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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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