N9853M

Destroyed
Serious

ZENITH Zodiac CH601S/N: 6-3624

Accident Details

Date
Sunday, December 8, 2024
NTSB Number
CEN25FA056
Location
Columbia, IL
Event ID
20241208199394
Coordinates
38.460748, -90.234427
Aircraft Damage
Destroyed
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
1

Aircraft Information

Registration
Make
ZENITH
Serial Number
6-3624
Engine Type
4-cycle
Year Built
2007
Model / ICAO
Zodiac CH601
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
ZENITH ZODIAC 601HDS

Registered Owner (Current)

Name
BRENNER MICHAEL P
Address
6351 BRAND LAKE DR
City
WATERLOO
State / Zip Code
IL 62298-3029
Country
United States

Analysis

On September 8, 2024, about 1207 central standard time, a Zenith Zodiac CH601 airplane, N9853M, was destroyed when it was involved in an accident near Columbia, Illinois. The pilot sustained serious injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The airplane was returning to Sackman Field Airport (IL91) in Columbia, Illinois, after suffering an apparent oil leak during a maintenance test flight. The pilot stated to first responders that he smelled oil and the cockpit started to fill with smoke. During the approach, the pilot opened the cockpit canopy to attempt to regain visibility and lost control of the airplane. The airplane impacted the ground and a postimpact fire ensued and destroyed the airplane.

The accident site was in a flat agricultural field about 0.3 nautical miles northwest of the approach end of runway 21. A nearby surveillance camera recording showed the airplane impact the field in a nose high upright configuration, nose over, and come to rest inverted with smoke immediately visible. The pilot stated that he used an onboard fire extinguisher until two witnesses arrived and pulled him from the airplane. The engine compartment, forward fuselage, and cockpit were fully engulfed by fire when first responders.

The debris path extended in the field about 60 ft on a heading of 140°, to the main wreckage. The airplane engine compartment, fuselage, and inboard sections of both wings had extensive thermal damage from a post-crash fire. Flight control continuity from the flight control surfaces to the cockpit controls were confirmed along with the engine power control.

The engine was an experimental inline four cylinder, normally aspirated, manufactured by Aero Momentum and was observed to have damage consisting of several holes in the engine case and oil pan that corresponded with a damaged piston assembly.

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# CEN25FA056