NTSB CAROL · Event
Event CEN26LA030
Registry · N46CR
FAA Aircraft Registry record.
Make / Model
PIPER PA-46-310P
Year of manufacture
1986 · 39 years old at event
Engine
CONT MOTOR TSIO-520 SER (300 hp)
Seats / Engines
6 seats · 1 engine
Last airworthiness date
20000714
ADS-B equipped
Yes — Mode-S A59784
Registrant of record
BAS PART SALES LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
On October 26, 2025, about 918 mountain daylight time, a Piper PA46-310P, N46CR, was substantially damaged when it was involved in an accident near El Paso, Texas. The pilot and two passengers were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The pilot reported he was climbing to his enroute cruise altitude when the engine made a loud bang, followed by decreasing temperature readings and a low oil pressure warning. The pilot declared an emergency, requested vectors to the nearest airport, and performed the engine failure emergency checklist. The pilot assessed different landing options before deciding on a north-south dirt road. The airplane touched down about 500 feet before a steep incline in the road. The pilot applied heavy braking until he spotted a 3 foot hole in the road, at which time he released the brakes and applied full aft elevator. All three landing gear separated from the airplane as the airplane went into and past the hole in the road. The wings and fuselage were substantially damaged. Once the airplane came to rest, the pilot shut down the electrical systems and began evacuation of the occupants through the emergency exit. The main door had become blocked by a tree and some brush. Post accident examination of the airplane revealed a hole in the top of the crankcase by the number two cylinder. The magneto above the hole was dislodged from its mounting point. Clean looking oil was present on the dipstick. The airplane was retained for further examination. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2025_CEN26LA030.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (engine failure). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- arXiv 2022 · arXiv preprint
Multi-level Adaptation for Automatic Landing with Engine Failure under Turbulent Weather
This paper addresses efficient feasibility evaluation of possible emergency landing sites, online navigation, and path following for automatic landing under engine-out failure subject to turbulent wea…
- NASA NTRS 2019 · Conference Paper
Simulation of Liquid Rocket Engine Failure Propagation Using Self-Evolving Scenarios
Traditional probabilistic risk assessment approaches often require failure scenarios to be explicitly defined through event sequences that are then quantified as part of the integrated analysis.
- NASA NTRS 2019 · Conference Paper
Rocket engine failure detection using system identification techiques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Conference Paper
Rocket engine failure detection using system identification techniques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Technical Memorandum (TM)
A simulator investigation of engine failure compensation for powered-lift STOL aircraft
A piloted simulator investigation of various engine failure compensation concepts for powered-lift STOL aircraft was carried out at the Ames Research Center.
- Semantic Scholar 2019 · Article (AIAA Scitech 2019 Forum)
Impact of Engine Failure Constraints on the Initial Sizing of Hybrid-Electric GA Aircraft
Potential advantages of hybrid-electric aircraft are fuel savings, lower emissions, and reduced noise. Since these aircraft generally apply multiple power sources, they can also be designed to sustain…
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