DEN04CA062
2004-04-14 · Las Vegas, New Mexico, United States · None · 1 aircraft · Status: Completed
Airport LVS
N8956Q has since been reassigned. It is now registered to a different aircraft (BOEING 737-8, built 2025), which was not involved in this event.
Aircraft involved
Probable cause & findings
the pilot's decision to takeoff in wind conditions that consisted of a quarterly tailwind and a crosswind in excess of the maximum demonstrated crosswind component, and his failure to maintain directional control.
Factual narrative
On April 14, 2004, at approximately 1725 mountain daylight time, a Cessna 180A, N8956Q, was substantially damaged when it nosed over during takeoff roll at Las Vegas Municipal Airport, Las Vegas, New Mexico. The commercial pilot, the sole occupant on board, was not injured. Visual meteorological conditions prevailed. An instrument flight rules flight plan had been filed for the flight being conducted under the provisions of Title 14 CFR Part 91. The cross-country flight was originating at the time of the accident and was en route to Colorado Springs, Colorado. According to the pilot, during the take off roll from runway 14, a gust of wind weathervaned the tail of the airplane into the wind. Subsequently, the airplane nosed over, crushing the vertical stabilizer and rudder. The 1653 Las Vegas METAR (Aviation Routine Weather Report) reported winds from 260 degrees at 15 knots, gusting to 25 knots. At 1609, a peak wind from 270 degrees at 30 knots was recorded. According to the Cessna Pilot Operating Handbook, the maximum demonstrated crosswind component is 12 knots. The crosswind component was calculated to be a 12 to 31 knot tailwind. During the take off roll from runway 14, a gust of wind weathervaned the tail of the airplane into the wind. Subsequently, the airplane nosed over substantially damaging the airplane. The Aviation Routine Weather Report reported winds from 260 degrees at 15 knots, gusting to 25 knots. At 1609, a peak wind from 270 degrees at 30 knots was recorded. According to the Cessna Pilot Operating Handbook, the maximum demonstrated crosswind component is 12 knots. The crosswind component was calculated to be a 12 to 31 knot tailwind. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2004_DEN04CA062.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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