ERA17FA210 · Piper PA28 181
Piper PA28 181 · Accident: loss of engine power (total) during initial climb
From Page Field (FMY) to Dunnellon Marion Co & Park of Commerce Airport (X35)
Event
- NTSB case
- ERA17FA210
- 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
- 1 · 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 181
- 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
- N199PA
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From Page Field (FMY), Fort Myers, FLTo Dunnellon Marion Co & Park of Commerce Airport (X35), Dunnellon, FL
- Aircraft age
- About 18 years (built 1999)
- 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
- Destroyed
Cause areas
- Not determined › Not determined
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
The private pilot and passenger were departing on a cross-country flight. Shortly after takeoff, the engine experienced a partial loss of power and the airplane would not climb. The pilot chose to perform a forced landing to a road, during which the airplane impacted a building, then the ground; a postimpact fire ensued.
The airplane was operated by a flying club. On two separate occasions before the accident, two different pilots experienced a loss of engine power in the accident airplane. About 1 month before the accident, a pilot experienced a partial loss of engine power shortly after takeoff; he subsequently landed the airplane on the remaining runway. Following that incident, a maintenance inspection revealed no anomalies. Maintenance personnel flushed both right and left fuel tanks, installed new fuel cap seals, drained the carburetor fuel bowl, cleaned and inspected the fuel filter, and flushed the fuel lines. A subsequent test run of the engine revealed no anomalies. Another pilot reported that, about 2 weeks before the accident, while in cruise flight at 8,000 ft, the engine experienced a total loss of power. The pilot was able to restart the engine at an altitude of 3,000 ft and uneventfully performed a precautionary landing. A subsequent maintenance inspection did not reveal any anomalies.
Postaccident examination of the engine did not reveal any preimpact mechanical malfunctions. Continuity of the crankshaft and camshaft were observed during manual rotation of the engine and the interiors of each cylinder revealed no anomalies. However, postimpact fire damage precluded a thorough examination of the ignition, fuel, and induction systems, and the reason for the partial loss of engine power could not be determined based on the available information.
Probable cause
A partial loss of engine power during initial climb for reasons that could not be determined because extensive fire damage precluded thorough examination of the engine and its associated systems.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record ERA17FA210
- Event ID
- 20170624X93152
- Case number
- ERA17FA210
- 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: e665160015ad899f7287d256648640eac119a1212b3066ae51c4784a75303e0b; retrieved 2026-09-15T06:04:42.598Z.