ERA16LA053 · Piper PA-32 260
Piper PA-32 260 · Accident: loss of engine power (total) during initial climb
From Miami-Opa Locka Executive Airport (KOPF) to South Bimini Airport (MYBS)
Narrative check · The NTSB narrative appears to contradict this record's departure or destination. Values are shown as recorded, not corrected; compare with the narrative.
Event
- NTSB case
- ERA16LA053
- 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 PA-32 260
- Aircraft type
- Piper PA-32
- 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
- N5568J
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route Narrative disagrees
- From Miami-Opa Locka Executive Airport (KOPF), Opa Locka, FLTo South Bimini Airport (MYBS), South Bimini, AO
- Aircraft age
- About 47 years (built 1968)
- 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
- 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
- Personnel issues › Task performance
Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.
NTSB narrative
The private pilot stated that the airplane was climbing through about 800 ft after takeoff when light smoke appeared from the instrument panel and windscreen area. The pilot began a turn back toward the airport, and, almost immediately, the engine experienced a total loss of power. The pilot performed an off-airport forced landing, the airplane struck a parked tractor-trailer, and came to rest inverted on a berm.
Subsequent examination of the airplane revealed soot and char marks on the left side of the engine cowling and in the engine compartment. The muffler's left sidewall displayed metal erosion and a wall breach that allowed exhaust gas to leak into the engine compartment. The engine fuel lines exhibited thermal damage but were not compromised. The front of the carburetor was charred, and some magneto leads were burned. The exact means by which the engine lost power could not be determined, but the intense heat of the exhaust gas could have burned off fuel in the carburetor, created a vapor lock in the fuel lines, or interrupted spark to the cylinders.
Further examination of the muffler revealed that the right sidewall was thin and rusted and had small erosion holes. The accident occurred less than 8 hours of operation after the airplane's most recent annual/100-hour inspection. Manufacturer-mandated inspection criteria required particular attention be paid to the exhaust system, especially fatigue-prone areas such as the muffler sidewalls. Given the degree of preexisting deterioration noted, it is likely that the exhaust system was not properly inspected during the last inspection.
Probable cause
Maintenance personnel's inadequate inspection of the exhaust system, which resulted in the escape of exhaust gases into the engine compartment and a subsequent total loss of engine power.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record ERA16LA053
- Event ID
- 20151201X30530
- Case number
- ERA16LA053
- 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. 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: d6d0d8c08dca4d7a19f119191c6fcf9135e9a798c8f92f0895eb1def20ebae06; retrieved 2026-09-16T02:59:59.015Z.