20250610007089A

Accident · Substantial damage

FAA accident report · Beech A36 · Murfreesboro, TN · June 10, 2025

Date
June 10, 2025 · 11:24 local
Place
Murfreesboro, TN
Phase of flight
Descent
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N15PM
NTSB investigation
NTSBERA25LA226
Reported as
Beech A36
Reported engine
Continental IO-520 series
People aboard
3
Fatal injuries
0
Other injuries
2

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 June 10, 2025, about 1220 central daylight time, a Beech A36, sn E1016 was substantially damaged when it was involved in an accident near Murfreesboro, Tennessee. The private pilot and a passenger were not injured. A second passenger was injured. The airplane was operated as a title 14 code of federal regulations part 91 personal flight.

According to the pilot, the flight departed from Douglas municipal airport (dqh), Douglas, Florida and was enroute to Murfreesboro municipal airport (mbt), Murfreesboro, Tennessee when when a partial loss of engine power occurred. Based on the “stumble” of the engine, he switched from the left fuel tank to the right fuel tank and pushed the mixture control in, which initially “cleared up” the problem. Shortly after, the engine lost power again and the pilot declared an emergency. He quickly assessed that he would not be able to make it to mbt and as a result, he attempted to make a forced landing in a field. He then realized that the field was out of reach and attempted to turn towards a cemetery where he lowered the landing gear, pitched the nose up, and attempted to clear trees. The airplane contacted the trees prior to the cemetery and came to rest nose down, suspended in vegetation.

A postaccident examination by a federal aviation administration inspector revealed that the left fuel tank contained a small amount of fuel with no evidence of that tank being breached by impact. The right fuel tank was breached and contained about 10 gallons of fuel. The fuel selector was observed to be on the right fuel tank position. The ignition key was observed on “both”; the mixture control, propeller control, and throttle were observed full forward.

The wreckage was retained for further examination

As the FAA filed it

ON JUNE 10, 2025, ABOUT 1220 CENTRAL DAYLIGHT TIME, A BEECH A36, SN E1016 WAS SUBSTANTIALLY DAMAGED WHEN IT WAS INVOLVED IN AN ACCIDENT NEAR MURFREESBORO, TENNESSEE. THE PRIVATE PILOT AND A PASSENGER WERE NOT INJURED. A SECOND PASSENGER WAS INJURED. THE AIRPLANE WAS OPERATED AS A TITLE 14 CODE OF FEDERAL REGULATIONS PART 91 PERSONAL FLIGHT.

ACCORDING TO THE PILOT, THE FLIGHT DEPARTED FROM DOUGLAS MUNICIPAL AIRPORT (DQH), DOUGLAS, FLORIDA AND WAS ENROUTE TO MURFREESBORO MUNICIPAL AIRPORT (MBT), MURFREESBORO, TENNESSEE WHEN WHEN A PARTIAL LOSS OF ENGINE POWER OCCURRED. BASED ON THE “STUMBLE” OF THE ENGINE, HE SWITCHED FROM THE LEFT FUEL TANK TO THE RIGHT FUEL TANK AND PUSHED THE MIXTURE CONTROL IN, WHICH INITIALLY “CLEARED UP” THE PROBLEM. SHORTLY AFTER, THE ENGINE LOST POWER AGAIN AND THE PILOT DECLARED AN EMERGENCY. HE QUICKLY ASSESSED THAT HE WOULD NOT BE ABLE TO MAKE IT TO MBT AND AS A RESULT, HE ATTEMPTED TO MAKE A FORCED LANDING IN A FIELD. HE THEN REALIZED THAT THE FIELD WAS OUT OF REACH AND ATTEMPTED TO TURN TOWARDS A CEMETERY WHERE HE LOWERED THE LANDING GEAR, PITCHED THE NOSE UP, AND ATTEMPTED TO CLEAR TREES. THE AIRPLANE CONTACTED THE TREES PRIOR TO THE CEMETERY AND CAME TO REST NOSE DOWN, SUSPENDED IN VEGETATION.

A POSTACCIDENT EXAMINATION BY A FEDERAL AVIATION ADMINISTRATION INSPECTOR REVEALED THAT THE LEFT FUEL TANK CONTAINED A SMALL AMOUNT OF FUEL WITH NO EVIDENCE OF THAT TANK BEING BREACHED BY IMPACT. THE RIGHT FUEL TANK WAS BREACHED AND CONTAINED ABOUT 10 GALLONS OF FUEL. THE FUEL SELECTOR WAS OBSERVED TO BE ON THE RIGHT FUEL TANK POSITION. THE IGNITION KEY WAS OBSERVED ON “BOTH”; THE MIXTURE CONTROL, PROPELLER CONTROL, AND THROTTLE WERE OBSERVED FULL FORWARD.

THE WRECKAGE WAS RETAINED FOR FURTHER EXAMINATION

NTSB investigation

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

Other reports on N15PM · 3

Matched to the same aircraft by N-number and date.