FTW01LA103
2001-04-22 · Bossier City, Louisiana, United States · Serious · 1 aircraft · Status: Completed
Airport BAD
Aircraft involved
Probable cause & findings
the pilot's failure to maintain control during the low level maneuver. A contribiting factor was the windshear.
Factual narrative
On April 22, 2001, at 1630 central daylight time, a Joe Underwood Lazer Z homebuilt experimental airplane, N363WB, registered to and operated by the pilot, was substantially damaged when it impacted terrain during an air show demonstration flight at the Barksdale Air Force Base, Bossier City, Louisiana. The commercial pilot, who was the sole occupant, sustained serious injuries. Visual meteorological conditions prevailed and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 aerobatic demonstration flight. During a telephone interview with the NTSB investigator-in-charge, the pilot reported that he had just completed an aerobatic maneuver and was flying wings level at 200 mph, approximately 10 feet AGL, down the "show" line on a heading of 150 degrees. He stated that he had established level flight for about 4 to 5 seconds when the aircraft was "suddenly and violently forced straight down until ground impact occured." After a "hard" bounce, the pilot immediately applied "up elevator" and "continued flying the aircraft." The pilot then shut the engine down and glided to a landing on runway 15. The pilot did not experience any "mechanical problems with the aircraft" and it "remained flyable and controllable following the ground impact." Inspection of the aircraft by a FAA airworthiness inspector revealed that both main landing gear were bent upward into the fuselage, which was buckled. After the accident, the pilot stated that he believed that the accident was "attributable to a severe wind shear and downdraft coming from a large hangar" located about 300 feet to the southwest of where the aircraft impacted the ground. The pilot reported the winds to be from 190 to 210 degrees at 25 knots, gusting to 35 knots. The homebuilt experimental airplane impacted terrain while performing a low pass during an air show demonstration flight. The pilot was flying wings level at 200 mph, approximately 10 feet AGL, down the "show" line on a heading of 150 degrees. Level flight was established for about 4 to 5 seconds when the aircraft was "suddenly and violently forced straight down until ground impact occured." After a "hard" bounce, the pilot immediately applied "up elevator" and "continued flying the aircraft." The pilot then shut the engine down and glided to a landing on an adjacent runway. The pilot did not experience any "mechanical problems with the aircraft" and it "remained flyable and controllable following the ground impact." The pilot stated that he believed that the accident was "attributable to a severe wind shear and downdraft coming from a large hangar" located about 300 feet to the southwest of where the aicraft impacted the ground. The pilot reported the winds to be from 190 to 210 degrees at 25 knots, gusting to 35 knots. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2001_FTW01LA103.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 (wind shear). 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 2019 · Contractor Report (CR) An Examination of Aviation Accidents Associated with Turbulence, Wind Shear and Thunderstorm
The focal point of the study reported here was the definition and examination of turbulence, wind shear and thunderstorm in relation to aviation accidents.
- NASA NTRS 2019 · Conference Paper Analysis of extreme wind shear
New methods utilizing extreme value statistical theory are applied in the analysis of the largest wind component shear in a wind profile as a function of shear layer thickness and season.
- NASA NTRS 2019 · Technical Memorandum (TM) Probabilities of zero wind shear phenomena based on Rawinsonde data records
Probabilities of zero wind shear occurence and depth based on rawinsonde data records
- NASA NTRS 2019 · Contractor Report (CR) A Wind Shear Mechanism for Producing Sporadic E by Concentrating Minor Meteoric Ions
Wind shear mechanism for producing sporadic E layer by concentrating minor meteoric ions
- NASA NTRS 2019 · Technical Memorandum (TM) Some aspects of wind shear in the upper atmosphere
Hydrodynamic turbulence and wind shear in upper atmosphere