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ERA10CA262 · Hiller UH12

9 May 2010 · Sarasota, FL, United States

Helicopter Service by Randy Hiller UH12 · Accident: hard landing during autorotation

From Dove Heliport (FA22) to Dove Heliport (FA22)

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Event

NTSB case
ERA10CA262
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

Hiller UH12

Aircraft type
Hiller UH12
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
N116S
Onboard fatalities
Unknown
Route
From Dove Heliport (FA22), Sarasota, FLTo Dove Heliport (FA22), Sarasota, FL
Aircraft age
Not recorded
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
Hard landing
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

  • Personnel issues › Action/decision

Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.

NTSB narrative

The pilot/owner of the helicopter stated that while in cruise flight, he let his rotor rpm decay due to inattention and "complacency." He decided he could not recover the rotor rpm "quickly enough" and performed an autorotation to a pasture. The pilot leveled the helicopter about 8 feet above the ground where it "lost lift [and] dropped straight down." At ground contact, the main rotor blades contacted the tail boom, which resulted in substantial damage. The pilot reported there were no mechanical malfunctions or failures of the helicopter.

Probable cause

The pilot's delayed remedial action to maintain main rotor rpm, which resulted in a loss of lift and hard landing.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record ERA10CA262
Event ID
20100512X55519
Case number
ERA10CA262
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: 04d2d558d83de08c8a77746f26983998c0a13e7214951047b5adee0a07ae2ff3; retrieved 2026-09-15T14:04:55.031Z.