NTSB investigations: Lycoming I0360 SER A&C
29 cases on aircraft whose registry engine model is Lycoming I0360 SER A&C, where the first occurrence was “Airframe/component/system failure/malfunction”. 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
| 1983 | 2 |
|---|---|
| 1985 | 1 |
| 1986 | 2 |
| 1988 | 1 |
| 1990 | 2 |
| 1991 | 1 |
| 1993 | 3 |
| 1994 | 1 |
| 1996 | 1 |
| 1998 | 1 |
| 1999 | 1 |
| 2000 | 2 |
| 2002 | 3 |
| 2003 | 3 |
| 2004 | 1 |
| 2005 | 2 |
| 2006 | 1 |
| 2007 | 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.engine_model_code IN ('41511')
AND EXISTS (SELECT 1 FROM 'https://openairdocs.org/data/latest/ntsb_occurrences.parquet' o WHERE o.case_mkey = x.case_mkey AND o.aircrafts_position = x.position AND o.\"occurrenceNumber\" = 1 AND o.\"occurrenceCode\" = 130))
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.engine_model_code IN ('41511')
AND EXISTS (SELECT 1 FROM 'https://openairdocs.org/data/latest/ntsb_occurrences.parquet' o WHERE o.case_mkey = x.case_mkey AND o.aircrafts_position = x.position AND o."occurrenceNumber" = 1 AND o."occurrenceCode" = 130))
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 NYC08LA018Accident · No injuriesLimited investigationFinal reportBlair Skybolt · Guntersville, ALSeparation of the right tailwheel control link spring from the right control arm of the tailwheel, which resulted in a loss of control during landing.NTSB MIA06LA091Accident · Serious injuriesLimited investigationFinal reportCessna 172R · Fort Myers, FLThe flight instructor's failure to maintain airspeed while maneuvering, which resulted in an inadvertent stall. Contributing to the accident was a malfunction of the elevator control for an undetermined reason, which required excessive forward pressure on the…NTSB DFW05CA219Accident · No injuriesData collectionFinal reportCessna 172R · Springtown, TXThe pilot's improper decision to shut down the engine. Contributing factors were the failure of the oil pressure switch and the lack of a suitable landing area.NTSB LAX05LA270Accident · Serious injuriesLimited investigationFinal reportPrescott Aeronautical Pusher · Redding, CAthe in-flight separation of the propeller for undetermined reasons.NTSB ATL04CA154Accident · No injuriesData collectionFinal reportGlassic Composites SQ-2000 XL · Dayton, TNThe pilot's failure to maintain directional control during landing roll, which resulted in a ground loop and the subsequent collapse of the landing gear.NTSB FTW03LA173Accident · 1 fatalLimited investigationFinal reportApex CAP 10B · Gladewater, TXThe failure of the left wing, which resulted from progressive compressive fractures in the upper wooden spar cap. Contributing the accident was the difficulty in performing adequate inspections of the spar caps in an attempt to detect the compressive…NTSB ATL03FA064Accident · 2 fatalField investigationFinal reportCessna 172S · Monroe, GAThe pilot’s exceedence of the design limits of the airplane, which resulted in the overload failure of the horizontal stabilizers, followed by the overload separation of the right wing and subsequent loss of control.NTSB LAX03FA065Accident · Serious injuriesField investigationFinal reportPiper PA-34-200 · Westlake Villag, CAa fatigue crack in the propeller hub due to the inadequate design location of the grease fitting and the chamfering process.NTSB MIA02LA166Accident · No injuriesLimited investigationFinal reportBeech C24R · Olar, SCThe pilot's failure to execute the proper remedial action for hydraulic leak fumes in the cockpit, and his decision to perform an immediate precautionary landing to a vacant field, resulting in collision with a tree. A factor in the accident was the…NTSB NYC02LA071Accident · Minor injuriesLimited investigationFinal reportCirrus Design SR-20 · Lexington, KYThe pilot's failure to maintain aircraft control. Factors in this accident were the undetermined failure of the turn coordinator, as reported by the pilot, and the instrument meteorological conditions.NTSB ATL02IA065Incident · No injuriesIncident investigationFinal reportBeech C24R · Greenville, MSAn overload failure of the nose gear assembly for undetermined reasons.NTSB CHI01IA047Incident · No injuriesIncident investigationFinal reportCessna 172S · St. Cloud, MNthe fatigue failure of the propeller blade during the initial takeoff climb. The failure was a result of a material defect, which occurred during the manufacturing process and the manufacturers failure to detect the defect.NTSB DEN01LA014Accident · Minor injuriesLimited investigationFinal reportMooney M20J · Longmont, COthe total failure of the left main gear strut during the landing roll. A contributing factor was the 6-foot high snow bank that the airplane impacted when it left the runway.NTSB MIA99LA127Accident · No injuriesLimited investigationFinal reportLake LA-4-200 · Pensacola, FLThe pilot's inability to maintain directional control due to failure of the main landing gear, and partial electrical system failure for undetermined reasons.NTSB MIA98LA078Accident · No injuriesLimited investigationFinal reportLake LA-4-200 · Sarasota, FLinadequate clearance and fretting wear of the fitting/beam attachment to the angle/top beam, due to inadequate design, which resulted in fatigue and subsequent failure of the fitting/beam attachment ear.NTSB IAD96FA126Accident · 1 fatalField investigationFinal reportAerotek Pitts Special S-1S · Pittsburgh, PAThe pilot's utilization of airspeeds greater than the manufacturer recommended maneuvering airspeeds which exceed the design limits of the airplane and resulted in the subsequent failure of the wing spar.NTSB ATL94LA070Accident · No injuriesLimited investigationFinal reportMooney M20J · Muscle Shoals, ALWas the loose throttle cable, and the pilot's failure to abort the takeoff when the engine did not produce full power. A factor was the inadequate maintenance inspection of the engine.NTSB CHI94LA054Accident · No injuriesLimited investigationFinal reportPiper PA-28R-200 · Lacon, ILThe pilot misjudged the landing flare. Factors related to the accident were: the dark night, the pilot's lack of recent night experience, and the failure of the airplane's electrical system.NTSB SEA93LA172Accident · No injuriesLimited investigationFinal reportBeech 76 · Portland, ORJamming of the nose landing gear assembly and the pilot-in-command not maintaining the proper glidepath during the nose gear up landing.NTSB BFO93LA067Accident · No injuriesLimited investigationFinal reportPiper PA-28RT-201 · Willimantic, CTFailure of the pilot to follow emergency procedures to ensure that the gear was locked. A factor related to the accident was the total electrical failure and the construction site located beside the runway.NTSB ATL91LA144Accident · No injuriesLimited investigationFinal reportBeech C24R · Morrisville, NCFailure of the left main landing gear uplock cylinder which precluded extension of the landing gear.NTSB MIA90LA103Accident · No injuriesLimited investigationFinal reportSwing Velocity RG · Wimauma, FLDelamination of a portion of one of the wooden propeller blades at a knot, resulting in severe vibration and necessitating a forced landing.NTSB ATL90LA058Accident · No injuriesLimited investigationFinal reportBeech C24R · Greer, SCThe pilot in command's improper flare which resulted in a hard landing.NTSB CHI89FA009Accident · 2 fatalField investigationFinal reportMooney M20J · Ludington, MIThe pilot in command failed to maintain proper altitude utilizing basic flight instruments while experiencing a loss of gyro instruments.NTSB NYC86LA208Accident · Serious injuriesLimited investigationFinal reportBeech C24R · Hartford, CTThe Beech 24R pilot noticed a build-up of a substance on the windshield. He also experienced a problem controlling the propeller. He said upon landing he could not judge forward visibility and flared high (30-40 ft). The pilot reported that the aircraft…NTSB LAX86FA278Accident · 4 fatalField investigationFinal reportBeech C24R · Meyers, CAWith a density altitude of about 8400 ft, and an aircraft near its max certificated gross weight, the plt & 3 pax departed on rwy 18. During takeoff either the pilot's door was not closed or it came open. The open door degraded the acft's climb performance.…NTSB MIA86LA043Accident · No injuriesLimited investigationFinal reportLake LA4-200 · Homestead, FLThe plt stated that while on a flight from marco island FL, to ocean reef FL, he heard a loud bang and elected to land at Homestead general arpt. Upon landing he found the left muffler had seperated from the acft, struck the propeller and was driven through…NTSB DEN84FA042Accident · Serious injuriesField investigationFinal reportMooney M20J · Bismarck, NDThe plt of N1151N reported that the departure arpt had some drifting snow which caused the r brake to freeze after takeoff. When the acft was landed, the r tire slid until it wore thru, then deflated. The plt stopped the acft on the rwy, informed tower psnl…NTSB FTW84LA025Accident · No injuriesLimited investigationFinal reportBeech C24R · Prairie Grove, ARThe plt stated that about 15 min after takeoff, the radio & navigation equpment quit working. He decided to return to the arpt to land. However, when he tried to extend the gear, he could not get a safe gear down indication. There was heavy traffic, so he…