ERA17LA278 · Piper PA28 180
Piper PA28 180 · Accident: powerplant system/component malfunction/failure en route
From Hilliard Airpark (01J) to Lee Gilmer Memorial Airport (GVL)
Event
- NTSB case
- ERA17LA278
- 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 PA28 180
- 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
- N6653J
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From Hilliard Airpark (01J), Hilliard, FLTo Lee Gilmer Memorial Airport (GVL), Gainesville, GA
- Aircraft age
- About 49 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
- 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
- Powerplant system/component malfunction/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
- Aircraft › Aircraft power plant
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
The private pilot was conducting a solo cross-country personal flight. The pilot reported that, when the airplane was about 10 miles from the destination airport, he moved the mixture control handle and that it felt like it caught on something. He pushed on the handle harder until it moved to full rich, but the engine power reduced to idle. He added that, while attempting to troubleshoot the problem by moving the mixture control handle back to the point where he thought it had gotten caught to see if would happen again, he heard a "pop" sound, followed by a partial loss of engine power. His attempts to restore engine power were unsuccessful. He then maneuvered the airplane for a forced landing in a field, during which the left wing sustained substantial damage.
Postaccident examination of the engine compartment by the pilot, who was also a certificated mechanic and had performed the airplane's last 100-hour inspection, revealed that the mixture control cable had separated from the mixture control lever at the carburetor. The attachment hardware was not recovered. The pilot reported that, when he inspected the engine controls at the carburetor during the 100-hour inspection (about 30 to 40 flight hours before the accident flight), they were all properly secured. No maintenance was conducted on the mixture control at the carburetor after the inspection was completed. The separation of the mixture control cable from the mixture control lever at the carburetor likely resulted in the partial loss of engine power. The reason for the separation of the mixture control cable from the mixture control lever at the carburetor could not be determined because the attachment hardware was not recovered.
Probable cause
The separation of the mixture control cable from the mixture control lever at the carburetor, which resulted in the partial loss of engine power.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record ERA17LA278
- Event ID
- 20170816X91808
- Case number
- ERA17LA278
- 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: 052fc8f303f4d44f2c0db70fab6f10a3701b5cc0477d2a014ad4406068a93e84; retrieved 2026-09-16T05:42:52.477Z.