NTSB CAROL · Event
Event MKC67D0312
Registry · N7912L
FAA Aircraft Registry record.
Make / Model
BEECH A23-19
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19660826
ADS-B equipped
Yes — Mode-S AABE65
Registrant of record
MILLER CAMERON
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 · N7912L
Damage
Substantial
Craft type
Airplane
Classification
Accident
Light condition
Dawn
Weather
VMC
Phase of flight
EB
Operator type
D
Kind of flying
B0
Weather at impact
Sky
CLEAR
Wind
180° / 5 kt
Temp
60° F
Aircraft history
Total time
133 hrs
Pilot
Certificate
Commercial — instrument
Total hours
566
Age
46
Investigator remarks
PILOT PRACTICING SIMULATED FORCED LANDING.
Cause factors
- 64/A/48 A PILOT IN COMMAND MISJUDGED DISTANCE AND ALTITUDE Cause — pilot/personnel action
- 88/J/85 J MISCELLANEOUS ACTS,CONDITIONS SIMULATED CONDITIONS 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
3 3840.
Source file
NTSB_1966_3_3840.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 ↗