CHI90LA269
1990-09-22 · FORT WAYNE, Indiana, United States · None · 1 aircraft · Status: Completed
Airport FWA
Current FAA registration · N24296
- Make / Model
- CESSNA 152
- Year of manufacture
- 1977 · 13 years old at event
- Engine
- LYCOMING 0-235 SERIES (115 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19770811
- ADS-B equipped
- Yes — Mode-S A23B1F
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
THE FAILURE OF THE PILOT OF THE ACCIDENT AIRPLANE TO MAINTAIN SUFFICIENT SPEED FOR FLIGHT. THE PILOTS LACK OF TOTAL EXPERIENCE AND THE CROSSWINDS THAT WERE PRESENT DURING THE APPROACH AND THE ATTEMPTED GO-AROUND ARE CONTRIBUTING FACTORS TO THE ACCIDENT.
Factual narrative
THE STUDENT PILOT RELATES IN HIS STATEMENT THAT HE DID NOT FEEL COMFORTABLE WITH HIS APPROACH. HE DESCRIBES PROBLEMS WITH MAINTAINING RUNWAY ALIGNMENT BECAUSE OF CROSSWINDS. ACCORDING TO THE PILOT HE 'TRIED TO EXECUTE A GO-AROUND AND PUSHED IN THE THROTTLE. I DID NOT LOWER THE NOSE PROPERLY AND THE PLANE EVENTUALLY STALLED, DROPPING TO THE RUNWAY'. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1990_CHI90LA269.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, go-around). 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 …
- NASA NTRS 2025 · Conference Paper A Training Study to Improve Monitoring During A Go-Around
As part of an FAA program to improve go-around (GA) safety, we were asked to determine if we could improve the performance of the Pilot Monitoring (PM) during a GA maneuver.
- Flight Safety Foundation 2024 · FSF / AeroSafety World Go-Around Safety Forum Findings
Foundation Go-Around Safety Forum technical findings — examines why pilots fail to execute go-arounds when criteria are met (stabilized approach gate not met, energy state out of envelope, traffic con…
- 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…