LAX06LA094 · Cessna T210N
Cessna T210N · Accident: total loss of engine power (mechanical failure) en route
From Visalia Municipal Airport (VIS) to Mariposa Yosemite Airport (MPI)
Event
- NTSB case
- LAX06LA094
- 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
- Instrument Meteorological Cond
Cessna T210N
- 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
- N4791C
- Operator
- Ross Rankin
- Onboard fatalities
- Unknown
- Route
- From Visalia Municipal Airport (VIS), Visalia, CATo Mariposa Yosemite Airport (MPI), Mariposa, 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 · 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 (mechanical failure)
- 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
- Engine assembly, cylinder › Separation
- Engine assembly, other › Loose part/bolt/nut/clamp/etc
- Other maintenance personnel › Maintenance, installation, inadequate
- Other maintenance personnel › Procedures/directives, not followed
Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.
NTSB narrative
The aircraft collided with multiple obstacles during a forced landing in rough terrain following a catastrophic engine failure. While en route about 6,000 feet mean sea level, one cylinder in the engine indicated a loss of exhaust gas and cylinder head temperature. Thereafter, an increasingly strong vibration was felt, oil dispersed onto the front windscreen, and all engine power was lost. During the landing flare, the airplane impacted an oak tree, a fence, and a rock outcrop. The engine was found separated from the airplane's firewall. Also, the number 6 cylinder was observed broken from the engine case. The engine was torn down and the case was opened. The evidence of the torque values found on all the engine through-bolts, combined with the fretting signature at the base of the number 6 cylinder, and the oil residue at the union of the case halves, indicates that when the cylinders were installed on the engine their respective bolts were inadequately torqued. During an interview with the mechanic who had replaced the 6 cylinders on the engine, he reported that he followed the instructions in TCM's maintenance manual when he had replaced the cylinders in May 2005. He said he torqued the nuts on the cylinders to about 500 inch pounds. According to TCM's maintenance manual, 1989 edition, the required torque for the through-bolts was 690 to 710 inch pounds. By 1996, TCM had revised its manual by issuance of service bulletin 96-7. In that bulletin the required torque was increased to between 790 to 810 inch pounds.
Probable cause
The failure of the maintenance personnel to follow the procedures in the TCM maintenance manual and adequately torque the engine through-bolts, which led to the separation of the No. 6 cylinder and the catastrophic failure of the engine.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record LAX06LA094
- Event ID
- 20060131X00141
- Case number
- LAX06LA094
- 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: 8790df02b3f64fd056de8ec688fc8fb27fd616882134dbdb7cfa264bba011733; retrieved 2026-09-21T18:50:02.150Z.