Titan T51 accident near Valkaria, Florida, October 27, 2018
On October 27, 2018 at about 5:15 pm local time, a 2015 Titan T51, an amateur-built aircraft,, registered N154DF, was substantially damaged in an accident during initial climb near Valkaria, Florida (Valkaria Airport). It was a personal flight under general aviation rules (Part 91). 1 person was seriously injured. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
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.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- October 27, 2018 · about 5:15 pm local time
- Place
- Valkaria, Florida · Valkaria Airport · map
- Type
- Accident
- Injuries
- 1 person was seriously injured.
- Weather
- visual conditions (good weather)
- Aircraft
- Titan T51 NO SERIES, built 2015, amateur-built
- Registration
- N154DF · no longer on the register · serial M10SV6S0HK0154
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
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.
The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.
The factual record from the NTSB's investigation tables, in plain English
What happened, in order
- Loss of engine power (partial) during initial climb defining event
- Loss of engine power (total) during maneuvering
- Dragged wing/rotor/float/other during landing (flare/touchdown)
The NTSB's findings
- cause Aircraft › Aircraft power plant › Engine (reciprocating) › Recip engine power section › Damaged/degraded
- factor Personnel issues › Task performance › Maintenance › Modification/alteration › Owner/builder
- Aircraft › Aircraft power plant › Engine fuel and control › Fuel control electronic › Incorrect service/maintenance
Pilot
- Certificate: flight instructor, commercial pilot
- Ratings: multi-engine land; single-engine land; single-engine sea; instructor: airplane multi-engine; instructor: airplane single-engine; instructor: instrument airplane; instrument: airplane
- Flight time: 9,988 hours in all; 4 in this make and model; 20 in the last 90 days; 7 in the last 30 days; 9,851 as pilot in command; 8,293 on instruments
- Last flight review: June 21, 2017
- Medical certificate: Class 3 (without waivers/limitations)
- Seat: frt
- Injury: serious injuries
The aircraft
- Airframe total time: 10 hours
- Last inspection: condition inspection, April 14, 2018
- Maximum gross weight: 1,462 lb
- Seats: 1
- Landing gear: retractable
- Engine: Honda J35 A6 (piston); 0 hours total
The flight
- Departed from: X59 Valkaria FL at 5:43 pm
- Destination: X59 Valkaria FL
- Flight plan: none
- Runway 28, 4,000 ft by 75 ft
Weather at the time
- Light: daylight
- Wind: from 280° at 11 knots
- Visibility: 10 statute miles
- Sky: broken clouds at 3,600 ft
- Temperature: 81°F (27°C), dew point 61°F (16°C)
- Altimeter: 29.90 inHg
- Observation at 4:53 pm from MLB, 9 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
10 documents, released by the NTSB on July 27, 2021. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.
| # | Document | What it is | |
|---|---|---|---|
| 1 | Pilot/operator Aircraft Accident Report, NTSB Form 6120.1 | PDF, 11 pages | View Download |
| 2 | Witness Statement | PDF, 1 page | View Download |
| 3 | Record of NTSB Conversations | PDF, 9 pages | View Download |
| 4 | Memorandum for Record - Engine Examination Results | PDF, 2 pages | View Download |
| 5 | Memorandum for Record - Engine Cooling System Trouble Shooting | PDF, 2 pages | View Download |
| 6 | Memorandum for Record - Engine Overheating Information | PDF, 1 page | View Download |
| 7 | Memorandum for Record - Ecu Set Up Procedures | PDF, 1 page | View Download |
| 8 | Engine Control Unit Program Values for Accident Airplane | PDF, 1 page | View Download |
| 9 | Engine Control Unit Program Values for Exemplar Airplane | PDF, 1 page | View Download |
| 10 | Investigative Photographs | PDF, 5 pages | View Download |
The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.
Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.
