DEN00LA162
2000-09-03 · LARAMIE, Wyoming, United States · Minor · 1 aircraft · Status: Completed
Airport LAR
Current FAA registration · N63FE
- Make / Model
- AVIAT INC A-1
- Year of manufacture
- 1992 · 8 years old at event
- Engine
- LYCOMING O&VO-360 SER (180 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19920819
- ADS-B equipped
- Yes — Mode-S A83BE5
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain directional control. A factor was his improper inflight decision in selecting a less-than-favorable runway on which to land that resulted in a ground loop.
Factual narrative
On September 3, 2000, approximately 1200 mountain daylight time, an Aviat A-1, N63FE, registered to and operated by the pilot, was substantially damaged when it collided with terrain while landing at Laramie Regional Airport, Laramie, Wyoming. The private pilot and sole occupant received minor injuries. Visual meteorological conditions prevailed, and no flight plan had been filed for the personal flight being conducted under Title 14 CFR Part 91. The flight originated at Jackson, Wyoming, approximately 0900. The pilot stated that he was attempting a landing on runway 30 with a left crosswind. Recorded wind was 200 degrees at 14 knots. The pilot said he lost control and the airplane "ground looped and tipped upside down." The airplane came to a rest in the center of the runway. According to Aviat Aircraft, Inc., the A-1's maximum demonstrated crosswind component is 15 mph (13 knots). Consulting the Crosswind Component Chart, it was determined that the pilot was attempting to land with an almost direct left crosswind (10 degree left quartering tailwind). These circumstances provided a tailwind component of 2 knots and a crosswind component of 13 knots, less than the maximum crosswind component specified by the manufacturer. In addition to runways 12-30, Laramie Regional Airport has a second, and longer, runway: 03-21. Landing on runway 21 would have presented a 10 degree left crosswind, and would have provided a 13 knot headwind component and a 2 knot crosswind component (see Crosswind Component Chart). The pilot was attempting to land on runway 30. Recorded wind was 200 degrees at 14 knots. Directional control was lost and the airplane 'ground looped and tipped upside down.' According to Aviat Aircraft, Inc., the A-1's maximum demonstrated crosswind component is 15 mph (13 knots). Consulting the Crosswind Component Chart, it was determined that the pilot was confronted with an almost direct left crosswind (10 degree left quartering tailwind). Under these circumstances, there was a tailwind component of 2 knots and a crosswind component of 13 knots, less than the maximum crosswind component specified by the manufacturer. In addition to runways 12-30, the airport has a second, and longer, runway: 03-21. Landing on runway 21 would have presented a 10 degree left crosswind, and would have provided a 13 knot headwind component and a 2 knot crosswind component. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2000_DEN00LA162.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. All research papers
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- Embry-Riddle Scholarly Commons 2022 · Faculty research project PLD Space Suborbital Microgravity Research
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- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER) Can Backward-Chained, Ab-Initio Pilot Training Decrease Time to First Solo?
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- Embry-Riddle Scholarly Commons 2020 · Conference paper Backwards Chaining – Accelerating Solo Flight Training
Flight simulation has made progressively significant inroads into pilot training at all levels of a pilot’s career – typically starting with training for the Instrument rating in light aircraft and co…
- NASA NTRS 2019 · Conference Paper Transonic Experimental Observations of Abrupt Wing Stall on an F/A-l8E Model
A transonic wind tunnel test of an 8% F/A-18E model was conducted in the NASA Langley Research Center (LaRC) 16 ft Transonic Tunnel (16-ft TT) to investigate on-surface flow physics during stall.
- Embry-Riddle Scholarly Commons 2018 · Conference paper Implementing Immersive Virtual Reality in an Aviation/Aerospace Teaching and Learning Paradigm
The ubiquity of computing technology has revolutionized the workplace and has also had a significant impact on education. The use of interactive simulations based on virtual reality (VR), augmented re…