ERA15LA332 · Lancair IV P
Lancair IV P · Accident: powerplant system/component malfunction/failure during initial climb
From Fort Lauderdale Executive Airport (FXE) to Lynchburg Regional Airport - Preston Glenn Field (LYH)
Event
- NTSB case
- ERA15LA332
- 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
Lancair IV P
- Aircraft type
- Lancair IV
- 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
- N864KM
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From Fort Lauderdale Executive Airport (FXE), Fort Lauderdale, FLTo Lynchburg Regional Airport - Preston Glenn Field (LYH), Lynchburg, VA
- Aircraft age
- About 18 years (built 1997)
- 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
- Initial climb
- 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
- Destroyed
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 pilot stated that, during the climb to cruise altitude, he noticed a loss of engine oil pressure. He declared an emergency with air traffic control (ATC) and requested to return to the airport. After ATC acknowledged, the pilot advised ATC that he lost all engine power and had to make an emergency landing. During the forced landing, the airplane collided with a ditch and was destroyed by postcrash fire. An examination of the engine revealed that it failed catastrophically, displaying signatures of lubrication distress; further, no measurable quantity of oil could be recovered from within the engine. Detailed examination of the engine's turbochargers revealed that one of the two units displayed evidence of burnt oil on the external surface and evidence of a foreign material in the unit's center housing, on the thrust bearing, and on the thrust collar. The foreign material was identified as polyethylene (plastic), similar to that used to protect the exposed orifices of the engine during shipment.
Review of maintenance records revealed that the pilot/mechanic had replaced both turbochargers with overhauled units two days before the accident flight. The turbocharger overhauler provided installation instructions and warnings that, in part, stated, "Remove all protective caps and plugs BEFORE installing this turbocharger." The foreign material discovered within the turbocharger's center housing suggests that the protective plastic cap at the oil outlet was likely not removed during the installation. It is likely that the turbocharger center housing filled with oil, which then flowed out of the engine via the turbocharger housing backplate, resulting in oil starvation and the subsequent total loss of engine power.
Probable cause
The mechanic's improper installation of the turbocharger assembly, which resulted in oil starvation and a subsequent total loss of the engine power.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record ERA15LA332
- Event ID
- 20150831X95341
- Case number
- ERA15LA332
- 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: 68430cbd01ad6cef19a48a534ca712c0fff5ac292394c4e0df3c2eced99bbe87; retrieved 2026-09-16T02:43:57.457Z.