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LAX94FA354 · Stinson 108-3

5 Sept 1994 · Shelter Cove, CA, United States

Stinson 108-3 · Accident: total loss of engine power (non-mechanical) during initial climb

From an unrecorded airport to Lodi Airport (1O3)

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Event

NTSB case
LAX94FA354
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
4 · 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

Stinson 108-3

Aircraft type
Stinson 108
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
N6446M
Operator
Gary D. Murdock · private individual
Onboard fatalities
Unknown
Route
From not recordedTo Lodi Airport (1O3), Lodi, CA
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
Initial climb
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
Destroyed

Cause areas

  • Fluid, fuel › Starvation
  • Pilot in command › Aircraft preflight, inadequate
  • Pilot in command › Airspeed, not maintained
  • Pilot in command › Fuel tank selector position, improper
  • Pilot in command › Stall/spin, inadvertent

Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.

NTSB narrative

IMMEDIATELY AFTER THE AIRPLANE TOOK OFF, WITNESSES HEARD AN ABNORMAL SOUND FROM THE ENGINE, AND THEN THE ENGINE SOUND STOPPED MOMENTARILY AND RESUMED. THE AIRCRAFT ENTERED A RIGHT 180-DEGREE TURN. WHILE IN THE TURN, ANOTHER POWER INTERRUPTION OCCURRED BEFORE THE ENGINE STOPPED COMPLETELY. GROUND WITNESSES SAID THAT AFTER THE FINAL ENGINE STOPPAGE, THE AIRCRAFT STALLED AND SPUN INTO THE SHORELINE. HIGH TIDE CAUSED THE AIRPLANE TO SHIFT BEFORE IT WAS INSPECTED. THE FUEL PRIMER CONTROL WAS FOUND UNLOCKED AND EXTENDED. THE FUEL SELECTOR WAS FOUND POSITIONED TO THE RIGHT TANK. ALTHOUGH BOTH MAIN FUEL TANKS HAD RUPTURED ON IMPACT, THERE WAS SIGNIFICANTLY MORE FIRE DAMAGE AND HYDRAULIC DEFORMATION ASSOCIATED WITH THE RIGHT MAIN TANK THAN THE LEFT. A COMPUTATION OF FUEL CONSUMPTION INDICATED THAT ABOUT 23 GALLONS OF FUEL HAD BEEN USED SINCE THE AIRPLANE WAS LAST REFUELED. THE CAPACITY OF EACH TANK WAS 23 GALLONS OF USABLE FUEL. NO PREIMPACT MECHANICAL FAILURE WAS FOUND.

Probable cause

INADEQUATE PREFLIGHT BY THE PILOT, WHICH RESULTED IN FUEL STARVATION AND LOSS OF ENGINE POWER, IMPROPER (OR DELAYED) POSITIONING OF THE FUEL SELECTOR TO THE FULLEST TANK, AND FAILURE OF THE PILOT TO MAINTAIN ADEQUATE AIRSPEED, WHILE MANEUVERING FOR A FORCED LANDING, WHICH RESULTED IN A STALL/SPIN AND COLLISION WITH TERRAIN.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record LAX94FA354
Event ID
20001206X02271
Case number
LAX94FA354
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: 062f5023be33b7f1cb36d7630c0c9e4bedc17e714f040df7f4a7ee95b569676f; retrieved 2026-09-21T00:01:11.002Z.