CHI03LA008
2002-10-14 · Lake Elmo, Minnesota, United States · Minor · 1 aircraft · Status: Completed
Airport 21D
Aircraft involved
Probable cause & findings
The pilot's failure to maintain aircraft control. Factors to the accident included the gusting wind conditions and the encountered windshear, which resulted in the inadvertent stall at a low altitude and subsequent in-flight collision with the transmission wire and hangar.
Factual narrative
On October 14, 2002, at 1215 central daylight time, a Cessna 175B, piloted by a private pilot, was destroyed during an in-flight collision with power transmission lines and subsequent collision with a hangar at the Lake Elmo Airport (21D), St. Paul, Minnesota. Visual meteorological conditions prevailed at the time of the accident. The personal flight was operating under the provisions of 14 CFR Part 91 without a flight plan. The pilot sustained minor injuries. The flight departed the General Mitchell International Airport (MKE), Milwaukee, Wisconsin, at 1000. According to the pilot's written statement, he had attempted to land on runway 22 (2,497 feet by 75 feet, dry/asphalt) at 21D and elected to go-around prior to touchdown. The pilot reported flying "about 90 to 100 mph" during the go-around and when he turned downwind he "encountered a wind shear." The pilot stated the encounter with the wind shear "increased angle of attack" and the "airplane stalled." The pilot reported, "I tried to regain control, pulled power, hit power lines and airplane hangar." Gusting wind conditions were reported around the time of the accident, with a reported wind speed of 36 knots at 1218. While performing a go-around the airplane encountered windshear and stalled, impacting a power line and an airplane hangar. The pilot stated he had attempted to land on runway 22 and elected to go-around prior to touchdown. The pilot reported flying "about 90 to 100 mph" during the go-around and when he turned downwind he "encountered a wind shear." The pilot stated the encounter with the wind shear "increased angle of attack" and the "airplane stalled." The pilot reported, "I tried to regain control, pulled power, hit power lines and airplane hangar." Gusting wind conditions were reported around the time of the accident, with a reported wind speed of 36 knots at 1218. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2002_CHI03LA008.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
Matched on aircraft type or causal vocabulary (wind shear, stall, go-around). All research papers
- NASA NTRS 2019 · Conference Paper Optimal recovery from microburst wind shear
The flight path of a twin-jet transport aircraft is optimized in a microburst encounter during approach to landing. The objective is to execute an escape maneuver that maintains safe ground clearance …
- NASA NTRS 2013 · Conference Paper Optimal nonlinear estimation for aircraft flight control in wind shear
The most recent results in an ongoing research effort at Princeton in the area of flight dynamics in wind shear are described.
- 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.