NTSB CAROL · Event
Event LAX77FUG26
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 · N72033
Damage
Destroyed
Craft type
Airplane
Classification
Accident
Light condition
E
Weather
VMC
Phase of flight
EB
Operator type
D
Airport
DAGGETT-BARSTOW
Kind of flying
B0
Weather at impact
Sky
CLEAR
Aircraft history
Serial number
000000003460
Total time
705 hrs
Pilot
Certificate
GA (GA)
Total hours
5,500
Age
38
Investigator remarks
HIT HIGH WIRES.
Cause factors
- 64/C/32 C PILOT IN COMMAND MISMANAGEMENT OF FUEL Cause
- 64/C/29 C PILOT IN COMMAND INADEQUATE PREFLIGHT PREPARATION AND/OR PLANNING Cause
- 88/C/63 C MISCELLANEOUS ACTS,CONDITIONS FUEL EXHAUSTION Cause
- 83/K/I K TERRAIN HIGH OBSTRUCTIONS Joint factor
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 0035.
Source file
NTSB_1977_3_0035.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 ↗