NTSB CAROL · Event
Event UNK64X1945
Registry · N10L
FAA Aircraft Registry record.
Make / Model
BEECH A36
Year of manufacture
1972
Engine
CONT MOTOR IO 520 SERIES (285 hp)
Seats / Engines
6 seats · 1 engine
ADS-B equipped
Yes — Mode-S A00355
Registrant of record
FIVE STATES HOLDINGS LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Historical record (pre-1982)
NTSB recorded this accident in the pre-1982 coded-field schema — structured fields rather than free-text narrative. Decoded codes use established NTSB single-letter taxonomies; cause factors remain verbatim pending the Form 6120.4 codebook lookup.
Aircraft
MINI MSTANG L1 · N10L
Damage
Destroyed
Craft type
Airplane
Classification
Accident
Light condition
Dawn
Weather
VMC
Phase of flight
D7
Operator type
D
Airport
WM J FOX
Kind of flying
B0
Aircraft history
Total time
122 hrs
Pilot
Certificate
F6 (F6)
Total hours
80,000
Age
466
Probable cause (from PRE1982.MDB)
IT
Investigator remarks
PILOT WORE PARACHUTE NO APPARENT ATTEMPT TO USE
Cause factors
- 64/A/09 A PILOT IN COMMAND EXCEEDED DESIGNED STRESS LIMITS OF AIRCRAFT Cause — pilot/personnel action
- 70/J/AA J AIRFRAME SPARS Joint cause
- 88/J/49 J MISCELLANEOUS ACTS,CONDITIONS SEPARATION IN FLIGHT Joint cause
- 88/J/94 J MISCELLANEOUS ACTS,CONDITIONS OVERLOAD FAILURE Joint cause
Decoded against the NTSB Form 6120.4 cause-factor codebook (ct_Pre1982 table). Each row shows the raw triplet, modifier (Cause / Factor / etc.), category, and specific code.
Source: NTSB pre-1982 historical archive. Docket
2 0313.
Source file
NTSB_1964_2_0313.txt.
Modern CAROL record 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. 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 2026 · arXiv preprint
Robust Adaptive MPC in the Presence of Nonlinear Time-Varying Uncertainties: An Uncertainty Compensation Approach
This paper introduces an uncertainty compensation-based robust adaptive model predictive control (MPC) framework for linear systems with nonlinear time-varying uncertainties.
- Semantic Scholar 2024 · Article (Volume 3A: Combustion, Fuels, and Emissions)
Considerations for Hydrogen Fueled Aerospace Gas Turbine Combustion Sub-System Design
As part of its commitment to the decarbonization of the aviation sector and the UN Race to Zero global campaign, Rolls-Royce is actively developing hydrogen combustion gas turbine engine technology ca…
- arXiv 2023 · arXiv preprint
From Propeller Damage Estimation and Adaptation to Fault Tolerant Control: Enhancing Quadrotor Resilience
Aerial robots are required to remain operational even in the event of system disturbances, damages, or failures to ensure resilient and robust task completion and safety.
- arXiv 2023 · arXiv preprint
Robust Adaptive MPC Using Uncertainty Compensation
This paper presents an uncertainty compensation-based robust adaptive model predictive control (MPC) framework for linear systems with both matched and unmatched nonlinear uncertainties subject to bot…
- arXiv 2022 · arXiv preprint
Integrated Adaptive Control and Reference Governors for Constrained Systems with State-Dependent Uncertainties
This paper presents an adaptive reference governor (RG) framework for a linear system with matched nonlinear uncertainties that can depend on both time and states, subject to both state and input cons…
- Embry-Riddle Scholarly Commons 2021 · Journal article (IJAAA)
Performance of the EGNOS system in Algeria for single and dual frequency
EGNOS (European Geostationary Navigation Overlay Service) transmits data for more accurate real time positioning with an integrity message for GNSS navigation satellites, which are in view by RIMS sta…
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