CHI92LA050
1991-12-10 · MINNEAPOLIS, Minnesota, United States · None · 1 aircraft · Status: Completed
Airport FCM
Current FAA registration · N72625
- Make / Model
- CESSNA 140
- Year of manufacture
- 1946 · 45 years old at event
- Engine
- CONT MOTOR C90 SERIES (95 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19551230
- ADS-B equipped
- Yes — Mode-S A9BC92
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
REMEDIAL ACTION WAS NOT PERFORMED BY THE CFI. A FACTOR RELATED TO THE ACCIDENT WAS DIRECTIONAL CONTROL WAS NOT MAINTAINED BY THE STUDENT PILOT.
Factual narrative
THE CFI PILOT SAID THAT THE STUDENT PILOT LOST DIRECTIONAL CONTROL DURING THE LANDING ROLL OUT AND OVER APPLIED THE BRAKES. THE AIRCRAFT SWERVED OFF THE RUNWAY AND NOSED OVER. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1991_CHI92LA050.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.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
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Related research
Matched on aircraft type. All research papers
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- 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.