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ERA24LA179 · Cessna R172 E

14 Apr 2024 · Rocky Mount, NC, United States

Cessna R172 E · Accident: fuel contamination en route

From Delaware Airpark (33N) to Rocky Mount Wilson Regional Airport (RWI)

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Event

NTSB case
ERA24LA179
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
0
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

Cessna R172 E

Aircraft type
Cessna 172
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
N3FR
Operator
Unknown
Onboard fatalities
Unknown
Route
From Delaware Airpark (33N), Dover/Cheswold, DETo Rocky Mount Wilson Regional Airport (RWI), Rocky Mount, NC
Aircraft age
About 57 years (built 1967)
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 · descent
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
Fuel contamination
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 › Fluids/miscellaneous hardware
  • Personnel issues › Task performance

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

NTSB narrative

The airplane had not been used for 2 years following an engine overhaul. A mechanic completed an annual inspection of the airplane, and when he and the pilot performed a preflight inspection before beginning the multi-leg trip, they found that the fuel contained, “a lot of water.” They fully fueled the airplane, allowed it to settle overnight, and then “shook” the airplane’s wings before sampling fuel. They also ran the airplane’s engine for two hours on the ground before departing on the first leg of the trip. At the next fuel stop, they drained about “a tablespoon” of water from the fuel system, and during the second fuel stop, they only observed about “2 drops” of water. The accident flight was the third leg of the trip. After nearly 3 hours of flight, and while descending to the destination airport with the carburetor heat applied, the engine lost total power. The pilot established best glide speed and attempted to restore engine power; however, he was unsuccessful and performed a forced landing onto a city street, substantially damaging the fuselage, empennage, and both wings. Postaccident examination of the engine revealed that one of the cylinders exhibited excessive piston-to-cylinder clearance, circumferential markings of the cylinder walls that were not consistent with the typical cross-hatching pattern that would be expected in an engine shortly after overhaul, and its intake valve was stuck open. While anomalous, each of these findings could reasonably be associated with some partial loss of engine power, but not the complete loss of engine power that was described by the pilot during the descent phase of the accident flight. The examination of the airframe also revealed rust around the fuel filler ports, indicative of water entry into the airplane’s fuel tanks. While fuel recovered from the left wing fuel tank was free from contaminants, significant water and debris were observed in fuel recovered from the gascolator and carburetor bowls. Given this information, it is likely that the total loss of engine power was due to contamination of the fuel supply with water and particulate matter.

Probable cause

The pilot and mechanic’s failure to identify and completely eliminate the water and debris contamination present in the airplane’s fuel system before embarking on the flight, which resulted in a total loss of engine power.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record ERA24LA179
Event ID
20240416194096
Case number
ERA24LA179
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: local date, investigation status, coordinates, cause areas. Values present in the bulk record are kept.
  • The date is the local date; the NTSB stores the UTC date 2024-04-15.
  • API snapshot SHA-256: 1b77beda2e15585086a45755338d8fb410ae812671b1b0ba02ca5c6849ce3562; retrieved 2026-09-16T18:40:36.696Z.