LAX01TA233 · Cessna 150
Cessna 150 · Accident: total loss of engine power (non-mechanical) en route
From Delano Municipal Airport (DLO) to an unrecorded destination
Event
- NTSB case
- LAX01TA233
- 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
Cessna 150
- Aircraft type
- Cessna 150
- 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
- N6475T
- Operator
- Randy L. Thompson · private individual
- Onboard fatalities
- Unknown
- Route
- From Delano Municipal Airport (DLO), Delano, CATo not recorded
- 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 exhaustion
- 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
- Fluid, fuel › Exhaustion
- Fuel system, carburetor › Excessive flow/output
- Mixture control › Bent
- Mixture control › Inoperative
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
The aircraft collided with grapevines and supporting trellises during a forced landing following a loss of engine power. According to the pilot, his passenger fueled the airplane prior to departure. They purposely waited until after they ate lunch and immediately before departure to refuel the airplane in order to obtain the maximum quantity of cool fuel. The passenger had flown about 40 photo missions with the pilot and was aware of the importance of fueling the airplane to maximum capacity. He assured the pilot that the fuel tanks were completely full. The accident occurred 3 hours 34 minutes after departure. The pilot stated that during recovery, 1/2-gallon of fuel was found in the airplane. The pilot also told the Safety Board investigator that he routinely flew the airplane 4 hours to 4 hours 5 minutes and it would require 20- to 20.5-gallons fuel to fill the tanks. The airplane holds 26 gallons fuel, of which 22.5 are usable fuel. The engine was test run and started promptly and ran smoothly. The magneto check and carburetor heat check were normal. The engine did not stop when the mixture control was moved to the idle cutoff position. The inspection revealed that the mixture control arm was loose on its shaft. The carburetor was examined and the mixture control valve stem shaft was found bent and was not inserted into the sleeve in the bowl. According to the representative from the carburetor manufacturer, the carburetor operates in the "full rich" condition at all times when the stem is not inserted in the sleeve and subsequent movement of the mixture control would have no effect. The examination also revealed that the mixture control lever was loose on the shaft and the stop peg traveled beyond the idle cutoff stop pad. The pilot/operator reported that no recent maintenance had been performed on the carburetor.
Probable cause
A bent mixture control valve stem shaft in the carburetor which made pilot control of the mixture inoperative resulting in excessive fuel consumption, and subsequent loss of engine power..
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record LAX01TA233
- Event ID
- 20010705X01308
- Case number
- LAX01TA233
- 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 2001-07-03.
- API snapshot SHA-256: 394677608f58115f778f0f746101d3780e47fa9d262351a30414eab7425fd6ee; retrieved 2026-09-22T11:48:31.546Z.