20260416007419I

Incident · Substantial damage

FAA incident report · Titan T-51 · Elizabethtown, KY · April 16, 2026

Date
April 16, 2026 · 09:04 local
Place
Elizabethtown, KY
Airport
Addington Field
Phase of flight
Landing: Approach
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N151TA
Reported as
Titan T-51
Reported engine
HONDA J35A
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
1,837 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.

During cruise flight, the pilot noticed the airspeed was decaying and the aircraft required increasing right rudder to maintain coordinated flight. The pilot elected to divert and assess the aircraft on the ground. During approach to the divert airfield the pilot selected landing gear down, however the landing gear failed to extend normally and the pilot does not recall seeing the landing gear position indicator lights or hearing the hydraulic pump. The pilot flew around the traffic pattern several times to troubleshoot the landing gear. The pilot also attempted an emergency extension while in the traffic pattern. It was uknown to the pilot if the landing gear had successfully locked in the down position. At this point the pilot also reported that engine RPM began to fluxuate. This prompted an immediate landing prior to confirming the landing gear was down and locked. Upon touchdown on the runway, the left main landing gear collapsed and the aircraft veered to the left. The aircraft ran off the left edge of the runway into grass. Upon entering the grass, the right main landing gear also collapsed. The aircraft stopped a short distance off the left edge of the runway on its belly with both main landing gear collapsed. All 4 propeller blades, both wingtips, the belly, and the tailwheel area sustained damage. The pilot was uninjured. The aircraft was lifted from the ground using a tractor and the main landing gear was manually extended and locked. The aircraft was then towed into a hangar for storage. The cause of the landing gear failure and RPM fluxuation is yet to be determined.

As the FAA filed it

DURING CRUISE FLIGHT, THE PILOT NOTICED THE AIRSPEED WAS DECAYING AND THE AIRCRAFT REQUIRED INCREASING RIGHT RUDDER TO MAINTAIN COORDINATED FLIGHT. THE PILOT ELECTED TO DIVERT AND ASSESS THE AIRCRAFT ON THE GROUND. DURING APPROACH TO THE DIVERT AIRFIELD THE PILOT SELECTED LANDING GEAR DOWN, HOWEVER THE LANDING GEAR FAILED TO EXTEND NORMALLY AND THE PILOT DOES NOT RECALL SEEING THE LANDING GEAR POSITION INDICATOR LIGHTS OR HEARING THE HYDRAULIC PUMP. THE PILOT FLEW AROUND THE TRAFFIC PATTERN SEVERAL TIMES TO TROUBLESHOOT THE LANDING GEAR. THE PILOT ALSO ATTEMPTED AN EMERGENCY EXTENSION WHILE IN THE TRAFFIC PATTERN. IT WAS UKNOWN TO THE PILOT IF THE LANDING GEAR HAD SUCCESSFULLY LOCKED IN THE DOWN POSITION. AT THIS POINT THE PILOT ALSO REPORTED THAT ENGINE RPM BEGAN TO FLUXUATE. THIS PROMPTED AN IMMEDIATE LANDING PRIOR TO CONFIRMING THE LANDING GEAR WAS DOWN AND LOCKED. UPON TOUCHDOWN ON THE RUNWAY, THE LEFT MAIN LANDING GEAR COLLAPSED AND THE AIRCRAFT VEERED TO THE LEFT. THE AIRCRAFT RAN OFF THE LEFT EDGE OF THE RUNWAY INTO GRASS. UPON ENTERING THE GRASS, THE RIGHT MAIN LANDING GEAR ALSO COLLAPSED. THE AIRCRAFT STOPPED A SHORT DISTANCE OFF THE LEFT EDGE OF THE RUNWAY ON ITS BELLY WITH BOTH MAIN LANDING GEAR COLLAPSED. ALL 4 PROPELLER BLADES, BOTH WINGTIPS, THE BELLY, AND THE TAILWHEEL AREA SUSTAINED DAMAGE. THE PILOT WAS UNINJURED. THE AIRCRAFT WAS LIFTED FROM THE GROUND USING A TRACTOR AND THE MAIN LANDING GEAR WAS MANUALLY EXTENDED AND LOCKED. THE AIRCRAFT WAS THEN TOWED INTO A HANGAR FOR STORAGE. THE CAUSE OF THE LANDING GEAR FAILURE AND RPM FLUXUATION IS YET TO BE DETERMINED.

Other reports on N151TA · 1

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