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ERA17LA278 · Piper PA28 180

7 Jul 2017 · Gainsville, GA, United States

Piper PA28 180 · Accident: powerplant system/component malfunction/failure en route

From Hilliard Airpark (01J) to Lee Gilmer Memorial Airport (GVL)

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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.