CHI03LA007
2002-10-09 · Forest Lake, Minnesota, United States · None · 1 aircraft · Status: Completed
Airport 25D
N21WL has since been reassigned. It is now registered to a different aircraft (PILATUS AIRCRAFT LTD PC-12/47E, built 2022), which was not involved in this event.
Aircraft involved
Probable cause & findings
The loss of engine power for undetermined reasons. A related factor was the swampy terrain.
Factual narrative
On October 9, 2002, at 1730 central daylight time, an amateur built Madewell EAA-Biplane-P, N21WL, sustained substantial damage during a forced landing to a swamp after a loss of engine power. The private pilot was not injured. The Title 14 CFR Part 91 flight departed Forest Lake Airport (25D), Forest Lake, Minnesota, at 1705 on a local flight. Visual meteorological conditions prevailed and no flight plan was filed. The pilot reported he had been practicing power on and power off stalls north of the airport. He returned to 25D and flew over the airport at 2,500 feet msl (1,575 feet agl) to check for two aircraft that were in the traffic pattern. He reported that when he was southwest of the approach end of runway 13 (2,650 feet by 150 feet, turf), he lost power to the engine and immediately turned right to land on runway 13. The pilot reported that he could not make the runway and executed a forced landing to a swamp. The pilot reported that he had switched the fuel selector from the 9 gallon fuel tank to the 12 gallon fuel tank about 7 miles prior to the loss of engine power. The pilot reported that during his preflight inspection, he did not sump the tanks individually for contamination, but he did sump the fuel scupper drain once to check for contamination. He reported that he had drained and fueled the 12 gallon tank with about 6 gallons of 100 LL Avgas twice about 2 weeks earlier when he purchased the airplane. He reported he had topped off the 12 gallon tank with 100 LL Avgas about two times since purchasing the airplane. A Federal Aviation Administration Airworthiness Inspector conducted a post-accident examination of the airplane. He reported the engine exhibited continuity and thumb compression. He reported, "The fuel line was wrapped with foam and aluminum speed tape to prevent vapor lock." The inspection of the airframe and engine revealed no pre-impact anomalies. The airplane sustained substantial damage during a forced landing to a swamp after a loss of engine power. The pilot reported he had been practicing power on and power off stalls north of the airport prior to returning to the airport. He over flew the airport about 1,575 feet agl to check for two aircraft that were in the traffic pattern. When he was southwest of the approach end of runway 13, he lost power to the engine and immediately turned right to land on runway 13. The pilot reported that he could not make the runway and executed a forced landing to a swamp. An inspection of the airframe and engine revealed no pre-impact anomalies. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2002_CHI03LA007.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 (icing, stall). All research papers
- 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 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…
- NASA NTRS 2019 · Contractor Report (CR) An Evaluation of an Analytical Simulation of an Airplane with Tailplane Icing by Comparison to Flight Data
This report presents the assessment of an analytical tool developed as part of the NASA/FAA Tailplane Icing Program. The analytical tool is a specialized simulation program called TAILSM4 which was de…
- NASA NTRS 2019 · Technical Publication (TP) NASA/FAA Tailplane Icing Program: Flight Test Report
This report presents results from research flights that explored the characteristics of an ice-contaminated tailplane using various simulated ice shapes attached to the leading edge of the horizontal …
- NASA NTRS 2019 · Other [Tail Plane Icing]
The Aviation Safety Program initiated by NASA in 1997 has put greater emphasis in safety related research activities. Ice-contaminated-tailplane stall (ICTS) has been identified by the NASA Lewis Icin…
- Embry-Riddle Scholarly Commons 2019 · Journal article (IJAAA) Airport Policing in Pakistan: Structure, Training, and Issue
Airports are strategically and economically important installations of any country. Airports are the gateway of any country and any incidents at these gateways may harm the very aspects of a country i…