20250913020969A

Accident · Substantial damage

FAA accident report · Pegasus QUANTUM 15 · Bedford, IN · September 13, 2025

Date
September 13, 2025 · 16:25 local
Place
Bedford, IN
Airport
Virgil I Grissom Municipal
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N36TJ
NTSB investigation
NTSBCEN25LA379
Reported as
Pegasus Quantum 15
Reported engine
ROTAX 503 series
People aboard
1
Fatal injuries
0
Other injuries
1

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 September 13, 2025, the subject pilot was taxiing from his hangar to runway 24 at the virgin I. Grissom municipal airport (bfr), Bedford, Indiana. An a&pia mechanic on the field witnessed the subject aircraft's engine quit as it approached taxiway a leading up to runway 24. The witness reported that he watched the pilot attempt to restart the engine 5 times. The engine restarted and the witness was expecting the aircraft to taxi to the maintnenance shop or return to the hangar. The pilot continued to the runway and proceeded with a takeoff from runway 24. The witness heard the aircraft abort the takeoff and return to the threshold of runway 24. At approximately 16:25 local, the aircraft continued with a second takeoff attempt. The witness stated that it sounded like the aircraft was producing about fifty (50) percent power.

The aircraft was not able to maintain a flying speed and the pilot turned to the right (north). The aircraft impacted a soybean field 0.2 miles from the departure end of runway 24 at a heading of 308 degrees.

Tire tracks from first responders deformed the crops surrounding the impact point. The aircraft came to rest on its left side. The left wing was folded backwards. The fuselage was laying on its left side and at a heading of 210 degrees.

Impact to the nose of the aircraft factured the fiberglass fuselage and pushed the nosegear upwards and inwards into the fuselage. The nose low impact angle would be consistent with the main gear contacting the 30 inch tall soybean first, causing a forward pitching moment

Fuel was leaking from the fuel tank. The fuel selector valve was in the "on" position. All three propellers struck the ground and delaminated

As the FAA filed it

ON SEPTEMBER 13, 2025, THE SUBJECT PILOT WAS TAXIING FROM HIS HANGAR TO RUNWAY 24 AT THE VIRGIN I. GRISSOM MUNICIPAL AIRPORT (BFR), BEDFORD, INDIANA. AN A&PIA MECHANIC ON THE FIELD WITNESSED THE SUBJECT AIRCRAFT'S ENGINE QUIT AS IT APPROACHED TAXIWAY A LEADING UP TO RUNWAY 24. THE WITNESS REPORTED THAT HE WATCHED THE PILOT ATTEMPT TO RESTART THE ENGINE 5 TIMES. THE ENGINE RESTARTED AND THE WITNESS WAS EXPECTING THE AIRCRAFT TO TAXI TO THE MAINTNENANCE SHOP OR RETURN TO THE HANGAR. THE PILOT CONTINUED TO THE RUNWAY AND PROCEEDED WITH A TAKEOFF FROM RUNWAY 24. THE WITNESS HEARD THE AIRCRAFT ABORT THE TAKEOFF AND RETURN TO THE THRESHOLD OF RUNWAY 24. AT APPROXIMATELY 16:25 LOCAL, THE AIRCRAFT CONTINUED WITH A SECOND TAKEOFF ATTEMPT. THE WITNESS STATED THAT IT SOUNDED LIKE THE AIRCRAFT WAS PRODUCING ABOUT FIFTY (50) PERCENT POWER.

THE AIRCRAFT WAS NOT ABLE TO MAINTAIN A FLYING SPEED AND THE PILOT TURNED TO THE RIGHT (NORTH). THE AIRCRAFT IMPACTED A SOYBEAN FIELD 0.2 MILES FROM THE DEPARTURE END OF RUNWAY 24 AT A HEADING OF 308 DEGREES.

TIRE TRACKS FROM FIRST RESPONDERS DEFORMED THE CROPS SURROUNDING THE IMPACT POINT. THE AIRCRAFT CAME TO REST ON ITS LEFT SIDE. THE LEFT WING WAS FOLDED BACKWARDS. THE FUSELAGE WAS LAYING ON ITS LEFT SIDE AND AT A HEADING OF 210 DEGREES.

IMPACT TO THE NOSE OF THE AIRCRAFT FACTURED THE FIBERGLASS FUSELAGE AND PUSHED THE NOSEGEAR UPWARDS AND INWARDS INTO THE FUSELAGE. THE NOSE LOW IMPACT ANGLE WOULD BE CONSISTENT WITH THE MAIN GEAR CONTACTING THE 30 INCH TALL SOYBEAN FIRST, CAUSING A FORWARD PITCHING MOMENT

FUEL WAS LEAKING FROM THE FUEL TANK. THE FUEL SELECTOR VALVE WAS IN THE "ON" POSITION. ALL THREE PROPELLERS STRUCK THE GROUND AND DELAMINATED

NTSB investigation

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