Casualties unknown

1996-10-29: Bell 47G-3B-1 (N3098G) — Usfs — Fillmore, UT

Fillmore, UT, US

On October 29, 1996, a Bell 47G-3B-1 (registration N3098G) operated by Usfs was involved in an aviation accident near Fillmore, UT. Investigators recorded the probable cause as: inadequate procedure and inadequate monitoring by the pilot, the operator, and/or other personnel, which allowed one of three external cables to the seed bucket to become entangled with the right skid of the helicopter, resulting in an imbalance and loss of… This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 2 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

A helicopter collided with a 45-degree slope after a seed bucket line became entangled around the right skid during a seeding operation. The pilot had jettisoned the load before impact but the line remained caught.

Background

A pilot had completed approximately 20 seeding runs using a helicopter fitted with a seed bucket suspended by three 40-foot-long lines. The landing zone for each run was the same. During each landing, the bucket touched the ground first, then the pilot maneuvered the helicopter backward and set down with the bucket positioned in front.

Flight Sequence

After two ground crew members filled the seed bucket, they moved away to avoid rotor wash. One crouched behind a rock; the other stood near the seed bags with his back to the helicopter. As the helicopter began to lift off, one of the three lines attached to the seed bucket looped over the right skid. The helicopter continued to gain altitude, and the seed bucket started to tip, spilling seed.

Accident

Witnesses located about 50 yards downhill from the landing zone reported that the pilot appeared to have difficulty controlling the helicopter as it climbed and moved forward. The helicopter continued into rising terrain and struck a 45-degree slope in a nose-down attitude with a slight right bank.

Post-accident Inspection

Examination of the helicopter after the accident revealed that the pilot had jettisoned the external load, and the hook release at the belly of the helicopter had activated before the collision. However, one of the lines remained entangled around the right skid.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001208X06988. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.