NTSB CAROL · Event
Event DEN77DTE65
Registry · N1130B
FAA Aircraft Registry record.
Make / Model
DASSAULT AVIATION FALCON 900EX
Year of manufacture
2014
Engine
HONEYWELL TFE731-60-1C
Seats / Engines
21 seats · 3 engines
Last airworthiness date
20150925
ADS-B equipped
Yes — Mode-S A039B2
Registrant of record
MJB TRI-MOTOR 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
LUSCOMBE 8E · N1130B
Damage
Substantial
Craft type
Airplane
Classification
Accident
Light condition
Dawn
Weather
VMC
Phase of flight
EE
Operator type
D
Airport
MEADOWLAKE
Kind of flying
A3
Weather at impact
Sky
CLEAR
Wind
270° / 7 kt
Aircraft history
Serial number
000000005757
Total time
1,345 hrs
Pilot
Certificate
Airline transport
Total hours
20
Age
23
Investigator remarks
PILOT TRIED TO STRETCH GLIDE.
Cause factors
- 64/A/25 A PILOT IN COMMAND IMPROPER LEVEL OFF Cause — pilot/personnel action
- 88/A/22 A MISCELLANEOUS ACTS,CONDITIONS POORLY PLANNED APPROACH Cause — pilot/personnel action
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 2062.
Source file
NTSB_1977_3_2062.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.
- NASA NTRS 2019 · Conference Paper
Transonic Experimental Observations of Abrupt Wing Stall on an F/A-l8E Model
A transonic wind tunnel test of an 8% F/A-18E model was conducted in the NASA Langley Research Center (LaRC) 16 ft Transonic Tunnel (16-ft TT) to investigate on-surface flow physics during stall.
- NASA NTRS 2019 · Conference Paper
Transonic Experimental Observations of Abrupt Wing Stall on an F/A-18E Model (Invited)
A transonic wind tunnel test of an 8% F/A-18E model was conducted in the NASA Langley Research Center (LaRC) 16 ft Transonic Tunnel (16-ft TT) to investigate on-surface flow physics during stall.
Browse the full corpus — academia portal ↗