CEN15LA172 · Beech B19
Beech B19 · Accident: loss of engine power (total) en route
From Grand Glaize Osage Beach Airport (K15) to Creve Coeur Airport (1H0)
Event
- NTSB case
- CEN15LA172
- 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
Beech B19
- Aircraft type
- Beechcraft 19
- 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
- N774TA
- Operator
- GDS Properties
- Onboard fatalities
- Unknown
- Route
- From Grand Glaize Osage Beach Airport (K15), Grand Glaize, MOTo Creve Coeur Airport (1H0), St. Louis, MO
- Aircraft age
- About 39 years (built 1976)
- 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
- Defining eventThe 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
- Loss of engine power (total)
- 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
- Aircraft › Aircraft power plant
- Aircraft › Fluids/miscellaneous hardware
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
The pilot reported that, shortly after takeoff, he noticed that the oil pressure was dropping. Shortly after the oil pressure dropped, the engine seized, and the pilot subsequently ditched the airplane in a lake.
When the airplane was recovered, the oil dipstick was missing. However, more than 4 quarts of oil and only about 1 to 2 cups of water were drained from the engine. If the dipstick had not been in the engine at impact, the engine would have been full of water. Further, the pilot reported that he had replaced the dipstick after checking the oil; so, the dipstick likely was in place at impact. No signs of oil were found in the engine cowling, and no oil streaks were observed underneath the fuselage. A postaccident examination of the engine revealed that the crankshaft middle bearing had seized. The third bearing aft, which was between the two banks of cylinders, and the No. 3 connecting rod bearing had rotated and exhibited severe heat distress and mechanical damage. The No. 4 piston wrist pin plug was deformed, and the deformation had damaged the side of the piston. Aluminum pieces and shavings were found throughout the engine. It is likely that, as the No. 4 wrist pin plug wore down, its shavings entered the oil system and clogged the oil passages, which caused the engine to seize. The examination also revealed that the engine parts installed on the airplane, including the No. 4 piston wrist pin plug, were not approved by the engine manufacturer.
Probable cause
The failure of the No. 4 piston wrist pin plug and the subsequent entry of its metal shavings into the oil system, which clogged the oil passages and caused the engine to seize. Contributing to the accident was the installation of engine parts that were not approved by the engine manufacturer.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record CEN15LA172
- Event ID
- 20150316X21312
- Case number
- CEN15LA172
- Dataset
- full-current
- Source SHA-256
- 5cf380f0061817c0331a6b2d8cc7e0ee3a79bea469a1001dc5c10e56f35f5ab3
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: 8f68f3faef47c1348b80521533712325e48cbe02ded9935951e6a7ab8770e522; retrieved 2026-09-16T02:09:20.196Z.