CEN23LA205
2023-05-29 · Larchwood, Iowa, United States · Serious · 1 aircraft · Status: Completed
Airport 2VA
Current FAA registration · N5038E
- Make / Model
- BELLANCA 8KCAB
- Year of manufacture
- 1979 · 44 years old at event
- Engine
- LYCOMING AEIO-320 SER (160 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19790126
- ADS-B equipped
- Yes — Mode-S A6488A
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot’s failure to maintain proper airspeed and his exceedance of the airplane’s critical angle of attack during initial climb after takeoff, which resulted in an aerodynamic stall and impact with the ground.
Factual narrative
On May 29, 2023, about 1330 central daylight time, a Bellanca 8KCAB airplane, N5038E, sustained substantial damage when it was involved in an accident near Larchwood, Iowa. The pilot sustained serious injuries and the passenger had minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The pilot reported that he did not recall anything about the accident. The passenger reported that his memory was vague but did recall taking off from the taxiway of a private airstrip (Larchwood-Zangger Vintage Airpark, 2VA). He recalled that he felt a little bit of a roller coaster sensation on the climb out. The airplane seemed to pitch up higher than normal, and then seemed to stall. He recalled that he heard the pilot say that they were stalling. He did not recall seeing the ground or impact with the ground. The pilot reported on the NTSB Form 6120 that there were no mechanical malfunctions or failures of the airplane. Examination of the accident site showed that the airplane impacted the ground about 700 ft to the left of the departure end of the paved taxiway. The front of the fuselage and both wings sustained substantial damage. Impact damage and low energy signatures were consistent with a stall. Examination of the flight controls revealed continuity from the cockpit to the rudder, ailerons, elevator, and elevator trim surfaces. Interruptions in the flight control continuity were attributed to impact damage. Fuel was present in the fuel lines and the carburetor bowl. The fuel tanks were breached, but first responders noted that fuel was leaking and the grass around the wreckage showed blight from fuel leakage. Examination of the engine revealed continuity throughout the drivetrain. Thumb compression was verified on all valves and cylinders. No pre-impact anomalies were found with the airframe, fuel, system, flight controls, or the engine. The passenger stated they were taking off from a paved taxiway at a private airstrip when the airplane pitched up higher than normal and stalled. He recalled that the pilot told him that they were stalling. The airplane descended and impacted the terrain adjacent to the taxiway. Impact signatures were consistent with a low-energy impact indicative of an aerodynamic stall. The fuselage and wings sustained substantial damage. The pilot reported that there were no mechanical malfunctions or failures of the airplane that would have precluded normal operation. Postaccident examination of the wreckage did not reveal any preimpact anomalies with the airframe, fuel, system, flight controls, or engine that would have resulted in the loss of control. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- — Personnel issues-Task performance-Use of equip/info-Use of equip/system-Pilot
- — Aircraft-Aircraft oper/perf/capability-Performance/control parameters-(general)-Not attained/maintained
Verbatim from NTSB's published report. Source file
NTSB_2023_CEN23LA205.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
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Related research
Matched on aircraft type or causal vocabulary (stall, loss of control). All research papers
- Semantic Scholar 2016 · Article (Interacción) Trajectory Recovery System: Angle of Attack Guidance for Inflight Loss of Control
This paper describes the design and development of an ecological display to aid pilots in the recovery of an In-Flight Loss of Control event due to a Stall (ILOC-S).
- NTSB Aircraft Accident Reports 2010 · Accident report Loss of Control on Approach — Colgan Air Flight 3407
Colgan Air 3407 / Continental Connection (Q400) Buffalo NY, February 12, 2009 — 50 fatalities. Definitive investigation of the Colgan 3407 stall-stick-pusher crash on approach to Buffalo.
- 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 …
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER) A Scoping Review of Aviation Loss of Control Inflight Research
Loss of control – inflight (LOC-I) contributes to aircraft accidents at unacceptably high rates. Significant industry efforts and research have aimed to improve LOC-I prevention, detection, and recove…
- SKYbrary (Eurocontrol) 2024 · SKYbrary article Loss of Control In-Flight (LOC-I) — SKYbrary Knowledge Base
SKYbrary comprehensive knowledge-base entry on Loss of Control In-Flight — definitions, contributing factors, accident case studies (Air France 447, Colgan 3407), and prevention strategies.
- Semantic Scholar 2024 · Article (International Conference on Networking and Services) Risk Assessment of Loss of Control In-Flight Trajectories for Urban Air Mobility Safety
In Urban Air Mobility (UAM), maintaining a minimum separation between aircraft is a safety requirement, which becomes challenging amidst congested air traffic and off-nominal conditions, such as Loss …