Casualties unknown

Helicopter Practice Takeoff Ends in Ridge Striking and Inversion Near Parkman, Wyoming (N7052L)

Parkman, WY, US

On June 1, 1999, a Hughes 269A (registration N7052L) was involved in an aviation accident near Parkman, WY. Investigators recorded the probable cause as: The pilot's inadequate in-flight planning by exceeding the helicopter's performance climb capability. Factors were the downdraft encountered during initial climb following takeoff, and the high density 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 2026-06-10Data APIEditorial standards

A pilot conducting a practice takeoff in a helicopter near Parkman, Wyoming, encountered a downdraft after clearing a ridge, resulting in a loss of altitude and impact with trees. The aircraft inverted. No mechanical issues were reported.

Accident Overview

An hour after landing in an open field at 6,200 feet mean sea level near Parkman, Wyoming, within the Bighorn National Forest, a pilot conducted a practice takeoff without a passenger to assess the helicopter's performance. The helicopter achieved effective translational lift and hovered normally, then climbed out at 40 knots.

Sequence of Events

Shortly after clearing a 75-foot ridge located 100 to 150 yards from the takeoff field, the aircraft exited ground effect and encountered a downdraft. Subsequently, the helicopter began to lose altitude. The power required for climbing exceeded the power available. The aircraft descended through 60 to 80 feet of trees before impacting the ground and coming to rest inverted.

Pilot and Performance Data

The pilot reported no mechanical problems and stated the engine was running upon impact. The density altitude at the time of the accident was calculated to be 7,578 feet. Based on calculated weight and performance data, the helicopter's gross weight at departure was approximately 1,232 lbs. At an indicated airspeed of 35 knots, the maximum obstacle clearance height was 75 feet, with a maximum distance of 800 feet.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X18972. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.