LAX01LA085 · Cessna T210M
Cessna T210M · Accident: total loss of engine power (non-mechanical) en route
From Healdsburg Municipal Airport (O31) to Willows Glenn County Airport (WLW)
Event
- NTSB case
- LAX01LA085
- 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 T210M
- Aircraft type
- Cessna 210
- 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
- N761SE
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From Healdsburg Municipal Airport (O31), Healdsburg, CATo Willows Glenn County Airport (WLW), Willows, 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
- En route · climb to 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)
- 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 › Emergency procedure, not complied with
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
The pilot reported that, during his preflight inspection of the aircraft, he noted the fuel gauges indicated about 25 gallons total fuel in the tanks, and, while looking in each of the two tanks and rocking the aircraft, he could hear sloshing and saw an irregular reflection. After takeoff, while climbing out at 120 - 130 knots and climbing 500 feet per minute, the airplane was near 4,000 feet msl when he felt the controls of the airplane get heavy. He had a headset on and couldn't hear the engine well. When he checked the instruments he saw that the engine tachometer was down to 1,200 rpm and the airspeed was slowing to below 100 knots. There was no roughness, no loud noise, and no sputtering from the engine. The engine continued to windmill. The airplane was on the right-hand fuel tank and he switched to the left tank. The throttle, propeller, and mixture controls were in the full forward position. He believed that he only turned on the low fuel boost pump switch position because he focused his attention outside the airplane on selecting a site and landing. The aircraft recovery company reported that, when they recovered the airplane, there was no fuel in the right tank and about 8 gallons fuel in the left tank (0.5 gallons of fuel in each tank is unusable). A postaccident examination of the aircraft did not reveal any mechanical abnormality. According to the Cessna Aircraft Company Pilot Operating Handbook for the model T210M (Emergency Procedures, Engine Failure During Flight), following loss of engine power, the pilot should; 1) switch to the fuller fuel tank, 2) place the mixture control in the full rich position, 3) turn the auxiliary fuel pump on for 3 - 5 seconds with the throttle 1/2 open, and 4) slowly advance the throttle. A Cessna Aircraft spokesman said that, if the throttle and mixture were full forward (full throttle and rich mixture) and the boost pump remained on while the engine was rotating at only 1,200 rpm, a flooded fuel condition was likely created in the engine which prevented restart.
Probable cause
The failure of the pilot to comply with emergency procedures contained in the Pilot's Operating Handbook, which resulted in an excessively rich mixture and loss of engine power.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record LAX01LA085
- Event ID
- 20010207X00414
- Case number
- LAX01LA085
- 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: ef226375b4b759cbe455e4357da9267c8f401d637da48cffa90b896e2f3db397; retrieved 2026-09-22T12:11:20.787Z.