NTSB investigations: Piper PA-28R-200
30 cases on aircraft the registry lists as Piper PA-28R-200, where the sequence of events included Off-field or emergency landing. 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
| 2008 | 3 |
|---|---|
| 2009 | 4 |
| 2010 | 2 |
| 2011 | 3 |
| 2012 | 2 |
| 2013 | 1 |
| 2015 | 1 |
| 2016 | 2 |
| 2017 | 4 |
| 2018 | 1 |
| 2019 | 4 |
| 2021 | 1 |
| 2022 | 1 |
| 2023 | 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 ('7102811')
AND EXISTS (SELECT 1 FROM 'https://openairdocs.org/data/latest/ntsb_events.parquet' s WHERE s.case_mkey = x.case_mkey AND s.aircrafts_position = x.position AND s.\"tier2Number\" = '440' AND s.case_mkey IN (SELECT case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_events.parquet' WHERE \"isDefiningEvent\")))
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 ('7102811')
AND EXISTS (SELECT 1 FROM 'https://openairdocs.org/data/latest/ntsb_events.parquet' s WHERE s.case_mkey = x.case_mkey AND s.aircrafts_position = x.position AND s."tier2Number" = '440' AND s.case_mkey IN (SELECT case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_events.parquet' WHERE "isDefiningEvent")))
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 WPR23LA094Accident · No injuriesClass 3 · LimitedFinal reportPiper PA28R · Carlsbad, CAA failure of the No. 2 piston connecting rod bearing due to oil starvation for reasons that could not be determined, which resulted in a complete loss of engine power.NTSB ERA22LA417Accident · Minor injuriesClass 3 · LimitedFinal reportPiper PA-28R-200 · Meridianville, ALA loss of engine power that could not be determined based on the available evidence.NTSB CEN21LA193Accident · Minor injuriesClass 3 · LimitedFinal reportPiper PA28R · McKinney, TXA total loss of engine power for reasons that could not be determined based on the available information.NTSB CEN20LA016Accident · Minor injuriesClass 3 · LimitedFinal reportPiper PA-28R-200 · Springtown, TXA total loss of engine power for undetermined reasons.NTSB WPR19LA136Accident · No injuriesClass 3 · LimitedFinal reportPiper PA28R · Winter Haven, FLA partial loss of engine power due to worn fuel valve O-rings, which allowed air into the fuel system and resulted in a forced landing to unsuitable terrain.NTSB CEN19LA132Accident · Serious injuriesClass 3 · LimitedFinal reportPiper PA28R · Prairieville, LAInstallation of an incorrect engine oil drain valve, which resulted in damage to the valve during landing gear retraction and subsequent engine failure due to oil starvation. Contributing to the accident was the failure of maintenance personnel to comply with…NTSB ERA19LA160Accident · No injuriesLimited investigationFinal reportPiper PA28R · Easton, MDThe loss of engine power for reasons that could not be determined because postaccident engine examination and testing revealed no preimpact mechanical malfunctions or failures that would have precluded normal operation.NTSB ERA18FA137Accident · 1 fatalField investigationFinal reportPiper PA28R · Gainesville, GAA partial loss of engine power due to inadequate thru-bolt and stud preload tension by undetermined maintenance personnel, which resulted in fretting between the engine crankcase halves, and the subsequent separation of the No. 2 cylinder due to the fatigue…NTSB ERA17LA300Accident · Minor injuriesLimited investigationFinal reportPiper PA 28R-200 · St. Augustine, FLA total loss of engine power for reasons that could not be determined because examination of the airplane and engine did not reveal evidence of any preimpact mechanical malfunctions or failures that would have precluded normal operation and because the amount…NTSB WPR17LA183Accident · Minor injuriesClass 3 · LimitedFinal reportPiper PA 28R-200 · West Jordan, UTThe pilot's failure to account for operation at high density altitude at or near the airplane’s maximum gross weight, which led to degraded engine performance and prevented the airplane from achieving an adequate airspeed for a positive rate of climb,…NTSB ERA17LA266Accident · No injuriesLimited investigationFinal reportPiper PA28R · Pembroke Pines, FLThe loss of engine power for reasons that could not be determined postaccident engine test-runs revealed no preimpact mechanical malfunctions or failures that would have precluded normal operation.NTSB ERA17LA110Accident · Serious injuriesLimited investigationFinal reportPiper PA28R · Bayonne, NJMaintenance personnel’s incorrect installation of the No. 3 cylinder’s hydraulic valve tappet plunger, which resulted in a failure of the No. 3 cylinder’s intake valve and the subsequent partial loss of engine power.NTSB ERA16LA276Accident · Minor injuriesLimited investigationFinal reportPiper PA28R · Panama City, FLA total loss of engine power during approach for reasons that could not be determined because postaccident examination did not reveal any evidence of preimpact mechanical malfunctions or failures that would have precluded normal operation.NTSB CEN16LA227Accident · No injuriesLimited investigationFinal reportPiper PA 28R-200 · Bowie, TXThe inadequate maintenance and inspection of the throttle control arm, which resulted in its in-flight separation and the subsequent loss of engine power.NTSB WPR15LA141Accident · Minor injuriesLimited investigationFinal reportPiper PA 28R-200 · Santa Maria, CAThe engine failure due to oil starvation, which resulted from the installation of an unapproved oil quick drain valve that subsequently led to the inadvertent draining of the oil when the nose landing gear was retracted. Contributing to the accident was the…NTSB ERA13LA111Accident · 1 fatalLimited investigationFinal reportPiper PA-28R-200 · Dover, DEThe pilot's failure to land the airplane at multiple airports that were equipped with adequate instrument approach procedures while operating in low instrument meteorological conditions and his delay in declaring a fuel-related emergency, which resulted in a…NTSB ERA13LA097Accident · Serious injuriesLimited investigationFinal reportPiper PA-28R-200 · Lock Haven, PAThe reinstallation of improper connecting rods at engine overhaul, which resulted in abnormal wear of the connecting rod bearings; while the bearings did not meet the manufacturer’s specifications, the use of the unapproved connecting rods more likely caused…NTSB ERA12LA267Accident · No injuriesLimited investigationFinal reportPiper PA-28R-200 · Eastover, SCInadequate or loss of through bolt preload tension, which resulted in fretting between the engine halves, the subsequent failure of one cylinder through bolt, the loosening of additional cylinder retaining studs, and the fracture of the crankcase.…NTSB WPR12FA058Accident · 1 fatalField investigationFinal reportPiper PA-28R-200 · Coupeville, WAThe total loss of engine power for reasons that could not be determined because postaccident examination of the airframe and engine did not reveal evidence of preaccident mechanical malfunctions or failures that would have precluded normal operation.NTSB CEN12FA025Accident · No injuriesField investigationFinal reportPiper PA-28R-200 · Watertown, WIThe separation of the number 2 connecting rod from the crankshaft for reasons that could not be determined during postaccident metallurgical examination, which ultimately resulted in a total loss of engine power.NTSB WPR11LA160Accident · No injuriesLimited investigationFinal reportPiper PA-28R-200 · Agoura Hills, CAThe loss of engine power during cruise flight for undetermined reasons.NTSB ERA10LA486Accident · No injuriesLimited investigationFinal reportPiper PA-28R-200 · Barnwell, SCThe failure of the No. 1 connecting rod end cap for undetermined reasons, which resulted in a total loss of engine power.NTSB WPR10LA165Accident · No injuriesLimited investigationFinal reportPiper PA-28R-200 · Eliza Island, WAThe total loss of engine power during cruise flight due to the failure of maintenance personnel to tighten a fitting on the propeller governor oil line, which resulted in a loss of engine oil and catastrophic engine failure.NTSB ERA10FA074Accident · 2 fatalField investigationFinal reportPiper PA-28R-200 · Wappinger, NYA total loss of engine power due to a delamination of the No. 3 connecting rod bearing. Contributing to the accident was the inadequate maintenance inspection of the engine oil system.NTSB ERA10LA073Accident · No injuriesLimited investigationFinal reportPiper PA-28R-200 · Hammonton, NJA total loss of engine power due to a blocked fuel vent.NTSB WPR09LA417Accident · No injuriesLimited investigationFinal reportPiper PA28R · Wendover, UTThe failure of the pilot to attain and maintain an airspeed sufficient for normal landing gear retraction during initial climb. Contributing to the accident was the pilot's failure to use the airplane's manual override landing gear system, misidentifying that…NTSB ERA09LA261Accident · No injuriesLimited investigationFinal reportPiper PA-28R-200 · Hilliard, FLA total loss of engine power due to the fatigue failure of the No. 3 cylinder attachment stud as a result of insufficient torque during installation. Contributing to the accident was the pilot’s operation of the airplane with a known mechanical deficiency.NTSB MIA08LA159Accident · No injuriesLimited investigationFinal reportPiper PA-28R-200 · West Kingston, RIThe pilot's misjudgment of speed and altitude while maneuvering to land during an emergency descent. Contributing to the accident was the partial loss of engine power.NTSB CHI08LA171Accident · Minor injuriesLimited investigationFinal reportPiper PA-28R-200 · Watseka, ILThe loss of engine power for undetermined reasons.NTSB NYC08LA086Accident · Minor injuriesLimited investigationFinal reportPiper PA-28-R200 · York, SCLoss of engine power due to improper welding of the crankcase, which resulted in fatigue failure of the through-studs and a subsequent separation of the number two cylinder. Contributing to the accident was the unsuitable terrain for a forced landing.