CHI83LA119
1983-02-22 · ELYRIA, Ohio, United States · None · 1 aircraft · Status: Completed
Airport 1G1
Current FAA registration · N72296
- Make / Model
- CESSNA 140
- Year of manufacture
- 1946 · 37 years old at event
- Engine
- CONT MOTOR C85 SERIES (85 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19560710
- ADS-B equipped
- Yes — Mode-S A9AEAC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
THE ACFT VEERED OFF THE LEFT SIDE OF RWY 27 AND NOSED OVER DURING LANDING. THIS WAS THE STUDENT PILOTS SECOND SUPERVISEDSOLO AND HIS THIRD LANDING TO A FULL STOP. THE WEATHER WAS VMC WITH THE WIND FROM 360 DEGREES AT 4 KTS. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1983_CHI83LA119.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
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Related research
Matched on aircraft type. All research papers
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The growth of ice stalagmites obtained by the solidification of impacting droplets on a cooled substrate ($-50^{\circ}$C to $-140^{\circ}$C) is investigated experimentally.
- NASA NTRS 2019 · Conference Paper Particulate Emissions Hazards Associated with Fueling Heat Engines
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- NASA NTRS 2016 · Conference Paper United Airlines LOFT training
Line oriented training is used in a broader, more generic sense that as a specific program under FAR 12.1409 and AC 120-35.
- Embry-Riddle Scholarly Commons 2016 · Conference paper Late Morning Concurrent Sessions: Innovations in Aviation Technologies: Presentation: Wingsuit Materials Research – The Effect of Currently Used Materials on Wingsuit Aerodynamics.
While wingsuit flight is exhilarating and one of the fastest growing facets of sport skydiving, current wingsuit performance is poor at best.
- 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.