CHI94LA228
1994-07-09 · OELWEIN, Iowa, United States · None · 1 aircraft · Status: Completed
Airport OLZ
Aircraft involved
Probable cause & findings
the pilot's decision to land on a runway with a tailwind. Factors associated with the accident were the tailwind and the wet runway.
Factual narrative
On July 9, 1994, at 1057 central daylight time, a Beech BE-58 airplane, N6404Z, sustained substantial damage when it departed the end of runway 13 while landing at the Oelwein Municipal Airport in Oelwein, Iowa. The private pilot and three passengers aboard sustained no injuries. The personal flight departed the Jeffco Airport in Denver, Colorado about 0700 mountain daylight time and was conducted under CFR Part 91. Visual meteorological conditions were reported at the accident airport and an IFR flight plan was filed. The pilot conducted the en route portion of the flight in instrument meteorological conditions. Descending through 3,000 feet he acquired visual meteorological conditions, cancelled IFR with Waterloo Approach Control, and proceeded to the Oelwein Municipal Airport under VFR. The pilot reported he had planned an instrument approach to runway 13. He attempted to obtain an airport advisory on the unicom frequency with no response. He said he used full flaps and landed on the wet runway with a tailwind. The automated weather observation system on the airport reported the winds were 290 degrees at 11 knots about the time of the accident. A standard wind sock and wind tee were located on the north side of the field. During a telephone interview, an employee of Connel Aviation, a local fixed-base operator (FBO), stated they were monitoring the unicom frequency and did not hear the request for an airport advisory. He said the aircraft landed long and it porpoised during the landing. An Officer from the Oelwein Police Department reported two skid marks on the runway, "from the airplanes landing gear", and estimated the length of the marks to be several hundred feet. He administered a preliminary breath test (PBT) to the pilot which yielded a result of .000. The pilot reported he flew in instrument meteorological conditions en route to the destination airport. He had planned an instrument approach to runway 13. Descending through 3,000 feet he encountered visual conditions, cancelled IFR, and flew a visual arrival to runway 13. He requested an airport advisory on the unicom frequency with no response. The pilot said he landed with a tailwind on the wet runway. Winds were from 290 degrees at 11 knots. A witness saw the airplane land long and porpoise during the landing. The airplane sustained substantial damage when it departed the runway. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1994_CHI94LA228.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. All research papers
- NASA NTRS 2011 · Conference Paper Joint thunderstorm operations using the NASA F-106B and FAATC/AFWAL Convair 580 airplanes
During the 1985 thunderstorm season, three joint thunderstorm research flights were conducted within 100 n.mi. of NASA Langley by the NASA Storm Hazards F-106B and the FAA/USAF CV-580 research airplan…
- NTSB Aircraft Accident Reports 2004 · Accident report In-Flight Separation of Vertical Stabilizer — American Airlines Flight 587
American Airlines 587 (A300-605R) Belle Harbor, NY, November 12, 2001 — 265 fatalities. Investigation of the post-takeoff in-flight breakup of American 587 over Belle Harbor.
- NASA NTRS 2024 · Presentation American Airlines Flight 587 Crash Investigation: NASA Langley Research Center Participation and Perspective
- NASA NTRS 2019 · Other Documentation for Three Wake Vortex Model Data Sets from Simulation of Flight 587 Wake Vortex Encounter Accident Case
This document contains a general description for data sets of a wake vortex system in a turbulent environment. The turbulence and thermal stratification of the environment are representative of the co…
- NASA NTRS 2016 · Conference Paper An overview of SAE ARP 1587: Aircraft gas turbine engine monitoring system guide
A systematic approach to developing an engine monitoring system (EMS) is outlined. An extensive shopping list of EMS capabilities and benefits are included.
- arXiv 2026 · arXiv preprint FESOM2-JAX v1.0: a differentiable shadow of the ocean-sea-ice model FESOM2, cast onto GPUs
We present FESOM2-JAX, a Python re-implementation of the Finite-volumE Sea ice-Ocean Model (FESOM2) in JAX. The model retains the unstructured-mesh, cell-vertex finite-volume formulation of the origin…