20260907013209A

Accident · Substantial damage

FAA accident report · Van Dyke Thomas P CH701XV · Neosho, MO · September 7, 2026

Date
September 7, 2026 · 17:42 local
Place
Neosho, MO
Airport
Neosho Hugh Robinson
Phase of flight
Maneuver
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N101XV
NTSB investigation
NTSBCEN26FA311
Reported as
Van Dyke Thomas P CH701XV
Reported engine
ROTAX 912UL
People aboard
2
Fatal injuries
2
Other injuries
0
Pilot’s certificate
Private pilot

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.

The pilot was reportedly performing pattern work when the aircraft entered a nearly vertical decent and impacted the terrain. The location of the impact is consistent with the left crosswind to left downwind for runway 19. With the exception of the left inboard leading-edge stol slat, the aircraft wreckage was found within 15 yards of the point of impact. The aircraft was destroyed, with the exception of the empennage, which appeared intact and relatively undamaged. On-scene investigators determined flight control continuity; however, the elevator control stop appeared to be broken off and missing. The elevator bell crank appeared to have traveled beyond its normal range and was jammed, allowing only a full nose-down position. It is currently unknown if this was a pre-accident condition. A dash camera located about .8 nautical miles east of the airport recorded an unknown object departing and falling away from the aircraft shortly before the aircraft nosed over. A few days after the accident, law enforcement located the leading-edge slat about 1/8 mile from the main wreckage.

As the FAA filed it

THE PILOT WAS REPORTEDLY PERFORMING PATTERN WORK WHEN THE AIRCRAFT ENTERED A NEARLY VERTICAL DECENT AND IMPACTED THE TERRAIN. THE LOCATION OF THE IMPACT IS CONSISTENT WITH THE LEFT CROSSWIND TO LEFT DOWNWIND FOR RUNWAY 19. WITH THE EXCEPTION OF THE LEFT INBOARD LEADING-EDGE STOL SLAT, THE AIRCRAFT WRECKAGE WAS FOUND WITHIN 15 YARDS OF THE POINT OF IMPACT. THE AIRCRAFT WAS DESTROYED, WITH THE EXCEPTION OF THE EMPENNAGE, WHICH APPEARED INTACT AND RELATIVELY UNDAMAGED. ON-SCENE INVESTIGATORS DETERMINED FLIGHT CONTROL CONTINUITY; HOWEVER, THE ELEVATOR CONTROL STOP APPEARED TO BE BROKEN OFF AND MISSING. THE ELEVATOR BELL CRANK APPEARED TO HAVE TRAVELED BEYOND ITS NORMAL RANGE AND WAS JAMMED, ALLOWING ONLY A FULL NOSE-DOWN POSITION. IT IS CURRENTLY UNKNOWN IF THIS WAS A PRE-ACCIDENT CONDITION. A DASH CAMERA LOCATED ABOUT .8 NAUTICAL MILES EAST OF THE AIRPORT RECORDED AN UNKNOWN OBJECT DEPARTING AND FALLING AWAY FROM THE AIRCRAFT SHORTLY BEFORE THE AIRCRAFT NOSED OVER. A FEW DAYS AFTER THE ACCIDENT, LAW ENFORCEMENT LOCATED THE LEADING-EDGE SLAT ABOUT 1/8 MILE FROM THE MAIN WRECKAGE.

NTSB investigation

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