2 fatalities

27 Aug 2025: CESSNA 340 A (N888MT) — SPELTS MARK WARREN TRUSTEE — Kearney, MO

Kearney, MO, United States

On 27 Aug 2025, a CESSNA 340 A (registration N888MT) operated by SPELTS MARK WARREN TRUSTEE was involved in an aviation accident near Kearney, MO. 2 people were killed. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On August 27, 2025, a Cessna 340A (N888MT) was substantially damaged in a crash near Kearney, Missouri, fatally injuring the pilot and passenger. The airplane was on a personal flight from Washington, Missouri to Mosby, Missouri.

Accident Overview

On August 27, 2025, at about 1158 central daylight time, a Cessna 340A, registration N888MT, was substantially damaged when it crashed near Kearney, Missouri. The pilot and passenger on board were fatally injured. The flight was conducted under Title 14 Code of Federal Regulations Part 91 as a personal flight.

Flight History

ADS-B data indicated that the airplane departed Washington Regional Airport (KFYG) in Washington, Missouri, at about 1057. It cruised at an altitude of 4,500 ft mean sea level en route to the Midwest National Air Center Airport (KGPH) in Mosby, Missouri. Approximately 25 miles from the destination, the airplane began a descent and entered the traffic pattern for a left base turn. Its altitude was lower than typical for a standard traffic pattern and continued to decrease.

Eyewitness Account

An eyewitness residing near the accident site reported that the airplane appeared to be flying low and slow. The left wing dipped momentarily, then the wings returned to level, but the left wing dipped again. The airplane then rolled to the left until it collided with terrain.

Impact and Wreckage

The airplane impacted an uncultivated soybean field about 0.6 miles from the approach end of runway 18. The initial impact point showed ground scars consistent with the left wing and nose of the airplane. A divot caused by the right engine contained the right propeller assembly, which had fractured at the crankshaft. The debris field was approximately 95 ft long, oriented along a 225° magnetic heading. The main wreckage included the fuselage, empennage, tail section, both wings, both engines, and the left propeller. It came to rest aligned on a 120° magnetic heading. A postimpact fire consumed a large portion of the fuselage.

Postaccident Examination

On-scene examination revealed that the landing gear was extended and the flaps were retracted. Flight control continuity was confirmed from the cockpit to all flight control surfaces. The cockpit instrumentation and electronic displays were largely destroyed by fire. The wreckage was retained for further examination.