Schweizer 269C
NTSB investigations · 129
Matched to the registry by N-number and event date, newest first.
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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_aircrafts.parquet' a JOIN 'https://openairdocs.org/data/latest/ntsb_case_detail.parquet' c ON c.\"mKey\" = a.case_mkey
WHERE a.aircraft_model_code IN ('8059502')
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_aircrafts.parquet' a JOIN 'https://openairdocs.org/data/latest/ntsb_case_detail.parquet' c ON c."mKey" = a.case_mkey
WHERE a.aircraft_model_code IN ('8059502')
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 DFW07CA146Accident · No injuriesData collectionFinal reportSchweizer 269C · Slidell, LAThe pilot's encounter with settling with power condition while hovering out of ground effect. A contributing factor was the prevailing tailwind.NTSB CHI06CA168Accident · No injuriesData collectionFinal reportSchweizer 269C · Grand Forks, NDThe dual student's failure to maintain rotor speed during the recovery from the intentional autorotation and the flight instructor's delayed remedial action. Contributing factors were the flight crew's intentional autorotation and dual student's misjudged…NTSB CHI06TA148Accident · Minor injuriesFinal reportSchweizer 269C · Schererville, INThe pilot's improper autorotation following an actual loss of engine power during a practice autorotation, which resulted in a hard landing. A factor associated with the accident was the loss of engine power at the beginning of the practice autorotation for…NTSB SEA06LA096Accident · No injuriesLimited investigationFinal reportSchweizer 269C · Boise, IDThe reduction of the throttle to idle at a high density altitude during a practice autorotation, which resulted in the engine stoppage. Factors contributing to the accident included the instructor pilot's improper planning by not adhering to the flight…NTSB CHI06CA131Accident · No injuriesData collectionFinal reportSchweizer 269C · Lees Summit, MOThe flight instructor's delay in taking remedial action which led to the hard landing during the practice autorotation. The misjudged glide path, the dual student restricting the throttle control, and the trees were factors in the accident.NTSB NYC06LA106Accident · Minor injuriesLimited investigationFinal reportSchweizer 269C · Kings Park, NYLoss of engine power due to the failure of the number 3 connecting rod bearing. A contributing factor was the lack of suitable terrain for the emrgency landing.NTSB DFW06LA108Accident · Serious injuriesLimited investigationFinal reportSchweizer 269C · Denton, TXThe flight instructor's failure to maintain rotor RPM, resulting in a hard landing.NTSB CHI06TA033Accident · No injuriesFinal reportSchweizer 269C · Manhattan, KSThe binding of the main rotor blade's tachometer cable during cruise flight resulting in an observed split tachometer indication/aural alarm and perceived mechanical emergency and the unsuitable terrain the pilot encountered during the emergency landing. A…NTSB DEN05CA079Accident · No injuriesData collectionFinal reportSchweizer 269C · Pueblo, COthe student pilot's failure to maintain control of the helicopter during the landing. Contributing to the accident was the flight instructor's inadequate supervision of the student pilot.NTSB IAD05LA046Accident · Serious injuriesLimited investigationFinal reportSchweizer 269C · Leet, WVA fatigue fracture of the main transmission drive pinion. Also causal was the manufacturer's failure to remove the affected pinions from service during the period that transpired between the initial failures and the accident flight.NTSB LAX05LA050Accident · No injuriesLimited investigationFinal reportSchweizer 269C · Ontario, CAa loss of engine power due to the Designated Pilot Examiner's failure to follow the flight manual procedures and directives regarding throttle settings to be used for practice autorotations.NTSB MIA05CA006Accident · No injuriesData collectionFinal reportSchweizer 269C · Diamond Head, MSThe pilot's inadvertent loss of tail rotor effectiveness during takeoff to a hover and aborted landing in a grass area resulting in the grass catching fire from the engine exhaust and the helicopter being consumed by fire.NTSB SEA04LA146Accident · No injuriesLimited investigationFinal reportSchweizer 269C · Homedale, IDThe loss of engine power for an undetermined reason while maneuvering at low altitude, which resulted in a hard landing.NTSB SEA04LA128Accident · No injuriesLimited investigationFinal reportHughes 269C · Arlington, WAA significant power loss for undetermined reasons while in cruise flight, leading to a full autorotational landing. Factors include no suitable terrain in the area, and soft swampy terrain at the point where the pilot found it necessary to perform the forced…NTSB DEN04CA092Accident · No injuriesData collectionFinal reportSchweizer 269C · Englewood, COthe settling with power situation encountered by the pilot. Contributing to the accident was the high density altitude.NTSB IAD04LA013Accident · No injuriesLimited investigationFinal reportSchweizer 269C · Media, PAA lack of previous lubrication to the tail rotor drive shaft forward fitting teeth, which resulted in their gradual wear, the eventual slippage of the shaft, and the subsequent loss of tailrotor thrust and forced landing.NTSB CHI04LA015Accident · 1 fatalLimited investigationFinal reportSchweizer 269C · Fenton, MIThe intentional low altitude flight maneuvering and the ostentatious display by the pilot. The water was a factor to the accident.NTSB SEA03LA151Accident · No injuriesLimited investigationFinal reportHughes 269C · Snohomish, WAThe dual students failure to maintain clearance from the terrain during the go-around from a simulated autorotational flare, and the instructor pilot's failure to take adequate remedial action to keep the dual student from allowing the aircraft to impact the…NTSB DEN03LA115Accident · No injuriesLimited investigationFinal reportSchweizer 269C · Bountiful, UTthe pilot not maintaining aircraft control during the aerial taxi. Factors contributing to the accident were the oscillating cyclic, the pilot's diverted attention, and the gusting crosswind.NTSB NYC03LA106Accident · Minor injuriesLimited investigationFinal reportSchweizer 269C · New Canaan, CTThe inadequate annual inspection performed by maintenance facility personnel, which resulted in a failure of a fuel system bellcrank. Factors were the subsequent inadequate inspections by other maintenance personnel and the pilot.NTSB LAX03FA060Accident · 1 fatalField investigationFinal reportSchweizer 269C · Collinsville, CAA loss of engine power for undetermined reasons, and the pilot's failure to maintain main rotor rpm during the subsequent autorotation. A factor in the accident was the unsuitable nature of the terrain for a forced landing.NTSB LAX03LA052Accident · No injuriesLimited investigationFinal reportSchweizer 269C · Los Banos, CAThe improper engine overhaul by other maintenance personnel, which resulted in an exhaust valve failure and a total loss of engine power while in maneuvering flight.NTSB DEN02LA098Accident · No injuriesLimited investigationFinal reportSchweizer 269C · Broomfield, COmaintenance personnel's failure to secure the landing skid oleo strut bolt during the last 50-hour inspection, causing the left rear skid to collapse and the tail rotor to strike the ground.NTSB ATL02LA159Accident · Serious injuriesLimited investigationFinal reportSchweizer 300C · Haleyville, ALThe failure of maintenance personnel to perform an adequate inspection of loose intake components, which resulted in a total loss of engine power and subsequent emergency descent, forced landing, and collision with terrain in dark night conditions.NTSB LAX02LA161Accident · Minor injuriesLimited investigationFinal reportSchweizer 269C · Phoenix, AZthe CFI's failure to maintain an adequate airspeed resulted in a settling with power, and the CFI's failure to take remedial action. A factor in the accident was the high density altitude.NTSB LAX02LA137Accident · No injuriesLimited investigationFinal reportSchweizer 269C · Scottsdale, AZThe flight instructor's inadequate remedial action following the onset of ground resonance.NTSB NYC01LA206Accident · Minor injuriesLimited investigationFinal reportSchweizer 300C · Cicero, NYThe pilot's failure to maintain directional control while hovering, and the CFI's delayed remedial action.NTSB CHI01FA257Accident · 2 fatalField investigationFinal reportSchweizer 269C · Waterloo, INAircraft control not maintained for undetermined reasons.NTSB CHI01LA215Accident · Minor injuriesLimited investigationFinal reportSchweizer 269C · Walker, MNthe loss of engine power for undetermined reasons during takeoff. Factors were the vehicles, the unsuitable terrain the pilot encountered, and the low altitude of the helicopter at the time of the loss of engine power.NTSB LAX01LA121Accident · Minor injuriesLimited investigationFinal reportSchweizer 269C · Ojai, CAA loss of engine power for undetermined reasons.NTSB FTW01LA053Accident · No injuriesLimited investigationFinal reportSchweizer 269C · Damon, TXthe pilot's failure to maintain helicopter control during takeoff to a hover, which resulted in a dynamic rollover.NTSB FTW00LA216Accident · Minor injuriesLimited investigationFinal reportSchweizer 269C · Sherman, TXthe total failure of the clutch cable during landing, which resulted from fatigue cracking of the cable's individual wires.NTSB LAX00LA276Accident · No injuriesLimited investigationFinal reportSchweizer 269C · Cave Creek, AZThe pilot's inadequate in-flight planning/decision to attempt a hover in atmospheric conditions and over terrain that would require maximum helicopter performance, and which would leave no viable alternate actions in the event of difficulties.NTSB CHI00GA160Accident · 2 fatalFinal reportSchweizer 269C · Topeka, KSthe pilot's failure to maintain translational lift while maneuvering, and the loss of tail rotor effectiveness. Factors relating to this accident were the tailwind, low airspeed, low rotor rpm, and the pilot's lack of overall experience in helicopters.NTSB FTW00LA105Accident · No injuriesLimited investigationFinal reportSchweizer 300C · New Ulm, TXThe pilot's inadequate in-flight evaluation of the landing area, which resulted in the separation of the main rotor system as a result of foreign object damage.NTSB SEA99FA168Accident · 1 fatalField investigationFinal reportSchweizer 269C · Westport, ORThe pilot's failure to maintain clearance from terrain. Factors include low clouds and visibility and near-night light conditions.NTSB CHI99LA257Accident · No injuriesLimited investigationFinal reportSchweizer 269C · Jetmore, KSThe pilot's use of improper procedures by not following the helicopter manufacturer's recommended engine RPM reduction procedures during autorotations. A factor was the pilot not attaining the proper rotor RPM during the autorotation practice.NTSB NYC99LA082Accident · Serious injuriesLimited investigationFinal reportSchweizer 269C · Westerville, OHThe failure of the pilot to maintain control of the helicopter.NTSB IAD99GA013Accident · 1 fatalFinal reportSchweizer 269C · Baltimore, MDinadequate assembly instructions from the engine manufacturer which resulted in improper engine assembly, and subsequent power loss over unsuitable terrain, with insufficient altitude for a successful autorotation.NTSB CHI99LA006Accident · No injuriesLimited investigationFinal reportSchweizer 269C · Oshkosh, NEthe pilot's failure to maintain control of the helicopter. Factors associated with the accident were the high winds, low altitude at which the pilot was maneuvering and the uneven terrain which the helicopter contacted.NTSB CHI98LA332Accident · No injuriesLimited investigationFinal reportSchweizer 269C · Decker, INThe pilot's failure to maintain obstacle clearance resulting in a collision with a fence.NTSB FTW98LA279Accident · No injuriesLimited investigationFinal reportSchweizer 269C · San Angelo, TXThe improper touchdown executed by the flight instructor, which resulted in the tail rotor impacting the ground.NTSB ATL98LA065Accident · No injuriesLimited investigationFinal reportSchweizer 269C · San Juan, PRThe pilot's failure to adequately secure the cargo strap which became entangled in the tail rotor, leading to a loss of the tail rotor control. This was followed by an improperly executed emergency procedure and an in-flight collision with the ground. A…NTSB MIA98LA127Accident · No injuriesLimited investigationFinal reportSchweizer 269-C · Ormond Beach, FLThe CFI's inadequate supervision and poor communication which led the rated student pilot to roll the throttle off, and the CFI's subsequent failure to apply forward cyclic to increase airspeed which resulted in the subsequent hard landing and roll over.NTSB CHI98LA021Accident · No injuriesLimited investigationFinal reportSchweizer 269C · Grand Forks, NDthe pilot's inadequate preflight planning which resulted in a low fuel state, and his inability to see the wire which the helicopter contacted. Factors associated to the accident were the precautionary landing, the dark night conditions, and the wire which…NTSB NYC97GA148Accident · Serious injuriesFinal reportSchweizer 269C · Baltimore, MDA total loss of engine power which was a result of incomplete and improper engine overhaul by company maintenance personnel. A factor in the accident was the unsuitable forced landing area terrain.NTSB IAD97GA054Accident · No injuriesFinal reportSchweizer 269C · Cleveland, OHThe engine failure from the rod cap bolt being sheared and the separation of the number two cylinder separating from the crankcase.NTSB FTW96LA174Accident · No injuriesLimited investigationFinal reportSchweizer 269C · Silver, TXthe pilot's failure to maintain adequate rotor RPM.NTSB FTW96LA095Accident · No injuriesLimited investigationFinal reportSchweizer 269C · San Ygnacio, TXFailure of the rotor drive system clutch assembly (separation of the swedge ball from the end of the clutch control cable), which resulted in disengagement of the rotor drive system, while the helicopter was in lateral movement at low altitude.NTSB NYC95TA190Accident · Minor injuriesFinal reportSchweizer 269C · Baltimore, MDThe pilot's failure to maintain adequate terrain clearance which resulted in an inflight collision with the ground.
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