FLIGHT FINDINGSAVIATION OCCURRENCE MAP
Back to map

ATL03LA012 · Beech F33A

31 Oct 2002 · Fernandina Bch, FL, United States

Beech F33A · Accident: total loss of engine power (non-mechanical) en route

From 55J · Fernandina Bch, FL to an unrecorded destination

Report a problem

Event

NTSB case
ATL03LA012
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
1 · 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

Beech F33A

Aircraft type
Beechcraft 33
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
N3122K
Operator
Unknown
Onboard fatalities
Unknown
Route
From 55J · Fernandina Bch, FLTo not recorded
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 · climb to 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
Tree(s)
DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
Destroyed

Cause areas

  • Fuel system › Contamination, water

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

NTSB narrative

According to the airframe and powerplant mechanic passenger, the airplane was on a maintenance test flight. After takeoff the airplane climbed to 2,500 feet, and experienced a loss of engine power. Attempts by the pilot to restore engine power were unsuccessful. While attempting to return to the airport the airplane collided into a wooded area short of runway 22. The pilot and mechanic exited the airplane. The airplane was consumed by post-crash fire. During the on scene engine examination approximately eight ounces of water was drained from the fuel selector. Examination of the fuel strainer found rust on the strainer spring, and heat damage on the internal rubber components. Approximately three ounces of water was drained from the sump during the on scene examination. The engine was removed and sent to Teledyne Continental Motors for further examination.The internal examination of the fuel pump found it to be damaged in the post-crash fire. There were heavy deposits of lacquer found in the internal vanes of the fuel pump that operate the pumping action. The fuel manifold was flow tested and it was found to be within operating parameters. The engine driven fuel pump could not be tested because it would not rotate.

Probable cause

Water contamination in the fuel system which resulted in the loss of engine power and the subsequent collision with trees.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record ATL03LA012
Event ID
20021104X05424
Case number
ATL03LA012
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: b842929eb7d411e31e8a5cfbb8280ad4e057e647d1ea180d651b555931a66275; retrieved 2026-09-20T19:43:14.608Z.