ERA11FA512 · Heronimus Kevin A GLASAIR III
Heronimus Kevin A GLASAIR III · Accident: powerplant system/component malfunction/failure while maneuvering
From Rough River State Park Airport (2I3) to Rough River State Park Airport (2I3)
Event
- NTSB case
- ERA11FA512
- 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
- 1 · 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
Heronimus Kevin A GLASAIR III
- Aircraft type
- Heronimus Kevin GLASAIR
- Category
- Airplane
- 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
- N43KH
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From Rough River State Park Airport (2I3), Falls of Rough, KYTo Rough River State Park Airport (2I3), Falls of Rough, KY
- 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
- Maneuvering · low-altitude flying
- 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
- Powerplant system/component malfunction/failure
- 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
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
According to witnesses, the airplane departed the airport and circled back to make a fly-by over the runway. As the airplane flew over the runway, a witness reported that the engine sounded like it “over revved.” Witnesses also stated that they saw what appeared to be a puff of smoke emitting from the nose of the airplane. The pilot made a left banking turn, and then entered a left downwind for the runway. The engine power seemed to surge as the airplane descended. Then the engine went silent and the airplane turned toward the airport but did not have enough altitude to reach the runway. The pilot appeared to level the wings, and the landing gear was lowered as the airplane descended into the trees, struck a building, and exploded.
A postaccident examination of the airplane revealed that it was equipped an automotive Chevrolet LS1 engine. The airplane’s propeller was attached to a propeller speed reduction unit (PSRU). The system was designed with an automatic clutch and was tuned to remain disengaged at idle and engage with an increase in power. An examination of the PSRU revealed that the propeller drive shaft fractured as a result of fatigue. This fracture separated the propeller drive gears from the clutch, which resulted in the loss of power to the propeller. Given the witness accounts of the loss of engine power, it is likely that the airplane lost airspeed and altitude due to this condition.
Probable cause
The failure of the propeller power speed reduction unit, which resulted in a loss of engine power at low altitude.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record ERA11FA512
- Event ID
- 20110930X51940
- Case number
- ERA11FA512
- 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: aa42323d3548703e321aa1e7d85738cc9e98d0ad799163d7ad8b3e31b287b1c2; retrieved 2026-09-13T21:53:18.857Z.