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WPR24LA174 · Beech 35-C33A

1 Jun 2024 · San Diego, CA, United States

L A M Capital Management Beech 35-C33A · Accident: fuel contamination on approach

From Hollister Municipal Airport (CVH) to Montgomery-Gibbs Executive Airport (MYF)

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Event

NTSB case
WPR24LA174
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

Beech 35-C33A

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
N1259M
Onboard fatalities
Unknown
Route
From Hollister Municipal Airport (CVH), Hollister, CATo Montgomery-Gibbs Executive Airport (MYF), San Diego, CA
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
Approach · VFR pattern final
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

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 reported that, while approaching the destination airport at the conclusion of a cross-country flight with the fuel selector set to the fullest tank, the engine began to run rough and lost partial power. Unable to reach the runway, the airplane landed hard short of the runway, resulting in substantial damage.

A postaccident examination revealed no evidence of mechanical malfunction or failure. Fuel system continuity was confirmed, and a test run of the engine revealed no anomalies. The fuel strainer screen was removed and exhibited areas of corrosion. A water-detecting paste revealed the presence of water in the fuel. The fuel manifold was disassembled. The rubber diaphragm inside was brittle and exhibited peeling, and there were numerous rubber flakes found, but it could not be determined if the contaminants would have affected the operation of the unit. There was evidence of rust on the screen and in the cavity. The fuel strainer screen and the fuel cap (filler) receptacles also contained rust consistent with water in the fuel system. Although the investigation was unable to determine when the water was introduced into the fuel system, the presence of rust was consistent with long-term water exposure.

Given the successful engine test run and the lack of anomalies of the fuel system, and the corrosion observed on some fuel system components, it is likely that the loss of engine power was the result of water contamination of the fuel system.

Probable cause

A partial loss of engine power due to water contamination of the fuel system.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record WPR24LA174
Event ID
20240604194392
Case number
WPR24LA174
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: investigation status, coordinates, cause areas. 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: aff4b2cfff3da60da2bf3f3a45d8cd96c6a9d86af73140a26c2283633cf9c55c; retrieved 2026-09-16T18:51:05.124Z.