MKC69F0249
1968-11-03 · STILWELL, Kansas, United States · Minor · 1 aircraft · Status: Completed
Aircraft involved
Historical record (pre-1982 coded fields)
- Aircraft
- CAMAIR 480 · N10600
- Damage
- Substantial
- Craft type
- Airplane
- Classification
- Accident
- Light condition
- Dusk
- Weather
- VMC
- Phase of flight
- D1
- Operator type
- Personal/private
- Airport
- VILLNAVE
- Kind of flying
- B0
Weather at impact
- Sky
- CLEAR
- Temp
- 42° F
Aircraft history
- Total time
- 1,255 hrs
Pilot
- Certificate
- Flight instructor (CFI)
- Total hours
- 1,150
- Age
- 30
Cause factors
- 64/C/32 C PILOT IN COMMAND MISMANAGEMENT OF FUEL Cause
- 88/C/96 C MISCELLANEOUS ACTS,CONDITIONS FUEL STARVATION Cause
- 88/C/48 C MISCELLANEOUS ACTS,CONDITIONS FAILURE OF TWO OR MORE ENGINES Cause
Decoded against the NTSB Form 6120.4 cause-factor codebook (ct_Pre1982 table).
Source: NTSB pre-1982 historical archive. Docket
3 3997.
Source file
NTSB_1968_3_3997.txt.
Modern CAROL record on
data.ntsb.gov ↗.
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Related research
Matched on aircraft type. All research papers
- NASA NTRS 2019 · Abstract Convective Weather Avoidance with Uncertain Weather Forecasts
Convective weather events have a disruptive impact on air traffic both in terminal area and in en-route airspaces. In order to make sure that the national air transportation system is safe and efficie…
- NASA NTRS 2019 · Conference Paper Constitutive modelling of single crystal and directionally solidified superalloys
The trend towards improved engine efficiency and durability places increasing demands on materials that operate in the hot section of the gas turbine engine.
- Embry-Riddle Scholarly Commons 2016 · Conference paper Late Afternoon Concurrent Sessions: GSIS Symposium: UAS Collaboration & Research Opportunities: Presentation: Adaptation of Forward Military Airspace Management Systems for Civilian UAS Emergency Services Operations
Potential use of unmanned aircraft system (UAS) to save lives, improve safety, and protect property has generated preliminary research in three major areas of the fire service, including aviation, str…
- NASA NTRS 2013 · Conference Paper Thermodynamic and fluid mechanic analysis of rapid pressurization in a dead-end tube
Three models have been applied to very rapid compression of oxygen in a dead-ended tube. Pressures as high as 41 MPa (6000 psi) leading to peak temperatures of 1400 K are predicted.