WPR23LA094 · Piper PA28R 200
Piper PA28R 200 · Accident: loss of engine power (total) en route
From Montgomery-Gibbs Executive Airport (MYF) to John Wayne Orange County International Airport (SNA)
Event
- NTSB case
- WPR23LA094
- 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
Piper PA28R 200
- Aircraft type
- Piper PA28
- 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
- N57355
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From Montgomery-Gibbs Executive Airport (MYF), San Diego, CATo John Wayne Orange County International Airport (SNA), Santa Ana, CA
- Aircraft age
- About 49 years (built 1974)
- 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
- 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
- Not determined › Not determined
Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.
NTSB narrative
The flight instructor was conducting an instructional flight when the accident occurred. During the takeoff climb, the pilots observed an abnormal oil pressure indication and elected to return to the airport. As they were returning to the airport, there was a complete loss of engine oil pressure followed by a total loss of engine power. Unable to maintain altitude, the pilots elected to make a water landing. The pilot receiving instruction flew the airplane to the surface. The flight instructor notified air traffic control (ATC) of the engine failure and intended landing site. They touched down about 50 yards from the shoreline with the landing gear up and were able to egress from the airplane as it floated
Postaccident examination of the engine revealed that the engine case was breached between the pushrod tubes of the No. 2 cylinder, showing a visible puncture along the pushrod tube channel. Internal examination of the engine revealed that the No. 2 connecting rod separated from the crankshaft. Thermal damage was observed along the shank of the No. 2 cylinder connecting rod. The No. 2 connecting rod bearing had separated from the journal, which was mechanically damaged. A remaining section of the No. 2 connecting rod end cap displayed score marks consistent with interfacing at the No. 2 crankshaft journal. Internal thermal discoloration and damage identified during the engine teardown were consistent with a lack of oil. While it’s likely that lubrication deprivation resulted in a total loss of engine power, a blockage or malfunction of the oil system could not be located due to engine damage that resulted from being submerged in salt water.
Probable cause
A failure of the No. 2 piston connecting rod bearing due to oil starvation for reasons that could not be determined, which resulted in a complete loss of engine power.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record WPR23LA094
- Event ID
- 20230119106604
- Case number
- WPR23LA094
- 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, coordinates, cause areas. 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: 2d6307bcf1aa5068ecb608ef74d4d1e76420f3a76531ad3f5607c1eb6a7181d4; retrieved 2026-09-16T17:15:49.485Z.