20260105000229A

Accident · Substantial damage

FAA accident report · Canard Aero SW-51 MUSTANG · Fredericksburg, TX · January 5, 2026

Date
January 5, 2026 · 15:21 local
Place
Fredericksburg, TX
Airport
Gillespie County Airport
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N351MT
NTSB investigation
NTSBCEN26LA079
Reported as
Canard Aero SW-51 Mustang
Reported engine
ROTAX 916 IS A
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Airline transport
Pilot’s flight hours
5,000 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.

On 01/05/2026 around 1521 CDT, the pilot in command conducted the maiden flight of his new experimental, amateur built aircraft. The pilot stated that he had a briefing and his taxi and run-up checks were all normal. Shortly after take-off the pilot experienced a substantial engine power loss after lift-off while still at very low altitude. With the throttle and propeller controls fully forward, the aircraft was unable to maintain level flight. The pilot elected to land straight ahead, on the same runway with the remaining runway available.

After touchdown, the aircraft sustained substantial damage to the left main landing gear and left wing, that led to a loss of directional control during the landing roll, culminating in an approximately 180 degree pivot on the runway.

Then the pilot completed the engine shutdown and emergency ground egress.

As the FAA filed it

ON 01/05/2026 AROUND 1521 CDT, THE PILOT IN COMMAND CONDUCTED THE MAIDEN FLIGHT OF HIS NEW EXPERIMENTAL, AMATEUR BUILT AIRCRAFT. THE PILOT STATED THAT HE HAD A BRIEFING AND HIS TAXI AND RUN-UP CHECKS WERE ALL NORMAL. SHORTLY AFTER TAKE-OFF THE PILOT EXPERIENCED A SUBSTANTIAL ENGINE POWER LOSS AFTER LIFT-OFF WHILE STILL AT VERY LOW ALTITUDE. WITH THE THROTTLE AND PROPELLER CONTROLS FULLY FORWARD, THE AIRCRAFT WAS UNABLE TO MAINTAIN LEVEL FLIGHT. THE PILOT ELECTED TO LAND STRAIGHT AHEAD, ON THE SAME RUNWAY WITH THE REMAINING RUNWAY AVAILABLE.

AFTER TOUCHDOWN, THE AIRCRAFT SUSTAINED SUBSTANTIAL DAMAGE TO THE LEFT MAIN LANDING GEAR AND LEFT WING, THAT LED TO A LOSS OF DIRECTIONAL CONTROL DURING THE LANDING ROLL, CULMINATING IN AN APPROXIMATELY 180 DEGREE PIVOT ON THE RUNWAY.

THEN THE PILOT COMPLETED THE ENGINE SHUTDOWN AND EMERGENCY GROUND EGRESS.

NTSB investigation

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