CHI04LA073
2004-02-18 · Memphis, Missouri, United States · None · 1 aircraft · Status: Completed
Airport 03D
Current FAA registration · N3419A
- Make / Model
- PIPER PA-22-135
- Year of manufacture
- 1953 · 51 years old at event
- Engine
- LYCOMING 0-290 SERIES (140 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19550924
- ADS-B equipped
- Yes — Mode-S A3C499
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
Directional control not maintained by the flight instructor during the landing roll. The snow on the edge of the runway, and the wind gusts were factors.
Factual narrative
On February 18, 2004, about 1400 central standard time, a Piper PA-22-135, N3419A, operated by a commercially rated flight instructor, sustained substantial damage on impact with a snow bank during landing roll at Memphis Memorial Airport (03D), Memphis, Missouri. The instructional flight was operated under 14 CFR Part 91. Visual meteorological conditions prevailed at the time of the accident. The flight instructor and student pilot sustained no injuries. No flight plan was on file. The flight originated from the Southeast Iowa Regional Airport (BRL) near Burlington, Iowa, about 1300, and was stopping at 03D for fuel en route to its final destination of Freeman Field Airport, near Junction City, Kansas. The Certified Flight Instructor (CFI) stated: We departed Burlington, Iowa at approximately 1300 hours enroute to Memphis, MO for refueling in order to make it back to Junction City, KS. The pilot that took us to Burlington was already on the ground at Memphis and stated that his landing was ok and he suggested runway 12, which concurred with the windsock. The winds aloft were strong and so my student pilot turned the aircraft over to me before short final. Upon descending to short final[,] the winds became light and so we landed, slightly right of the center line with very little aileron or rudder input. After rolling out for an unknown distance and before I could tell my student to start applying some light braking, a gust of wind hit the right side of the aircraft, lifting the right wing and pushing the tail to the left. The yoke was full aft and to the right and at that point I put in full left rudder to correct the direction of the roll out. The right wing became level but we were approximately 2 feet off the runway with the right main gear in the snow which had been pushed off the runway. At this point we were heading down the runway except for the right main gear which was still in the snow. Without brakes on the right side for assistance[,] we continued down the runway edge for approximately 40 feet before the right main gear either compacted with snow or hit some frozen snow making the aircraft tip forward [and] over on the windshield. To the south of the runway the terrain had some small hills, trees and farther south was a lake. The runway was in good shape. The pilot reported no mechanical malfunctions with the airplane. His safety recommendation was the installation of foot brakes on the right crew station to assist with directional control. At 1355, the recorded weather at Kirksville Regional Airport (IRK), approximately 26 nautical miles southwest of the accident airport, near Kirksville, Missouri, was: Wind 210 degrees at 18 knots gusting to 27 knots; visibility 10 statute miles; sky conditions clear; temperature 9 degrees C; dew point 1 degree C; altimeter 30.13 inches of mercury. Remarks: Peak winds 210 degrees at 28 knots at 1342. At 1353, the recorded weather at Ottumwa Industrial Airport (OTM), approximately 41 nautical miles north of the accident airport, near Ottumwa Iowa, was: Wind 220 degrees at 16 knots; visibility 7 statute miles; sky conditions clear; temperature 7 degrees C; dew point -1 degree C; altimeter 30.09 inches of mercury. The tailwheel airplane operated by a commercially rated flight instructor, sustained substantial damage on impact with a snow bank during landing roll during an instructional flight. The Certified Flight Instructor (CFI) stated, "Upon descending to short final[,] the winds became light and so we landed, slightly right of the center line with very little aileron or rudder input. After rolling out for an unknown distance and before I could tell my student to start applying some light braking, a gust of wind hit the right side of the aircraft, lifting the right wing and pushing the tail to the left. The yoke was full aft and to the right and at that point I put in full left rudder to correct the direction of the roll out. The right wing became level but we were approximately 2 feet off the runway with the right main gear in the snow which had been pushed off the runway. At this point we were heading down the runway except for the right main gear which was still in the snow. Without brakes on the right side for assistance[,] we continued down the runway edge for approximately 40 feet before the right main gear either compacted with snow or hit some frozen snow making the aircraft tip forward [and] over on the windshield." Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2004_CHI04LA073.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 ↗
- NTSB Docket Agency ↗
- Aviation Safety Network Aviation press ↗
- Kathryn's Report Aviation press ↗
- Aviation Herald Aviation press ↗
- AVweb Aviation press ↗
- Pilots of America Community ↗
- Reddit /r/flying Community ↗
- FlightAware Aviation press ↗
- AOPA accident database Aviation press ↗
- Google News News ↗
- DuckDuckGo News ↗
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…