ERA19LA032 · Titan T51
Titan T51 · Accident: loss of engine power (partial) during initial climb
From Valkaria Airport (X59) to Valkaria Airport (X59)
Event
- NTSB case
- ERA19LA032
- 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
Titan T51
- Aircraft type
- Titan T51
- 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
- N154DF
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From Valkaria Airport (X59), Valkaria, FLTo Valkaria Airport (X59), Valkaria, FL
- Aircraft age
- About 3 years (built 2015)
- 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
- Loss of engine power (partial)
- 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
The pilot stated that, shortly after takeoff on a local test flight of the experimental, amateur-built airplane, the engine surged, with a corresponding fuel pressure fluctuation. Because the engine was developing partial power, he elected to return to the airport for landing, but while on the base leg of the airport traffic pattern, the engine lost total power. The airplane subsequently impacted a small retention pond and came to rest partially submerged in water. Postaccident examination of the engine revealed damage to the Nos. 2 and 5 cast aluminum pistons consistent with detonation. The fuel pumps and engine control unit were operationally tested with no discrepancies reported. Inspection of the cooling system components revealed no evidence of pre-impact failure or malfunction, and no evidence of warpage of the cylinder heads was observed.
The owner reported continuing engine overheating problems that occurred at sustained “moderate” power settings, which he was unable to correct despite extensive troubleshooting efforts including re-routing of the coolant reservoir. Although he believed he was operating the engine with a rich fuel-to-air ratio, when compared to an identical airplane that was operating successfully, the accident engine was being operated in a lean fuel-to-air ratio at all power settings (500 to 5,000 in 250 rpm increments). This finding was consistent with the pilot’s report of overheating at sustained moderate power settings.
Probable cause
The partial, then total, loss of engine power due to detonation and associated damage to several pistons as a result of an overly lean fuel-to-air ratio.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record ERA19LA032
- Event ID
- 20181027X43914
- Case number
- ERA19LA032
- 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: e7042c29929cc2f2c81e64ff35182e8bc1b6a573f24956184a8e30f2b05e42a9; retrieved 2026-09-16T08:23:16.097Z.