Casualties unknown

Cessna 172RG Forced Landing on Mountain After Encountering Downdraft (N401TA)

Gunnison, CO, US

On July 28, 2001, a Cessna 172RG (registration N401TA) was involved in an aviation accident near Gunnison, CO. Investigators recorded the probable cause as: the pilot's failure to attain the proper climb rate, and his improper inflight planning/decision to attempt to cross mountainous terrain at an inadequate altitude. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-07-04Data APIEditorial standards

After takeoff, a Cessna 172RG encountered severe updraft and downdraft while attempting to cross mountains. The pilot executed a gear-up landing on a mountainside. The aircraft was overweight and climb performance was insufficient.

Accident Details

The pilot reported that after takeoff, he climbed to 9,700 feet mean sea level (msl) to cross the mountains. The airplane then encountered a "300 foot updraft, and then a 2,000 foot downdraft." The pilot decided to "land the plane without the use of the landing gear on the side of the mountain."

Passenger Account

One passenger noted that it was the pilot's first mountain flying experience. The passenger recalled the airplane was at 80 knots and 8,300 feet as they approached a mountain. The pilot pulled back on the control yoke in an attempt to gain sufficient altitude to clear the peak, but the airplane responded slowly, and the passenger stated, "we literally came straight down" and "the belly [struck the ground] pretty hard."

Site and Performance Data

Rescue personnel reported the accident site elevation at 8,510 feet. The straight-line distance from the departure airport to the accident site was 9 nautical miles (nm). The difference in elevation between the accident site and the airport (8,510 - 7,673 feet) was 837 feet. The computed climb rate was 93 feet per nm. The estimated airplane weight at takeoff was 2,670 pounds, exceeding the maximum certificated gross weight of 2,650 pounds. The altimeter setting was 30.49 inches of mercury, with a computed pressure altitude of 7,103 feet msl. Referring to the Cessna 172RG Maximum Rate of Climb chart, the airplane was capable of a climb rate of 464 feet per minute (fpm) and, at a climb speed of 79 knots, a climb gradient of 352.4 feet per nm.

Frequently asked questions

What happened in the 28 Jul 2001 Cessna 172RG accident near Gunnison, CO?

After takeoff, a Cessna 172RG encountered severe updraft and downdraft while attempting to cross mountains. The pilot executed a gear-up landing on a mountainside. The aircraft was overweight and climb performance was insufficient.

What aircraft was involved and where did it happen?

The accident on 28 Jul 2001 involved a Cessna 172RG, registration N401TA, at Gunnison, CO.

What was the probable cause of the accident?

the pilot's failure to attain the proper climb rate, and his improper inflight planning/decision to attempt to cross mountainous terrain at an inadequate altitude. Contributing factors were the downdraft and the pilot's total lack of experience in mountain flying.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20010807X01621. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.