NTSB CAROL · Event
Event MKC67D0123
Registry · N8775M
FAA Aircraft Registry record.
Make / Model
BEECH A23
Engine
CONT MOTOR IO-346 SERIES (165 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19641016
ADS-B equipped
Yes — Mode-S AC136A
Registrant of record
RIO AVIATION 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
BEECH A23 · N8775M
Damage
Substantial
Craft type
Airplane
Classification
Accident
Light condition
Dawn
Weather
VMC
Phase of flight
D0
Operator type
Personal/private
Kind of flying
A0
Weather at impact
Sky
CLEAR
Wind
240° / 13 kt
Temp
90° F
Aircraft history
Total time
930 hrs
Pilot
Certificate
Flight instructor (CFI)
Total hours
800
Age
20
Investigator remarks
SIMULATED FORCED LANDING.
Cause factors
- 74/C/KA C POWERPLANT POWERPLANT FAILURE FOR UNDETERMINED REASONS Cause
- 88/L/85 L MISCELLANEOUS ACTS,CONDITIONS SIMULATED CONDITIONS
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
3 3115.
Source file
NTSB_1966_3_3115.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 2023 · arXiv preprint
Large-eddy simulations of the NACA23012 airfoil with laser-scanned ice shapes
In this study, five ice shapes generated at NASA Glenn's Icing Research Tunnel (IRT) are simulated at multiple angles of attack (Broeren et al., J. of Aircraft, 2018).
- arXiv 2025 · arXiv preprint
Transonic buffet and incompressible low-frequency oscillations at high Reynolds numbers
Coherent, self-sustained oscillations of the flow over aircraft wings can lead to unsteady loads that detrimentally affect aircraft safety and stability, thus limiting the flight envelope.
Browse the full corpus — academia portal ↗