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NYC04CA001 · Williams RV-4

3 Oct 2003 · Metz, WV, United States

Williams RV-4 · Accident: total loss of engine power (non-mechanical) en route

From Vermilion Regional Airport (DNV) to Morgantown Municipal Airport Walter L. (Bill) Hart Field (MGW)

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Event

NTSB case
NYC04CA001
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

Williams RV-4

Aircraft type
Williams RV-4
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
N475F
Operator
Unknown
Onboard fatalities
Unknown
Route
From Vermilion Regional Airport (DNV), Danville, ILTo Morgantown Municipal Airport Walter L. (Bill) Hart Field (MGW), Morgantown, WV
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
En route · cruise
First occurrenceThe 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
Total loss of engine power (non-mechanical)
Also codedOther events the NTSB coded in the sequence, such as a wire strike after a loss of power. Flight Findings uses them for its kinds of event. Glossary
Fuel exhaustion; Pole
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

  • Fluid, fuel › Exhaustion
  • Pilot in command › Operation with known deficiencies in equipment, intentional

Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.

NTSB narrative

The pilot was en route to his home base, with a homebuilt kit airplane when the engine lost power, after about 2.4 hours of flight. During the forced landing the airplane struck an electrical pole. Examination revealed the fuel tanks were empty, and there was no evidence of a fuel spill on the ground, although both fuel tanks were ruptured. There was no blue staining on the top of the wings, or under the fuselage, although heavy rains had fallen for two days between the accident, and its examination by the FAA. There were no loose fittings on the fuel line leading to the engine. The spark plugs were slate gray in appearance, and thumb compression was found in all cylinders. The pilot reported that the fuel gauges were inaccurate and fuel consumption on the 2 previous flights had averaged between 8.5 and 9.5 gallons per hour. At the last refueling, the pilot had requested that the fuel servicing person leave about 1 inch of space at the top of the fuel tank. The pilot reported that when he preflighted the airplane, he thought the fuel level was down about 1 inch from the top of the tank, The fuel tanks were reported to hold 16 gallons in each wing. A representative of the kit manufacturer reported that the fuel tank capacity could vary by a few gallons, along with the amount of unusable fuel due to variations in fuel tank assembly by builders. The experimental operating limitations issued by the FAA for the airplane required an operative fuel indicating system to indicate the amount of fuel in each tank.

Probable cause

The pilot's improper decision to operate without accurate fuel gauges, which resulted in a power loss due to fuel exhaustion, and an off airport landing

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record NYC04CA001
Event ID
20031113X01895
Case number
NYC04CA001
Dataset
historical-pre2008
Source SHA-256
89e2df6d848e7ab3b42e7d7c7a03ff403303057a26ca04c95b3ea67201c3ce74
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, coordinates. 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: 4c57c0d5042d10a818d2839784ba8dce1f2e7ccdc47c998ad1d4c6b051fff9d1; retrieved 2026-09-22T08:24:51.856Z.