MIA93FA031 · Beech 65
Beech 65 · Accident: total loss of engine power (non-mechanical) en route
From Orlando Sanford International Airport (SFB) to Fort Lauderdale Executive Airport (FXE)
Event
- NTSB case
- MIA93FA031
- 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
- 5 · 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
- Instrument Meteorological Cond
Beech 65
- Aircraft type
- Beechcraft 65
- 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
- N555GC
- Operator
- Edwards, William J. · private individual
- Onboard fatalities
- Unknown
- Route
- From Orlando Sanford International Airport (SFB), Sanford, FLTo Fort Lauderdale Executive Airport (FXE), Fort Lauderdale, FL
- 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)
- 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, fuel control › Contamination
- Fuel system, fuel control › Corroded
- Fuel system, strainer › Incorrect
- Other maintenance personnel › Maintenance, improper
- Pilot in command › Altitude, not maintained
- Pilot in command › Propeller feathering, not performed
- Reason for occurrence undetermined
Approximate · Estimated position: the centre of Orlando, FL, the place the record names. Not the accident site.
NTSB narrative
PLT REPORTED LEVEL AT 6,000 FT; NO FURTHER TRANSMISSIONS WERE RECEIVED. RADAR DATA SHOWS THAT AFTER 5 MIN AT CRUISE FLT GROUNDSPEED BEGAN TO SLOW, AND AS SPEED REACHED 85 KTS (VMC IS 83 KTS) ACFT MADE A RAPID TURN TO THE LEFT AND THE SPEED DROPPED TO 74 KTS. RADAR CONTACT WAS THEN LOST. WITNESSES REPORTED HEARING AND SEEING ACFT WITH AN ENG SPUTTERING AND QUITTING, AT WHICH TIME NO ENG NOISE WAS AUDIBLE. ENG WOULD THEN RESTART, AND AT ONE POINT ACFT WAS OBSERVED INITIATING A CLIMB AFTER ENG START. ENG RESTARTED AND OBTAINED NEAR FULL POWER, AND A SHORT TIME LATER SOUND OF IMPACT WAS HEARD. THE LEFT ENG FUEL SERVO WAS FOUND CONTAMINATED WITH CORROSION AND DIRT, AND WOULD NOT ALLOW FUEL FLOW TO THE ENG. THE FUEL STRAINER FOR THIS ENG WAS INSTALLED BACKWARDS ALLOWING UNFILTERED FUEL TO ENTER THE ENG. THE LEFT PROPELLER WAS NOT FEATHERED AND HAD NO SIGNS OF ROTATION UNDER POWER. RIGHT ENG FUEL SERVO ALSO CONTAINED CORROSION & CONTAMINATION. THE AIRCRAFT DID NOT HAVE A CURRENT ANNUAL INSPECTION.
Probable cause
THE PILOT'S FAILURE TO FEATHER THE PROPELLER TO MAINTAIN ALTITUDE FOLLOWING A LOSS OF POWER OF THE LEFT ENGINE. THE POWER LOSS WAS DUE TO AN IMPROPERLY MAINTAINED FUEL SYSTEM. IN ADDITION, THE RIGHT ENGINE LOST POWER FOR AN UNDETERMINED REASON(S).
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record MIA93FA031
- Event ID
- 20001211X16201
- Case number
- MIA93FA031
- 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. 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: 1b77e8665fe26cce9b3a2bf0741bd27755f4e0b4eea6b4abcd608b40ddefd0db; retrieved 2026-09-21T00:45:45.452Z.