ERA20CA106 · Aerospatiale AS350 B2
Hillsborough County Sheriffs Office Aerospatiale AS350 B2 · Accident: loss of engine power (total) during autorotation
From Peter O Knight Airport (TPF) to Tampa Executive Airport (VDF)
Event
- NTSB case
- ERA20CA106
- Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
- Accident
- InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
- Completed
- API-reported fatalities
- 0 · all aircraft and ground
- Ground fatalities
- Unknown
- OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
- General aviation
- WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
- Visual Meteorological Cond
Aerospatiale AS350 B2
- Aircraft type
- Aerospatiale AS350
- Category
- Helicopter
- RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
- N188FS
- Onboard fatalities
- Unknown
- Route
- From Peter O Knight Airport (TPF), Tampa, FLTo Tampa Executive Airport (VDF), Tampa, FL
- Aircraft age
- About 6 years (built 2014)
- Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
- Part 91: General Aviation
- Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
- Autorotation
- Defining eventThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
- Loss of engine power (total)
- DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
- Substantial
Cause areas
- Aircraft › Aircraft power plant
- Personnel issues › Task performance
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
The flight instructor in the helicopter reported that he directed the pilot receiving instruction to conduct an autorotation with a 180° turn, followed by a power recovery. Abeam the departure end of runway, he moved the throttle lever from the "fly" position to idle. While conducting the maneuver, the pilot overshot the runway and aligned the helicopter with the parallel taxiway. Upon realizing that the helicopter was not in the correct position, the pilots chose to abort the maneuver and perform a go-around. While the pilot continued to fly the helicopter, the instructor inadvertently moved the throttle lever from idle aft toward the "off" position and then forward to the "fly" position. The engine experienced a total loss of power, and the instructor adjusted the throttle to no avail. As the helicopter descended, the pilot requested that the instructor "get on the controls." The instructor took the controls, conducted a power-off autorotation, and landed the helicopter on the taxiway. The helicopter skidded about 180 ft, departed the taxiway onto adjacent grass, and came to rest in a drainage ditch. The instructor reported that there were no preaccident mechanical failures or malfunctions with the helicopter that would have precluded normal operation. The Federal Aviation Administrator inspector who examined the helicopter reported that the left antivibrator mount beam had sustained substantial damage.
Probable cause
The flight instructor's inadvertent throttle reduction below idle, which resulted in a total loss of engine power and subsequent impact with terrain following a power-off autorotation.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record ERA20CA106
- Event ID
- 20200220X92633
- Case number
- ERA20CA106
- Dataset
- full-current
- Source SHA-256
- 5cf380f0061817c0331a6b2d8cc7e0ee3a79bea469a1001dc5c10e56f35f5ab3
Source notes (4)
- Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
- Filled from the NTSB case API where the bulk record had no value: investigation status. Values present in the bulk record are kept.
- The date is the local date, which is the same as the UTC date the NTSB stores.
- API snapshot SHA-256: 280bcb9a4f660516b182da62bab5aab558c61da04dd0ade5898be5707863a789; retrieved 2026-09-16T11:09:05.284Z.