ERA24LA007
2023-10-11 · Martinsville, Virginia, United States · None · 1 aircraft · Status: Completed
Airport MTV
Current FAA registration · N253BC
- Make / Model
- CIRRUS DESIGN SR22T
- Year of manufacture
- 2023 · 0 years old at event
- Engine
- CONT MOTOR TSIO-550-K (315 hp)
- Seats / Engines
- 5 seats · 1 engine
- Last airworthiness date
- 20230323
- ADS-B equipped
- Yes — Mode-S A262BF
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
On October 11, 2023, about 2130 eastern daylight time, a Cirrus SR-22, N253BC, was substantially damaged when it was involved in an accident near Martinsville, Virginia. The pilot and three passengers were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The pilot refueled the airplane, completed a preflight inspection, updated the airplane’s electronic flight instrument system, and departed Blue Ridge Airport (MTV), Martinsville, Virginia, for a night, visual flight rules cross-country flight to Oklahoma. The pilot reported that on takeoff, after he established a positive rate of climb at an airspeed of 95 kts, he retracted the flaps, which had been set to 50°. Shortly thereafter, he reported that the primary flight display blinked off momentarily and then reappeared with a “Taxiway! Taxiway!” banner. He looked at the multifunction flight display and noted that it was “completely orange” and appeared to depict an autopilot track turning directly left, which made him wonder if the autopilot was engaged. He further reported that it was “an extremely dark evening” and he “just happened to look up” and saw that the airplane was flying directly toward a large pine tree. He attempted to avoid the tree; however, the airplane struck trees to the left of the departure end of the runway. The pilot was able to maintain control of the airplane and the engine was developing full power as it continued to climb to the traffic pattern altitude. The pilot stated that the airplane was very “shaky,” and he was unable to see the altitude on the primary flight display. He was not certain if the autopilot was engaged, so he repeatedly pressed the autopilot disconnect button. He circled back toward MTV, trimmed the airplane for landing, and made a safe landing on runway 13, after which he immediately cleared the runway and shut off the engine. Examination of the airplane by a Federal Aviation Administration inspector revealed that the airplane sustained substantial damage to the wings. The inspector also observed that the pitch trim was set in the full nose-up position. The airplane was retained for further examination. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- — Personnel issues-Action/decision-Info processing/decision-Decision making/judgment-Pilot
- — Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Climb rate-Not attained/maintained
- — Personnel issues-Task performance-Planning/preparation-Weight/balance calculations-Pilot
- — Personnel issues-Psychological-Attention/monitoring-Task monitoring/vigilance-Pilot
Verbatim from NTSB's published report. Source file
NTSB_2023_ERA24LA007.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
Matched on aircraft type or causal vocabulary (autopilot). All research papers
- 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 2022 · arXiv preprint Experimental Flight Testing of a Fault-Tolerant Adaptive Autopilot for Fixed-Wing Aircraft
This paper presents an adaptive autopilot for fixed-wing aircraft and compares its performance with a fixed-gain autopilot.
- arXiv 2021 · arXiv preprint An Adaptive Digital Autopilot for Fixed-Wing Aircraft with Actuator Faults
This paper develops an adaptive digital autopilot for a fixed-wing aircraft and compares its performance with a fixed-gain autopilot.
- arXiv 2026 · arXiv preprint Robust Adaptive Sliding-Mode Control for Damaged Fixed-Wing UAVs
Many unmanned aerial vehicles (UAVs) can remain aerodynamically flyable after sustaining structural or control surface damage, yet insufficient robustness in conventional autopilots often leads to mis…