Casualties unknown

1994-09-22: Hughes 369D (N58352) — Same AS Registered Owner — Genoa, NV

Genoa, NV, US

On September 22, 1994, a Hughes 369D (registration N58352) operated by Same AS Registered Owner was involved in an aviation accident near Genoa, NV. Investigators recorded the probable cause as: THE PILOT/OPERATOR'S OPERATION OF THE HELICOPTER WITH A DISCONNECTED THROTTLE ON THE RIGHT COLLECTIVE; THE FAA INSPECTOR'S INADEQUATE PREFLIGHT/PRETAKEOFF CHECKS OF THE FLIGHT CONTROL/THROTTLE SYSTEMS; AND THE PILOT/OPERATOR'S FAILURE TO ADEQUATELY INFORM THE… 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 FAA inspector conducting a proficiency check experienced a hard landing when the pilot attempted to recover from a simulated engine failure, unaware that the right collective throttle was disconnected.

Incident Overview

An FAA operations inspector was performing a proficiency check for a pilot/operator while also obtaining flight time for personal recency requirements. Before the flight, the inspector administered an oral examination to the pilot. During preflight preparations, the pilot informed the inspector that the throttle on the right collective was inoperative—specifically, it was disconnected. However, the inspector did not assimilate this information. Additionally, during the preflight inspection, the inspector, who occupied the left seat, did not check throttle continuity to the right collective control.

Flight and Maneuvers

During the initial portion of the flight, the inspector flew the helicopter most of the time. Subsequently, the inspector directed the pilot to perform specific maneuvers to satisfy the proficiency check requirements. While returning to the airport, the inspector reduced his throttle to flight idle to simulate an engine failure and then transferred control to the pilot, instructing him to execute an autorotation.

Incident Sequence

The pilot did not realize that the inspector had reduced power using the operable (left) throttle until he raised the right collective in an attempt to recover from the autorotation near the ground. The helicopter subsequently sustained a hard landing.

Investigation Findings

An investigation disclosed that the pilot/operator had disconnected the right collective throttle linkage approximately two years before the flight. The inspector's failure to recognize the significance of the preflight briefing about the inoperative throttle and the lack of a throttle continuity check during preflight contributed to the sequence of events.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001206X02275. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.