CEN15LA084
2014-12-08 · Fort Lupton, Colorado, United States · Minor · 1 aircraft · Status: Completed
Airport 18V
N409LH has since been reassigned. It is now registered to a different aircraft (PILATUS AIRCRAFT LTD PC-12/47E, built 2024), which was not involved in this event.
Aircraft involved
Probable cause & findings
The loss of engine power during cruise flight for reasons that could not be determined based on the available information.
Factual narrative
On December 8, 2014, at 1115 mountain standard time, an Enstrom Helicopter, N409LH; experienced a total loss of engine power during cruise flight. The student pilot performed an autorotation to a field. The helicopter sustained substantial damage. The student pilot was uninjured. The helicopter was operated by Mountain One Helicopters under 14 Code of Federal Regulations Part 91 as an instructional flight that was operating on a flight plan. The flight last departed from Greeley-Weld County Airport, Greeley, Colorado, and was destined to Platte Valley Airpark, Hudson, Colorado. During a solo cross country flight flown by a student pilot, the helicopter experienced a total loss of engine power during cruise flight. The pilot performed an autorotation to a field. During landing flare, the helicopter tail struck the ground resulting in the main rotor blades flexing downwards, which severed the tail rotor boom. The helicopter sustained substantial damage to the fuselage and rotor blades. The pilot was uninjured. The engine was test run by the operator without the knowledge and permission of the National Transportation Safety Board Investigator-In-Charge or the Federal Aviation Administration Inspector assigned to the accident investigation. The operator stated the engine was run without any anomalies. The student pilot reported that, during a solo cross-country flight, the helicopter experienced a total loss of engine power during cruise flight. The pilot performed an autorotation to a field. During the landing flare, the helicopter's tail struck the ground, which resulted in the main rotor blades flexing upward and severing the tail rotor from the tailboom. The helicopter then fell to the ground and sustained substantial damage to the fuselage. The operator test ran the engine and noted no anomalies; no further engine examination or testing was conducted. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Not determined-Not determined-(general)-(general)-Unknown/Not determined - C
Verbatim from NTSB's published report. Source file
NTSB_2014_CEN15LA084.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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