Casualties unknown

1991-07-01: Hughes 269C (N11017) — Flight Safety International — Blakely, GA

Blakely, GA, US

On July 1, 1991, a Hughes 269C (registration N11017) operated by Flight Safety International was involved in an aviation accident near Blakely, GA. Investigators recorded the probable cause as: LOSS OF ENGINE POWER FOR AN UNDETERMINED REASON, AND FAILURE OF THE INSTRUCTOR PILOT (CFI) TO FOLLOW PROCEDURES AND MAINTAIN ROTOR RPM. 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

During a cross-country training flight, a CFI simulated an engine failure by closing the throttle at 900 feet AGL. Rotor RPM was not maintained as per POH, and the helicopter impacted a large field after a low-altitude restart attempt.

Incident Overview

A helicopter engaged in cross-country training experienced a simulated engine failure that led to an uncontrolled descent and impact with terrain. The flight instructor (CFI) had closed the throttle at approximately 900 feet above ground level (AGL) to simulate an engine failure. The subsequent autorotation did not maintain engine rpm at 2,500 as recommended by the pilot’s operating handbook (POH).

Sequence of Events

During the autorotation, the student pilot allowed the rotor rpm to deteriorate while attempting a power-on recovery at about 700 feet AGL. The student later reported that he did not realize the engine had stopped running. The CFI took control of the helicopter at approximately 700 feet AGL and attempted to restart the engine. The student stated that the rotor rpm remained low throughout the descent. Subsequently, the helicopter impacted the ground in a large field. The student noted that the helicopter felt as if it just dropped the last few feet of the autorotation.

Post-Accident Findings

No reason was verified for the loss of engine power. The POH specified that rpm should have been maintained during practice autorotations and that engine restarts should not be attempted below 2,000 feet AGL.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X17427. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.