MIA72FLD05
1971-08-01 · LAKE WALES, Florida, United States · None · 1 aircraft · Status: Completed
N233 has since been reassigned. It is now registered to a different aircraft (CESSNA 150H, built 1968), which was not involved in this event.
Aircraft involved
Historical record (pre-1982 coded fields)
- Aircraft
- CAMAIR 480 · N233
- Damage
- Substantial
- Craft type
- Airplane
- Classification
- Accident
- Light condition
- Dawn
- Weather
- VMC
- Phase of flight
- Cruise — descent (EF)
- Operator type
- D
- Airport
- LAKE WALES
- Kind of flying
- B0
Weather at impact
- Sky
- CLEAR
- Wind
- 250° / 10 kt
Aircraft history
- Serial number
- 00000001-069
- Total time
- 1,920 hrs
Pilot
- Certificate
- DA (DA)
- Age
- 44
Probable cause (from PRE1982.MDB)
ME BOLT HOLES EXCESSIVELY WORN.
Investigator remarks
NOSE GR ACTUATING CYL BOLT HOLES,AND SUPPORT FRA
Cause factors
- 70/A/CE A AIRFRAME NOSEWHEEL ASSEMBLIES Cause — pilot/personnel action
- 88/A/BP A MISCELLANEOUS ACTS,CONDITIONS ELONGATED Cause — pilot/personnel action
- 68/A/D6 A PERSONNEL INADEQUATE MAINTENANCE AND INSPECTION Cause — pilot/personnel action
- 88/J/AH J MISCELLANEOUS ACTS,CONDITIONS PREVIOUS DAMAGE Joint cause
Decoded against the NTSB Form 6120.4 cause-factor codebook (ct_Pre1982 table).
Source: NTSB pre-1982 historical archive. Docket
3 4508.
Source file
NTSB_1971_3_4508.txt.
Modern CAROL record on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
- TallyAero Live Wire Aviation press
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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.