20260720008859A

Accident · Destroyed

FAA accident report · Piper J3C-65 · Richmond, TX · July 20, 2026

Date
July 20, 2026 · 06:41 local
Place
Richmond, TX
Airport
Covey Trails
Phase of flight
Descent
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N92432
NTSB investigation
NTSBCEN26LA266
Reported as
Piper J3C-65
Reported engine
Continental A&C65 series
People aboard
1
Fatal injuries
0
Other injuries
1
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
5,045 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.

According to preliminary pilot statements and video accounts, the flight departed the airfield to the south for a local sunrise observation. The aircraft executed a right turn to the west, tracked back across the airfield heading east, and climbed to approximately 2,000 to 3,000 feet. After viewing the sunrise, the pilot initiated a turn back to the west and started a descent. The pilot reports a complete lapse of memory (retrograde amnesia) from this point of descent onward. Pilot suffered head trama during the accident and a broken ankle. Neighbor security camera footage (audio unavailable) captured the aircraft descending in a clean glide profile before it impacted a residential structure located on the east side of Covey Trails airfield. Post-accident examination confirmed flight control continuity from the cockpit controls to all respective flight control surfaces. Powerplant / propeller: the two-blade wood propeller and metal spinner exhibited little to no rotation marks and lacked torsional damage features typically consistent with an engine producing power at the time of impact. Impact site: the aircraft struck the roof/structure of a residence situated on the eastern perimeter of the airpark residential community. Preliminary assessment physical evidence—specifically the lack of propeller torsional damage combined with video confirmation of a clean glide path—strongly indicates an unpowered flight profile (engine starvation, failure, or stoppage) during the final maneuver back toward the airport environment. Investigation is ongoing to determine the exact cause of power loss and subsequent loss of control.

As the FAA filed it

ACCORDING TO PRELIMINARY PILOT STATEMENTS AND VIDEO ACCOUNTS, THE FLIGHT DEPARTED THE AIRFIELD TO THE SOUTH FOR A LOCAL SUNRISE OBSERVATION. THE AIRCRAFT EXECUTED A RIGHT TURN TO THE WEST, TRACKED BACK ACROSS THE AIRFIELD HEADING EAST, AND CLIMBED TO APPROXIMATELY 2,000 TO 3,000 FEET. AFTER VIEWING THE SUNRISE, THE PILOT INITIATED A TURN BACK TO THE WEST AND STARTED A DESCENT. THE PILOT REPORTS A COMPLETE LAPSE OF MEMORY (RETROGRADE AMNESIA) FROM THIS POINT OF DESCENT ONWARD. PILOT SUFFERED HEAD TRAMA DURING THE ACCIDENT AND A BROKEN ANKLE. NEIGHBOR SECURITY CAMERA FOOTAGE (AUDIO UNAVAILABLE) CAPTURED THE AIRCRAFT DESCENDING IN A CLEAN GLIDE PROFILE BEFORE IT IMPACTED A RESIDENTIAL STRUCTURE LOCATED ON THE EAST SIDE OF COVEY TRAILS AIRFIELD. POST-ACCIDENT EXAMINATION CONFIRMED FLIGHT CONTROL CONTINUITY FROM THE COCKPIT CONTROLS TO ALL RESPECTIVE FLIGHT CONTROL SURFACES. POWERPLANT / PROPELLER: THE TWO-BLADE WOOD PROPELLER AND METAL SPINNER EXHIBITED LITTLE TO NO ROTATION MARKS AND LACKED TORSIONAL DAMAGE FEATURES TYPICALLY CONSISTENT WITH AN ENGINE PRODUCING POWER AT THE TIME OF IMPACT. IMPACT SITE: THE AIRCRAFT STRUCK THE ROOF/STRUCTURE OF A RESIDENCE SITUATED ON THE EASTERN PERIMETER OF THE AIRPARK RESIDENTIAL COMMUNITY. PRELIMINARY ASSESSMENT PHYSICAL EVIDENCE—SPECIFICALLY THE LACK OF PROPELLER TORSIONAL DAMAGE COMBINED WITH VIDEO CONFIRMATION OF A CLEAN GLIDE PATH—STRONGLY INDICATES AN UNPOWERED FLIGHT PROFILE (ENGINE STARVATION, FAILURE, OR STOPPAGE) DURING THE FINAL MANEUVER BACK TOWARD THE AIRPORT ENVIRONMENT. INVESTIGATION IS ONGOING TO DETERMINE THE EXACT CAUSE OF POWER LOSS AND SUBSEQUENT LOSS OF CONTROL.

NTSB investigation

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