ERA17LA128 · Piper PA28 140
Piper PA28 140 · Accident: loss of engine power (partial) during initial climb
From Peter O Knight Airport (TPF) to Sebastian Municipal Airport (X26)
Event
- NTSB case
- ERA17LA128
- 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 140
- 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
- N8447R
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From Peter O Knight Airport (TPF), Tampa, FLTo Sebastian Municipal Airport (X26), Sebastian, FL
- Aircraft age
- About 51 years (built 1966)
- 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 (partial)
- 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 handling/service
- Aircraft › Aircraft power plant
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
The private pilot stated that he rented the airplane 2 days before the accident flight to fly across the state for several days. On the day of the accident, the pilot performed a preflight inspection of the airplane with no anomalies noted. After takeoff and during the initial climb, the pilot noticed a loss of engine power, and the rpm started to drop. He attempted to return to the departure airport and land on an intersecting runway, but during the turn, he realized he would not make it back to the airport; he ditched the airplane into the surrounding water. The airplane was substantially damaged during the ditching.
Postaccident examination of the airplane revealed that the induction duct from the air filter to the carburetor had collapsed, which likely restricted air flow to the engine and ultimately resulted in the loss of engine power. Further examination revealed that the induction duct on the accident airplane was not approved for installation on the engine. About 3 years before the accident, the Federal Aviation Administration had issued a special airworthiness information bulletin recommending operators inspect airplanes of this model to ensure that the correct induction duct was installed; that there was no loose or displaced supporting wire or signs of wear, perforation, or deterioration; and that the part had not collapsed. However, the operator was unaware of the bulletin and had not performed the inspection. After the accident, the operator inspected the fleet and installed the approved part on all affected airplanes.
Probable cause
A collapsed engine induction duct, which resulted in restricted air flow to the engine and a subsequent loss of engine power. Contributing to the accident was the operator's failure to ensure that the correct induction duct was installed.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record ERA17LA128
- Event ID
- 20170313X22258
- Case number
- ERA17LA128
- 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: c5f40aa28b45a0092d552d62f10c1e497417bb5d4d99e5864228513400972d3c; retrieved 2026-09-16T05:05:26.699Z.