Aviation Accident Summaries

Aviation Accident Summary FTW96LA273

LONGMONT, CO, USA

Aircraft #1

N525V

WILLIAMS VELOCITY 173RG

Analysis

During takeoff, the aircraft failed to achieve sufficient airspeed and overran the departure end of runway 29. Density altitude at the time was 7,500 feet. The pilot said he was aware of a high density altitude, and had purposely serviced the airplane with a partial load of fuel. Also, he noted that he had no problem on takeoff from Hattiesburg, Mississippi (elevation 151 feet) or Wichita Falls, Texas (elevation 1,005 feet), and he expected no problem during this takeoff. No pre-accident/mechanical malfunction or failure was noted during the investigation.

Factual Information

On June 24, 1996, at 0930 mountain daylight time, an experimental home built Williams Velocity 173RG, N525V, registered to a private owner, exited the end of runway 29 onto soft ground during the takeoff roll at the Vance Brand Airport, Longmont, Colorado. The private pilot and the one passenger were not injured and the aircraft sustained substantial damage. The flight was operating under Title 14 CFR Part 91 when the accident occurred and no flight plan was filed. Visual meteorological conditions prevailed for this personal flight which was departing to Melbourne Beach, Florida, with the first en route stop planned at Salina, Kansas. According to the pilot, he was aware of the density altitude (7,500 feet) but said he had experienced no problems on takeoff from Hattiesburg, Mississippi, or Wichita Falls, Texas, on the trip to Colorado, from Florida, so he expected none on takeoff from Longmont. (Hattiesburg is 151 feet above sea level and Wichita Falls is 1,005 feet above sea level.) According to the Koch chart on altitude performance, given the conditions present at takeoff, the pilot would experience a takeoff run 130 percent longer than at sea level and climb performance would be degraded by 63 percent. No empirical data was provided by the manufacture of the kit airplane to assist the pilot in calculating takeoff and climb performance under non-standard conditions. The FAA currently does not require kit manufacturers to develop and distribute such information. The pilot stated that he was aware of density altitude and purposely had less than full fuel tanks on takeoff due to the high elevation of the airport. He reported that in the future he intended to confine his flying to airports 3,000 feet above mean sea level or less.

Probable Cause and Findings

the pilot's improper planning/decision. Factors relating to the accident were: the high density altitude, and the pilot's inadequate weather evaluation.

 

Source: NTSB Aviation Accident Database

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