ERA16LA071 · Piper PA-32 300
KDK Associates Piper PA-32 300 · Accident: loss of engine power (total) en route
From Jacksonville Executive at Craig Airport (CRG) to Rock Hill - York County Airport (UZA)
Event
- NTSB case
- ERA16LA071
- 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-32 300
- 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
- N8675N
- Operator
- KDK Associates
- Onboard fatalities
- Unknown
- Route
- From Jacksonville Executive at Craig Airport (CRG), Jacksonville, FLTo Rock Hill - York County Airport (UZA), Rock Hill, SC
- Aircraft age
- About 44 years (built 1971)
- 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
- 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 was conducting a personal cross-country flight. The pilot reported that the airplane was in cruise flight at 7,500 ft mean sea level when, without any warning, there was a loud explosion from the engine and an immediate loss of engine power. The explosion caused the oil filler door to open, and oil subsequently spewed over the windshield, and smoke filled the cockpit. The pilot declared an emergency and attempted to glide to a nearby airport; however, he landed the airplane on a rooftop a few hundred yards short of the runway.
Examination of the engine revealed that the No. 4 cylinder had separated from the engine case. All of the No.4 cylinder mounting stubs and through bolts were fractured except for the bottom forward stub; the nut for this stub was not located. The piston and corresponding connecting rod for the No. 4 cylinder were found in the bottom of the engine cowling.
A review of the engine maintenance logbooks revealed that the engine was overhauled almost 8 years before the accident and had accrued a total time of 1,005.0 hours since overhaul. There were no subsequent maintenance entries related to the No. 4 cylinder. Based on the evidence, it is likely that maintenance personnel applied insufficient torque to the cylinder's bottom forward hold-down nut, which allowed it to loosen over time. The stress load was then transferred to the remaining nuts, which resulted in the failure of the stubs and through bolts and to the separation of the No. 4 cylinder.
Probable cause
Maintenance personnel's failure to properly torque a No. 4 cylinder hold-down nut during engine overhaul, which resulted in the loosening of the nut and the subsequent failure of the studs and through bolts and separation of the cylinder.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record ERA16LA071
- Event ID
- 20151217X13937
- Case number
- ERA16LA071
- 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: db3ea555b1c1c3cbc5ad4fbbeb367fc78f5943fe5b081fdf0fc4ddcd6f35a020; retrieved 2026-09-16T03:02:21.858Z.