NTSB CAROL · Event
Event WPR25LA111
Registry · N711HE
FAA Aircraft Registry record.
Make / Model
CESSNA P210N
Year of manufacture
1979 · 46 years old at event
Engine
CONT MOTOR TSIO-520 SER (300 hp)
Seats / Engines
6 seats · 1 engine
Last airworthiness date
20200624
ADS-B equipped
Yes — Mode-S A98078
Registrant of record
DESERT WEST ENTERPISES LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
On March 11, 2025, at 1340 mountain daylight time, a Cessna P210N, N711HE, was substantially damaged when it was involved in an accident near Roswell, New Mexico. The pilot and passenger were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. According to the pilot, he departed Roswell Air Center Airport (ROW), Roswell, New Mexico, for a cross-country flight. While climbing through about 11,000 ft mean sea level, a warning for cylinder head temperature appeared on the primary flight display (PFD) and the pilot recognized that the fuel flow was lower that expected. A short time later a “low bus voltage” message appeared on the multifunction flight display (MFD). The pilot notified the Air Traffic Control Tower at ROW that he would be returning to the airport and started descent towards the airport. The pilot disconnected the autopilot and noted the electric trim did not appear to be working. He tried turning the trim wheel and felt resistance. The PFDs and MFD lost power during the descent and the pilot said he was “fighting the elevator control” and the airplane was descending about 2,000 ft per minute. He also stated he activated the landing gear selector, but the warning horn and gear position indicator lights were not operating. He did not visually confirm the position of the landing gear prior to landing and stated he thought the gear may have been “hanging” when he landed on runway 17. The landing gear subsequently collapsed, and the airplane slid off the right side of the runway which resulted in substantial damage to the empennage. The airplane had a new alternator installed about 10 hours of flight time prior to the accident. The airplane was retained for examination. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2025_WPR25LA111.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 (stall, autopilot). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- NASA NTRS 2026 · Conference Paper
Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- arXiv 2025 · arXiv preprint
ROSflight 2.0: Lean ROS 2-Based Autopilot for Unmanned Aerial Vehicles
ROSflight is a lean, open-source autopilot ecosystem for unmanned aerial vehicles (UAVs). Designed by researchers for researchers, it is built to lower the barrier to entry to UAV research and acceler…
- arXiv 2025 · arXiv preprint
ROSplane 2.0: A Fixed-Wing Autopilot for Research
Unmanned aerial vehicle (UAV) research requires the integration of cutting-edge technology into existing autopilot frameworks.
- arXiv 2024 · arXiv preprint
A Data-Driven Autopilot for Fixed-Wing Aircraft Based on Model Predictive Control
Autopilots for fixed-wing aircraft are typically designed based on linearized aerodynamic models consisting of stability and control derivatives obtained from wind-tunnel testing.
- arXiv 2023 · arXiv preprint
Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- arXiv 2023 · arXiv preprint
Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
Browse the full corpus — academia portal ↗