NYC08FA292 · Steven A. Jones Lancair IV P
Steven A. Jones Lancair IV P · Accident: electrical system malfunction/failure while maneuvering
From Stafford Regional Airport (RMN) to Stafford Regional Airport (RMN)
Event
- NTSB case
- NYC08FA292
- 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
Steven A. Jones Lancair IV P
- Aircraft type
- Steven A Jones LANCAIR
- 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
- N731SJ
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From Stafford Regional Airport (RMN), Stafford, VATo Stafford Regional Airport (RMN), Stafford, VA
- 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
- 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
- Electrical system 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
- Personnel issues › Action/decision
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
The airplane was equipped with a dual battery system. After takeoff the pilot turned on the standby battery switch to charge the standby battery. He smelled smoke which became “very heavy and thick.” After landing, he opened the door and the smoke evacuated. He observed "billowing clouds of black and gray acrid smoke," toward the rear of the airplane. After opening the baggage compartment door, and removing the compartment floor, the pilot discharged a fire extinguisher into the area of the standby battery. He observed a flame, and discharged the fire extinguisher again. He then observed a red glow in the battery box. During construction of the airplane, the pilot had coated the inside of the battery box with room temperature vulcanizing (RTV) silicone. Examination revealed, remnants of a charred wood block (a combustible organic material), and the RTV silicone which had charred, melted, and adhered to the top of the standby battery and its partially melted vent caps. Holes with charring along the upper edge of one side of the battery case were evident where the battery outgassed since its vents caps were blocked. Lead acid batteries must be protected from overcharging and sources of ignition, as hydrogen gas can explode when ignited. Sulfuric acid in contact with combustible and/or organic materials can cause fire or explosion. The airplane’s voltage regulators were mounted in the engine compartment. Their cases were metal, they were rectangular in shape, and a plastic terminal strip protruded from a slot in the case on one side. The regulators were not potted, the internal circuit board was not conformally coated, and no weather seal existed between the plastic terminal strip and the case. Water staining and evidence of arcing were present on the inside of the standby regulator. The manufacturer recommended the regulators be installed in a location that would protect them from heat, vibration, and water on the pilot side of the firewall, or inside the cabin. The pilot was aware of the recommendation, but thought that the heat in the airplane would be worse in the cockpit than in the engine compartment. He also believed the regulators were "sealed in Bakelite," and it would provide "ease of access" to mount them on the firewall.
Probable cause
The pilot's decision to install voltage regulators in the engine compartment where they were susceptible to water intrusion, which resulted in a malfunction of the standby electrical system's voltage regulator and a subsequent in-flight fire.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record NYC08FA292
- Event ID
- 20080922X01515
- Case number
- NYC08FA292
- 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: eff387faf2262e1f18920adf1bd2218c8227b09131d98417e697d6535f003882; retrieved 2026-09-15T10:15:42.194Z.