, both engines, and the left propeller. The main wreckage was aligned on a 120° magnetic heading. A postimpact fire had consumed a large portion of the fuselage. On-scene examination of the airplane found that the landing gear was down, and the flaps were retracted. Flight control continuity was established from the cockpit to the flight controls. The cockpit instrumentation and electronic displays were largely destroyed in the fire. The wreckage was retained for further examination. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2025_CEN25FA346.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
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Academic papers and agency reports matching this event's aircraft type. Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
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