NTSB investigations: Piper PA-28-180
14 cases on aircraft the registry lists as Piper PA-28-180, where the defining event was Loss of engine power (partial). Aircraft are matched to the registry by N-number and event date, checked against the reported serial number, make and model, so older matches can be wrong.
Cases per year
| 2010 | 1 |
|---|---|
| 2011 | 2 |
| 2013 | 2 |
| 2014 | 2 |
| 2016 | 1 |
| 2020 | 2 |
| 2023 | 1 |
| 2024 | 1 |
| 2025 | 1 |
| 2026 | 1 |
Where
Open the mapLatest cases
Query with SQL
duckdb -csv -c "SELECT c.\"ntsbNumber\", c.\"eventDate\", c.\"eventType\", c.\"eventCity\", c.\"eventStateOrRegion\", a.n_number, a.\"aircraftMake\", a.\"aircraftModel\", c.\"highestInjuryLevel\", c.\"totalFatal\", c.\"completionStatus\", c.report_url
FROM 'https://openairdocs.org/data/latest/ntsb_case_detail.parquet' c LEFT JOIN 'https://openairdocs.org/data/latest/ntsb_aircrafts.parquet' a ON a.case_mkey = c.\"mKey\" AND a.position = 1
WHERE c.\"mKey\" IN (SELECT x.case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_aircrafts.parquet' x WHERE x.aircraft_model_code IN ('7102808')
AND EXISTS (SELECT 1 FROM 'https://openairdocs.org/data/latest/ntsb_events.parquet' e WHERE e.case_mkey = x.case_mkey AND e.aircrafts_position = x.position AND e.\"isDefiningEvent\" AND e.\"tier2Number\" = '342'))
ORDER BY c.\"eventDate\" DESC, c.\"ntsbNumber\" DESC"Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT c."ntsbNumber", c."eventDate", c."eventType", c."eventCity", c."eventStateOrRegion", a.n_number, a."aircraftMake", a."aircraftModel", c."highestInjuryLevel", c."totalFatal", c."completionStatus", c.report_url
FROM 'https://openairdocs.org/data/latest/ntsb_case_detail.parquet' c LEFT JOIN 'https://openairdocs.org/data/latest/ntsb_aircrafts.parquet' a ON a.case_mkey = c."mKey" AND a.position = 1
WHERE c."mKey" IN (SELECT x.case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_aircrafts.parquet' x WHERE x.aircraft_model_code IN ('7102808')
AND EXISTS (SELECT 1 FROM 'https://openairdocs.org/data/latest/ntsb_events.parquet' e WHERE e.case_mkey = x.case_mkey AND e.aircrafts_position = x.position AND e."isDefiningEvent" AND e."tier2Number" = '342'))
ORDER BY c."eventDate" DESC, c."ntsbNumber" DESCRun it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
NTSB CEN26LA265Accident · Minor injuriesClass 3 · LimitedPreliminary reportPiper PA-28-180 · Bulverde, TXOn July 20, 2026, about 1340 central daylight time, a Piper PA-28-180, N454MD was substantially damaged when it was involved in an accident near Bulberde, Texas. The flight instructor and student pilot received minor injuries. The airplane was operated as a…NTSB ANC25LA094Accident · Minor injuriesClass 3 · LimitedPreliminary reportPiper PA-28-180 · Chicken, AKOn August 24, 2025, about 0820 Alaska daylight time, a Piper PA-28-180 airplane, N7771N, was substantially damaged when it was involved in an accident near Chicken, Alaska. The pilot and one passenger sustained minor injuries; the second passenger was…NTSB WPR24LA178Accident · Minor injuriesClass 4 · LimitedFinal reportPiper PA-28-180 · Nephi, UTThe pilot’s incorrect movement of the fuel selector valve to an off or restricted position, which resulted in fuel starvation and a loss of engine power.NTSB ERA23LA264Accident · Minor injuriesClass 3 · LimitedFinal reportPiper PA28 · Lancaster, TNThe fatigue failure of an exhaust valve, resulting in a partial loss of engine power.NTSB WPR21LA020Accident · No injuriesClass 3 · LimitedFinal reportPiper PA-28-180 · Show Low, AZA partial loss of engine power due to the failure of the No. 4 cylinder exhaust valve.NTSB ERA20LA277Accident · Minor injuriesClass 3 · LimitedFinal reportPiper PA28 · St. Agatha, METhe failure of the crankshaft gear alignment dowel due to fatigue crack propagation and overstress, which resulted in a partial loss of engine power.NTSB CEN16LA349Accident · No injuriesLimited investigationFinal reportPiper PA 28-180 · Cuba, NMA partial loss of engine power for reasons that could not be determined based on available information.NTSB WPR15LA008Accident · Minor injuriesLimited investigationFinal reportPiper PA 28-180 · Bend, ORA partial loss of engine power due to carburetor icing, which resulted from the pilot’s failure to apply carburetor heat after takeoff and during the climb.NTSB WPR14LA249Accident · No injuriesLimited investigationFinal reportPiper PA 28-180 · Quincy, CAThe partial loss of engine power during takeoff due to the separation of the exhaust baffling, which resulted in a partial blockage of airflow to the engine. Contributing to the accident was maintenance personnel’s inadequate inspection of the exhaust system…NTSB WPR13LA384Accident · Serious injuriesLimited investigationFinal reportPiper PA 28 · Sacramento, CAA partial loss of engine power during initial climb for reasons that could not be determined because postaccident examination revealed no evidence of preimpact mechanical malfunction or failure that would have precluded normal operation.NTSB WPR13LA366Accident · No injuriesLimited investigationFinal reportPiper PA-28-180 · Overgaard, AZThe partial loss of engine power during takeoff due to the separation of the exhaust baffling, which resulted in a partial blockage of airflow. Contributing to the accident was inadequate maintenance of the exhaust system.NTSB CEN11CA678Accident · Minor injuriesData collectionFinal reportPiper PA-28-180 · Buena Vista, COThe airplane’s diminished climb performance due to the pilot not leaning the engine mixture enough prior to takeoff in high density altitude conditions and at nearly maximum gross takeoff weight.NTSB ERA11CA243Accident · No injuriesData collectionFinal reportPiper PA-28-180 · Latrobe, PAMaintenance personnel’s failure to properly secure the throttle cable to the fuel servo.NTSB ERA10LA306Accident · No injuriesLimited investigationFinal reportPiper PA-28-180 · Lucedale, MSThe partial separation of the No. 3 cylinder due to improper torquing of the cylinder hold-down bolts by maintenance personnel during installation of the cylinder.