CHI92LA235
1992-08-08 · ST. PAUL, Minnesota, United States · None · 1 aircraft · Status: Completed
Airport STP
Current FAA registration · N55982
- Make / Model
- BOEING A75N1(PT17)
- Engine
- P&W R-985 SERIES (450 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19700715
- ADS-B equipped
- Yes — Mode-S A72465
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
THE PILOT'S INATTENTIVENESS AND IMPROPER USE OF THE AIRPLANES BRAKES. A FACTOR WHICH CONTRIBUTED TO THIS ACCIDENT WAS THE INCORRECT BRAKE SYSTEM INSTALLED ON THE AIRPLANE.
Factual narrative
THE FORMER WORLD WAR II BI-PLANE TRAINER HAD MADE A WHEEL LANDING ON THE HARD SURFACED RUNWAY. THE PILOT STATED THE AIRPLANE YAWED TO THE LEFT DUE TO A LIGHT LEFTHAND CROSSWIND. HE STATED HE APPLIED SOME RIGHT RUDDER TO COMPENSATE FOR THE YAW. SHORTLY AFTER RIGHT RUDDER APPLICATION THE AIRPLANE NOSED OVER INVERTED ONTO THE RUNWAY. THE PILOT STATED HE HAS MADE HUNDREDS OF LANDINGS IN THE AIRPLANE AND STATED IT'S AN '...AIRPLANE YOU CANNOT RELAX WITH ON LANDINGS.' ACCORDING TO THE PILOT, THE AIRPLANE WAS EQUIPPED WITH LARGER WHEELS AND BRAKES. THE LARGER WHEELS AND BRAKES ARE NORMALLY FOUND ON ANOTHER WORLD WAR II TRAINING AIRPLANE THAT WEIGHS APPROXIMATELY 1330 POUNDS MORE THAN THE ACCIDENT AIRPLANE. THE FEDERAL AVIATION ADMINISTRATION (FAA) AIRCRAFT RECORDS BRANCH DID NOT LOCATE A RECORD OF AN FAA FORM 337 FOR THIS INSTALLATION. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1992_CHI92LA235.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 or causal vocabulary (stall). All research papers
- NASA NTRS 2026 · Conference Paper Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- arXiv 2023 · arXiv preprint Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- arXiv 2023 · arXiv preprint Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2023 · arXiv preprint Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
- arXiv 2022 · arXiv preprint Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER) Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…