ERA14CA080
2013-12-28 · White Plains, New York, United States · Minor · 1 aircraft · Status: Completed
Airport HPN
Aircraft involved
Probable cause & findings
The flight instructor's failure to maintain airspeed during a practice autorotation, which resulted in a hard landing and subsequent loss of control
Factual narrative
The flight instructor (CFI) was demonstrating a 180-degree autorotation to a student pilot while performing an instructional flight. The CFI reported entering the autorotation when, at about 100 feet agl, the indicated airspeed suddenly dropped to about 40 knots. He pushed the cyclic forward in an attempt to regain airspeed and flared at about 50 feet agl in an attempt to slow down the helicopter's rate of descent. The helicopter landed on the edge of the runway on the back of the skids, bounced back into the air, and began an accelerated yaw to the right. According to the CFI, he lowered the collective and reduced throttle while the helicopter spun four or five times. The helicopter subsequently impacted the ground, and came to rest on its left side. A postaccident examination by a Federal Aviation Administration inspector revealed substantial damage to the cabin and the tail boom. The CFI reported no preaccident mechanical malfunctions or failures that would have precluded normal operation. The flight instructor (CFI) was demonstrating a 180-degree autorotation to a student pilot while performing an instructional flight. The CFI reported entering the autorotation when, at about 100 feet agl, the indicated airspeed suddenly dropped to about 40 knots. He pushed the cyclic forward in an attempt to regain airspeed and flared at about 50 feet agl in an attempt to slow down the helicopter's rate of descent. The helicopter landed on the edge of the runway on the back of the skids, bounced back into the air, and began an accelerated yaw to the right. According to the CFI, he lowered the collective and reduced throttle while the helicopter spun four or five times. The helicopter subsequently impacted the ground, and came to rest on its left side. A postaccident examination by a Federal Aviation Administration inspector revealed substantial damage to the cabin and the tail boom. The CFI reported no preaccident mechanical malfunctions or failures that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Personnel issues-Psychological-Attention/monitoring-Monitoring equip/instruments-Instructor/check pilot - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Airspeed-Not attained/maintained - C
- F Personnel issues-Task performance-Use of equip/info-Use of equip/system-Instructor/check pilot - F
- F Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Landing flare-Incorrect use/operation - F
Verbatim from NTSB's published report. Source file
NTSB_2013_ERA14CA080.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
Matched on aircraft type or causal vocabulary (loss of control). All research papers
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- Semantic Scholar 2021 · Article (Aviation) ANALYSIS OF GENERAL AVIATION FIXED-WING AIRCRAFT ACCIDENTS INVOLVING INFLIGHT LOSS OF CONTROL USING A STATE-BASED APPROACH
Inflight loss of control (LOC-I) is a significant cause of General Aviation (GA) fixed-wing aircraft accidents. The United States National Transportation Safety Board’s database provides a rich source…
- NASA NTRS 2021 · Presentation Use of Design of Experiments in Determining Neural Network Architectures for Loss of Control Detection
Abstract—We describe empirical methods for selecting a neural network architecture to implement belief state inference on generic commercial transport aircraft.