N951T

Destroyed
Fatal

BEECH M35S/N: D-6341

Accident Details

Date
Thursday, August 14, 2025
NTSB Number
WPR25FA256
Location
Des Moines, NM
Event ID
20250815200790
Coordinates
36.713680, -103.894300
Aircraft Damage
Destroyed
Highest Injury
Fatal
Fatalities
2
Serious Injuries
0
Minor Injuries
0
Uninjured
0
Total Aboard
2

Aircraft Information

Registration
Make
BEECH
Serial Number
D-6341
Engine Type
Reciprocating
Model / ICAO
M35BE35
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
5
FAA Model
M35

Registered Owner (Current)

Name
HOVERTER DOUGLAS K
Address
551 HAWTHORN CIR
City
FREDERICK
State / Zip Code
CO 80530-6010
Country
United States

Analysis

On August 13, 2025, about 2300 mountain daylight time, a Beech M35, N951T, was destroyed when it was involved in an accident near Des Moines, New Mexico. The pilot and passenger were fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The airplane was subject to an Alert Notification (ALNOT) that was issued on August 14, 2025, when the pilot did not show up to work in Uvalde, Texas. The accident site was located by the New Mexico State Police later that same day.

According to preliminary ADS-B data, the airplane departed from the Pueblo Memorial Airport (PUB), Pueblo, Colorado about 2200 and flew on a southerly heading toward Texas. The last ADS-B data point was at an altitude of 7,900 ft msl about a 1/4 mile north of the accident site.

Examination of the accident site revealed that the airplane had impacted wooded terrain on the northern side of Sierra Grande Mountain at an elevation of about 7,810 ft mean sea level (msl). The first identified point of contact (FIPC) was a damaged tree about 20 ft tall. The wreckage debris path was oriented along a magnetic heading of about 280° and extended about 300 ft from the FIPC to the main wreckage and to the farthest piece of wreckage debris and was mostly consumed by the postcrash fire. The propeller assembly separated from the engine was located adjacent to the main wreckage. The engine separated from the engine mounts and came to rest about 50 ft west of the main wreckage. All major structural components of the airplane were accounted for at the accident site.

The wreckage was transported to a secure location 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# WPR25FA256