LAX06FA129 · Beech A36
Beech A36 · Accident: total loss of engine power (mechanical failure) during initial climb
From Santa Monica Municipal Airport (SMO) to Brown Field Municipal Airport (SDM)
Event
- NTSB case
- LAX06FA129
- 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
- 2 · 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
Beech A36
- Aircraft type
- Beechcraft 36
- 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
- N16JR
- Operator
- Peter Tomarken
- Onboard fatalities
- Unknown
- Route
- From Santa Monica Municipal Airport (SMO), Santa Monica, CATo Brown Field Municipal Airport (SDM), San Diego, 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 (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, connecting rod › Separation
- Other maintenance personnel › Maintenance, annual inspection, inadequate
Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.
NTSB narrative
The engine lost power during the takeoff-initial climb and the pilot ditched the airplane in the ocean. Examination showed that the number 2 connecting rod fractured from the crankshaft. Metallurgical examination of the connecting rod, and associated bolts, nuts, and bearings, showed that following the first nut and bolt separation, the overall separation was not instantaneous. After the first nut unthreaded from its respective bolt, subsequent increased loads on the opposite bolt then stripped the threads of the other nut that had partially unthreaded from its bolt. Furthermore, there was no evidence of cotter pin installation. In general, a properly torqued nut and connecting rod bolt will not loosen under normal operational conditions. The engine underwent a field overhaul 735.31 hours prior to the accident. At 233.59 hours prior to the accident, the cylinders were removed for a blow by condition during an annual inspection; however, the aviation maintenance technician who performed this work stated that he did not remove the connecting rods from the crankshaft. Review of the autopsy results and impact damage to the wreckage indicated that the occupants' use of shoulder harnesses would have significantly increased their chances of survival.
Probable cause
The failure of an aviation maintenance technician to properly torque and cotter pin the number 2 connecting rod bolts at their attach point to the crankshaft, which resulted in the separation of the connecting rod in flight, and complete power loss.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record LAX06FA129
- Event ID
- 20060317X00321
- Case number
- LAX06FA129
- 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: 17a9bb4e317564629fff3233312c3618dc5c560fc2e14e4163fb6b20cce699ac; retrieved 2026-09-20T17:30:01.295Z.