Casualties unknown

2000-04-25: Cessna 152 (N67435) — Austin, NV

Austin, NV, US

On April 25, 2000, a Cessna 152 (registration N67435) was involved in an aviation accident near Austin, NV. Investigators recorded the probable cause as: The pilot's decision to attempt flight in an area of high rising mountainous terrain at an inadequate altitude, which resulted in an impact during a turn to reverse direction. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

An airplane impacted a 20-degree upsloping mountainside at 8,100 ft msl while attempting a reverse course maneuver in a valley. The climb rate under high density altitude was insufficient to outclimb the terrain gradient. No mechanical malfunction was found.

Accident Narrative

According to data from a handheld GPS unit, the pilot flew up a valley at low altitude over upsloping mountainous terrain along the flight route. The airplane was unable to outclimb the rising terrain and struck the mountainside nearly perpendicular to its face at an elevation of 8,100 feet mean sea level. The impact occurred on a 20-degree upsloping slope while the pilot was maneuvering the airplane during an attempted reverse course maneuver.

Pilot Background

In January 2000, both pilots began primary flight training at a Texas-based flight school. They were issued Private Pilot certificates in March 2000 and had each received approximately 6 hours of dual cross-country flight training. Neither pilot had received training in high-density altitude operations or mountain flying.

Performance and Terrain Analysis

The airplane possessed the published performance capability to overfly the mountainous terrain. However, under high density altitude standard atmospheric conditions, its maximum rate of climb was reduced to about 380 feet per minute at 62 knots indicated airspeed (70 knots true airspeed), equating to approximately 326 feet per nautical mile. Within the 3 nautical miles leading to the accident site, the terrain elevation increased from 7,100 to 8,100 feet mean sea level, a gradient of about 333 feet per nautical mile. The airplane's climb rate ability was therefore less than the slope of the terrain.

Wreckage Examination

No evidence of any airframe or engine mechanical malfunction was noted during the on-scene wreckage examination.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X20840. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.