FTW93FA008 · Beech 95-B55B
Beech 95-B55B · Accident: total loss of engine power (non-mechanical) en route
From OM6 · Batesville, MS to Beaumont Municipal Airport (BMT)
Event
- NTSB case
- FTW93FA008
- 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
- 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
Beech 95-B55B
- Aircraft type
- Beechcraft 95
- 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
- N153Q
- Operator
- Larocca, Victor T. · private individual
- Onboard fatalities
- Unknown
- Route
- From OM6 · Batesville, MSTo Beaumont Municipal Airport (BMT), Beaumont, TX
- 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 starvation; Stall/spin
- 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
- Pilot in command › Stall/spin, inadvertent
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
THE PRIVATE PILOT HAD PREVIOUSLY MADE ONLY ONE NIGHT CROSS-COUNTRY FLIGHT AS THE ONLY RATED PILOT IN THE AIRPLANE. ANOTHER PILOT WHO USUALLY SERVED AS A CREW MEMBER REPORTED THAT DURING THE CRUISE PORTION OF THE SECOND LEG OF HIS CROSS COUNTRY FLIGHT, THE PILOT WOULD NORMALLY RUN THE ENGINES ON THE AUXILIARY TANKS UNTIL THEY WERE EMPTY AND THEN SWITCH TO THE MAIN FUEL TANKS AND AIR START THE ENGINES. THIS PROCEDURE REQUIRES THAT THE FUEL BOOST PUMPS BE IN THE 'ON' POSITION. THE FUEL BOOST PUMPS WERE IN THE 'OFF' POSITION AT THE ACCIDENT SITE. THE RIGHT MAIN FUEL TANK HAD RUPTURED AND ONLY FOUR GALLONS OF FUEL REMAINED. TWENTY SEVEN GALLONS OF FUEL REMAINED IN THE LEFT MAIN TANK. EACH OF THE AUXILIARY TANKS CONTAINED LESS THAN ONE PINT OF FUEL. WITNESSES THREE MILES FROM THE ACCIDENT SITE REPORTED A DARK NIGHT. ENGINE TEST RUNS WERE PERFORMED ON BOTH ENGINES THROUGHOUT ALL POWER RANGES AND THERE WERE NO ANOMALIES FOUND THAT WOULD HAVE CONTRIBUTED TO THE ACCIDENT. A REVIEW OF THE AIR TRAFFIC CONTROL DATA REVEALED THAT THE PILOT DECLARED AN EMERGENCY AND REPORTED THE AIRPLANE OUT OF CONTROL IN A FLAT SPIN. THE PILOT DID NOT REFUEL PRIOR TO DEPARTING ON THE SECOND LEG OF HIS NIGHT CROSS COUNTRY FLIGHT.
Probable cause
THE INADVERTENT STALL AND SPIN. FACTORS WERE THE POWER LOSS DUE TO FUEL STARVATION, THE DARK NIGHT, AND HIS FAILURE TO USE THE BOOST PUMP FOR ENGINE RESTART.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record FTW93FA008
- Event ID
- 20001211X15859
- Case number
- FTW93FA008
- 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: local date, investigation status. Values present in the bulk record are kept.
- The date is the local date; the NTSB stores the UTC date 1992-10-08.
- API snapshot SHA-256: db6e9bd0d8af7d3bf7139906bea088959918829ac10bccafa62c4f440f3a5a57; retrieved 2026-09-21T00:52:16.105Z.