ERA20CA095
2020-02-07 · Baltimore, Maryland, United States · None · 1 aircraft · Status: Completed
Airport BWI
Current FAA registration · N988FX
- Make / Model
- CESSNA 208B
- Year of manufacture
- 2012 · 8 years old at event
- Engine
- P&W CANADA PT6A-114A (675 hp)
- Seats / Engines
- 12 seats · 1 engine
- Last airworthiness date
- 20120926
- ADS-B equipped
- Yes — Mode-S ADC96F
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain clearance from the approach lights during an instrument approach.
Factual narrative
The pilot was conducting an instrument landing system approach in night instrument meteorological conditions to the destination airport. The pilot was utilizing the autopilot for the approach and disengaged it when he had the runway and airport lighting system in view. As he approached the runway, the pilot heard a sound and thought the airplane had hit a bird. He felt the airplane pitch up so he increased engine power and pitched down in order to reach the runway. After the pilot landed and taxied to the ramp, he saw that a large piece of an approach light was caught on the airplane's right main landing gear. Further inspection revealed that the airplane's empennage, right horizontal stabilizer, right wing strut, and front cargo pod were also damaged. The operator reported that the airplane had struck four separate approach light towers as well as a localizer antenna. The pilot was conducting an instrument landing system approach in night instrument meteorological conditions. The pilot was using the autopilot for the approach to the destination airport and disengaged it when he had the runway and airport lighting system in view. The pilot reported that, as he approached the runway, he heard a sound and thought the airplane had hit a bird. He felt the airplane pitch up, so he increased engine power and pitched down to reach the runway. After the pilot landed and taxied to the ramp, he saw that a large piece of an approach light was caught on the right main landing gear. Further examination revealed that the empennage, right horizontal stabilizer, right wing strut, and front cargo pod had sustained substantial damage. The operator reported that the airplane had struck four approach light towers and a localizer antenna. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Personnel issues-Psychological-Attention/monitoring-Monitoring environment-Pilot - C
- C Environmental issues-Physical environment-Object/animal/substance-Runway/taxi/approach light-Effect on operation - C
Verbatim from NTSB's published report. Source file
NTSB_2020_ERA20CA095.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
- NTSB Docket Agency ↗
- Aviation Safety Network Aviation press ↗
- Kathryn's Report Aviation press ↗
- Aviation Herald Aviation press ↗
- AVweb Aviation press ↗
- Pilots of America Community ↗
- Reddit /r/flying Community ↗
- FlightAware Aviation press ↗
- AOPA accident database Aviation press ↗
- Google News News ↗
- DuckDuckGo News ↗
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…