No fatalities

11 Feb 2024: ROBINSON HELICOPTER COMPANY R44 II (N74868) — SHEEP MOUNTAIN AIR LLC — Glacier View, AK

Glacier View, AK, United States

On 11 Feb 2024, a ROBINSON HELICOPTER COMPANY R44 II (registration N74868) operated by SHEEP MOUNTAIN AIR LLC was involved in an aviation accident near Glacier View, AK. No fatalities were reported. Investigators recorded the probable cause as: A sudden stoppage of the tail rotor for unknown reasons, which resulted in the tortional overload failure of the tail rotor driveshaft. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On February 11, 2024, a Robinson R44 II helicopter sustained substantial damage near Glacier View, Alaska, after the tail rotor driveshaft fractured during cruise flight. The pilot was not injured.

Accident Details

On February 11, 2024, at approximately 1130 Alaska standard time, a Robinson Helicopter R44 II, registration N74868, was substantially damaged in an accident near Glacier View, Alaska. The pilot was not injured. The helicopter was being operated as a Title 14 Code of Federal Regulations Part 91 business flight.

Pilot Account

According to the pilot, while in cruise flight with both aft doors removed, at about 700 ft above an area of snow-covered glacial terrain, he heard a loud “boom” noise and felt a slight airframe vibration. The pilot stated that he subsequently lost tail rotor thrust and performed an autorotation to an area of snow-covered, mountainous terrain.

Postaccident Inspection

A postaccident inspection, after the helicopter was recovered, revealed that the tail rotor driveshaft was fractured between the forward and aft flex plates, which resulted in substantial damage to the tail rotor driveshaft system.

Metallurgical Examination

The fractured pieces of the tail rotor driveshaft were sent to the NTSB Materials Laboratory for further examination. The examination revealed the fractures were consistent with ductile torsion overload. There was no evidence of pre-existing cracks or other damage to the driveshaft surfaces. The tail rotor blades were not damaged.

Tail Rotor Gearbox Inspection

The tail rotor gearbox assembly was removed from the accident helicopter and no anomalies were discovered.

Pilot Statements

The pilot stated that he did not have a passenger, but that he did have the doors off in preparation for a passenger/photographer later that day. He also stated that during his preflight inspection, he checked for loose items that could blow out and strike the tail rotor. The pilot did not submit the National Transportation Safety Board Pilot/Operator Aircraft Accident/Incident Report Form 6120.1.

Contributing factors

Tail rotor bladeTail rotor drive shaft — Failure