20250620007639A

Accident · Substantial damage

FAA accident report · TL Ultralight Sro STINGSPORT · Fredericksburg, VA · June 20, 2025

Date
June 20, 2025 · 14:00 local
Place
Fredericksburg, VA
Phase of flight
Cruise/Level Flight
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N878N
NTSB investigation
NTSBERA25LA236
Reported as
TL Ultralight Sro Stingsport
Reported engine
Bombardier ROTAX (ALL)
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Sport pilot
Pilot’s flight hours
205 total

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

PIC reported the aircraft's engine suddenly began to shake violently while in cruise flight for 5 seconds before the engine shut down un-commanded. The PIC executed a power off landing in a field near shannon airport (kezf). During the on-scene FAA investigation, 2 of the 3 propeller blades had separated from the propeller hub and could not be located at the accident scene. The violent nature of the in-flight engine vibrations and subsequent engine failure was caused by the in-flight separation of the propeller blades at a cruise power setting.

As the FAA filed it

PIC REPORTED THE AIRCRAFT'S ENGINE SUDDENLY BEGAN TO SHAKE VIOLENTLY WHILE IN CRUISE FLIGHT FOR 5 SECONDS BEFORE THE ENGINE SHUT DOWN UN-COMMANDED. THE PIC EXECUTED A POWER OFF LANDING IN A FIELD NEAR SHANNON AIRPORT (KEZF). DURING THE ON-SCENE FAA INVESTIGATION, 2 OF THE 3 PROPELLER BLADES HAD SEPARATED FROM THE PROPELLER HUB AND COULD NOT BE LOCATED AT THE ACCIDENT SCENE. THE VIOLENT NATURE OF THE IN-FLIGHT ENGINE VIBRATIONS AND SUBSEQUENT ENGINE FAILURE WAS CAUSED BY THE IN-FLIGHT SEPARATION OF THE PROPELLER BLADES AT A CRUISE POWER SETTING.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.