ERA16CA160
2016-04-16 · Baltimore, Maryland, United States · None · 1 aircraft · Status: Completed
Airport BWI
N326AC has since been reassigned. It is now registered to a different aircraft (DJI AGRAS T100), which was not involved in this event.
Aircraft involved
Probable cause & findings
The pilot's inadequate compensation for the wind while hovering out of ground effect, which resulted in a loss of tail rotor effectiveness.
Factual narrative
The helicopter began the power line aerial observation flight near its maximum gross weight. As the pilot maneuvered the helicopter into an out-of-ground-effect hover with a 12-knot left crosswind, a nose-right yaw ensued that could not be corrected with a full left pedal application. Despite other remedial actions taken by the pilot, the helicopter descended to ground contact where the occupants egressed, but the helicopter was later destroyed by post-crash fire. The pilot stated there were no mechanical anomalies that would have precluded normal operation. He said, "It was an aerodynamic issue, not a mechanical issue."FAA Advisory Circular (AC) 90-95, Unanticipated Right Yaw in Helicopters stated, "Any maneuver which requires the pilot to operate in a high-power, low-airspeed environment with a left crosswind or tailwind creates an environment where unanticipated right yaw may occur." The helicopter began the power line aerial observation flight near its maximum gross weight. As the pilot maneuvered the helicopter into an out-of-ground-effect hover with a 12-knot left crosswind, a nose-right yaw ensued that could not be corrected with a full left pedal application. Despite other remedial actions taken by the pilot, the helicopter descended to ground contact where the occupants egressed, but the helicopter was later destroyed by post-crash fire. The pilot stated there were no mechanical anomalies that would have precluded normal operation. He said, "It was an aerodynamic issue, not a mechanical issue." FAA Advisory Circular (AC) 90-95, Unanticipated Right Yaw in Helicopters stated, "Any maneuver which requires the pilot to operate in a high-power, low-airspeed environment with a left crosswind or tailwind creates an environment where unanticipated right yaw may occur." Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Environmental issues-Conditions/weather/phenomena-Wind-(general)-Response/compensation - C
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- C Personnel issues-Task performance-Planning/preparation-Performance calculations-Pilot - C
- — Personnel issues-Task performance-Planning/preparation-Weight/balance calculations-Pilot
- — Aircraft-Aircraft propeller/rotor-Tail rotor-(general)-Related operating info
Verbatim from NTSB's published report. Source file
NTSB_2016_ERA16CA160.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. All research papers
- NASA NTRS 2019 · Preprint (Draft being sent to journal) Terrain Portrayal for Head-Down Displays Flight Test
The Synthetic Vision Systems General Aviation (SVS-GA) element of NASA's Aviation Safety Program is developing technology to eliminate low visibility induced General Aviation (GA) accidents through th…
- NASA NTRS 2010 · Abstract Emerging Standards for Aerodrome Mapping Databases and Datalink Technologies to Enable Reductions in Runway Incursions/Excursions
The integration of onboard databases with data linked aeronautical information services (AIS) is a task that RTCA and EUROCAE are pursuing.