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MIA04LA082 · Beech K35

12 May 2004 · Lake Worth, FL, United States

Beech K35 · Accident: loss of engine power on approach

From Fort Lauderdale Executive Airport (FXE) to Palm Beach County Park Airport (LNA)

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Event

NTSB case
MIA04LA082
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

Beech K35

Aircraft type
Beechcraft 35
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
N551PK
Operator
Unknown
Onboard fatalities
Unknown
Route
From Fort Lauderdale Executive Airport (FXE), Fort Lauderdale, FLTo Palm Beach County Park Airport (LNA), Lake Worth, 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
Approach · VFR pattern base
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
Loss of engine power
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

  • Reason for occurrence undetermined

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 stated that while flying the downwind leg at Palm Beach County Park Airport, he conducted a pre-landing checklist, which included extending the landing gear and lowering the flaps. After leveling the wings following the turn from downwind leg to the base leg, he attempted to increase power but the engine was unresponsive. He said that upon realizing the engine was not producing power, he also noticed the fuel flow was low. At this point, he cycled the magneto switch, switched fuel tanks, turned on the fuel boost pump to "low" but there was no change in the fuel flow. He then turned toward the airport, realized he was not going to make the runway, and elected to land on a golf course driving range north of the airport. The pilot further stated the landing went well but during the landing rollout, the aircraft hit a berm and nosed over coming to rest inverted. During recovery of the airplane, the main fuel tanks were found to contain about 15 gallons of fuel in each. The auxiliary tanks contained about 5 gallons of fuel in each and the right tip tank contained 1 gallon of fuel. The left tip tank had been damaged by impact forces and contained no fuel. The fuel selector, magneto switch, and electrical master switch were found in the off position. Fire department personnel reported they turned off the fuel selector, magneto, and electrical master switches after the accident. No contamination was found in the airframe and engine fuel systems. All fuel lines were unobstructed. After recovery of the airplane, which required removal of the airplanes wings, a fuel supply was connected to the airplane and engine fuel system. The engine was then started and operated to full power with no evidence of failure or malfunction. During the engine test run the electric fuel boost pump was moved from the off position to the low position. The engine began to fail. The boost pump was turned off and the engine regained power. The electric fuel boost pump was tested and found to produce pressures within the normal range in the low and high positions. The flight manual for the Beech K35 states that the electric boost pump is used for starting and emergency operation after failure of the engine driven fuel pump.

Probable cause

The loss of engine power for undetermined reasons which resulted in a forced landing, collision with a berm during landing rollout, and the airplane nosing over.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record MIA04LA082
Event ID
20040520X00618
Case number
MIA04LA082
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: a3beb169394a201a23c55fa95ec318fc63e09a07238c7c66fbab08cc8f165e4a; retrieved 2026-09-21T09:17:32.891Z.