N888MT

Substantial
Fatal

CESSNA 340S/N: 340A0763

Accident Details

Date
Wednesday, August 27, 2025
NTSB Number
CEN25FA346
Location
Kearney, MO
Event ID
20250827200880
Coordinates
39.349484, -94.306452
Aircraft Damage
Substantial
Highest Injury
Fatal
Fatalities
2
Serious Injuries
0
Minor Injuries
0
Uninjured
0
Total Aboard
2

Aircraft Information

Registration
Make
CESSNA
Serial Number
340A0763
Engine Type
Reciprocating
Year Built
1979
Model / ICAO
340C340
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2
Seats
6
FAA Model
340A

Registered Owner (Current)

Name
SPELTS MARK WARREN TRUSTEE
Address
3191 VIA CASITA PL
City
CHICO
State / Zip Code
CA 95928-8416
Country
United States

Analysis

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.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN25FA346