Piper PA-24-250 accident near Tyler, Texas, January 15, 2025
On January 15, 2025 at about 10:30 pm local time, a Piper PA-24-250, registered N8051P, was substantially damaged in an accident during initial climb near Tyler, Texas (Tyler Pounds Rgnl airport). It was a personal flight under general aviation rules (Part 91). No one was hurt; 3 people were on board or involved. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
An electrical system surge for a reason that could not be determined that resulted in an overvoltage event, internal damage to electronics equipment, smoke in the cockpit, and a gear up landing.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- January 15, 2025 · about 10:30 pm local time
- Place
- Tyler, Texas · Tyler Pounds Rgnl · map
- Type
- Accident
- Injuries
- No one was hurt; 3 people were on board or involved.
- Weather
- visual conditions (good weather)
- Aircraft
- Piper PA-24-250 · all PA-24-250s on the register
- Registration
- N8051P · registry record · serial 24-3297
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The pilot reported that just before the accident flight, the airplane’s battery was not charged, and the airplane was connected to a truck using jumper cables to start the engine. The pilot then proceeded with the flight and shortly after departure he noted sparks and smoke emanating from behind the instrument panel. He turned off the generator and the sparking stopped. He turned the electrical power back on a few times to notify air traffic control and to attempt to lower the landing gear. He believed that the landing gear was down and locked based on position of the gear itself and by noting the position of the emergency extension handle, but upon landing the airplane’s landing gear collapsed which resulted in substantial damage to the fuselage. The pilot noted that before the landing he did not physically grab the emergency landing gear extension handle to verify that it was fully forward (down and locked). Postaccident examination of the airplane by a mechanic revealed several marked and unmarked circuit breakers that were tripped. Testing of those circuits revealed that resetting the breakers and applying power to the aircraft electrical system resulted in the breakers tripping again. Further testing revealed that removal of the protected devices resulted in some of the protected circuits drawing excessive current and continuing to trip while others showed no further current draw and did not trip. It was found that many of the devices removed had internal damage and excessive current draw. One item tested, the Garmin GMA340 Audio Panel, would produce smoke from the rear of the unit when power was applied and the smoke continued for several seconds after power was removed. The mechanic did not test the airplane’s generator or voltage regulator. Investigators were unable to test the generator or voltage regulator as the wreckage was disposed of before the testing could take place. Based on the postaccident testing, the smoke reported by the pilot was likely from the internally compromised audio panel. The internal damage to the audio panel and other avionics components was consistent with a power surge due to a faulty voltage regulator, but since the generator and voltage regulator were not tested the definitive reason could not be determined. During the event the pilot attempted to lower the landing gear, and he believed it was down but the collapse upon landing is consistent with it not having reached the fully down and locked position.
The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.
The factual record from the NTSB's investigation tables, in plain English
What happened, in order
- Electrical system malf/failure during initial climb defining event
The NTSB's findings
- Aircraft › Aircraft systems › Electrical power system › DC generation system › Unknown/Not determined
- Personnel issues › Action/decision › Action › Incomplete action › Pilot
- Aircraft › Aircraft systems › Landing gear system › Gear extension and retract sys › Not used/operated
Pilot
- Certificate: private
- Ratings: single-engine land
- Flight time: 376 hours in all; 308 in this make and model; 39 in the last 90 days; 9 in the last 30 days; 227 as pilot in command; 0 on instruments
- Medical certificate: Class 3 (without waivers/limitations)
- Seat: left
- Injury: no injuries
The aircraft
- Airframe total time: 4,831 hours
- Last inspection: annual inspection, August 1, 2024; 40 hours since
- Maximum gross weight: 2,800 lb
- Seats: 4
- Landing gear: retractable
- Engine: Lycoming IO-540-A1A5 (piston); 4,831 hours total
The flight
- Destination: FTW Fort Worth TX
- Flight plan: none
- Runway 04/2, 8,334 ft by 150 ft
Weather at the time
- Light: daylight
- Wind: from 350° at 6 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 61°F (16°C), dew point 27°F (-3°C)
- Altimeter: 30.37 inHg
- Observation at 4:53 pm from KTYR
Weather report (METAR): METAR KTYR 152253Z 35006KT 10SM CLR 16/M03 A3037 RMK AO2 SLP281 T01611028=
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 | |||
| Passengers | 2 |
Photographs from the investigation 2 pictures from the NTSB's docket, as the NTSB released them
The NTSB's photographs with the NTSB's captions, at screen size. Open a picture to see it full size or to report one that should not be shown.
Documents from the investigation the NTSB's docket: the evidence folder behind the report
6 documents, released by the NTSB on August 19, 2026. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.
| # | Document | What it is | |
|---|---|---|---|
| 1 | Propeller Logbook | PDF, 3 pages | View Download |
| 2 | Engine Logbook | PDF, 5 pages | View Download |
| 3 | Airframe Logbook | PDF, 8 pages | View Download |
| 4 | Pilot/operator Aircraft Accident Report, NTSB Form 6120.1 | PDF, 10 pages | View Download |
| 5 | Accident Photographs | PDF, 3 pages · our copy | View Download |
| 6 | Postaccident Examination Summary from Mechanic | PDF, 2 pages | View Download |
The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.
Other NTSB records under N8051P the same tail number, which may have belonged to a different aircraft at the time
Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.


