NTSB investigations
654 cases where NTSB found Aircraft structures.
Cases, newest first
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 f.case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_findings.parquet' f WHERE starts_with(f.\"findingCode\", '0103')) 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 f.case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_findings.parquet' f WHERE starts_with(f."findingCode", '0103')) ORDER BY c."eventDate" DESC, c."ntsbNumber" DESC
Run 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 ERA22LA171Accident · No injuriesClass 3 · LimitedFinal reportCessna 172 · Sparta, TNMaintenance personnel’s failure to properly affix left main landing gear components, which led to the failure of the left main landing gear during the accident flight.NTSB ERA22LA124Accident · No injuriesClass 4 · LimitedFinal reportCessna 172RG · Rocky Mount, NCAn inflight collision with a bird, which resulted in substantial damage to the left wing.NTSB ERA22LA116Accident · No injuriesClass 4 · LimitedFinal reportDehavilland DHC-2 · Gilbert, SCThe pilot’s improper flap setting, which resulted in a collision with trees during a takeoff attempt from a short grass field.NTSB ERA22FA095Accident · 2 fatalClass 3 · FieldFinal reportMooney M20J · Jacksonville, FLThe pilot’s failure to maintain airspeed during initial climb, which resulted in an aerodynamic stall/spin. Contributing was the pilot’s likely distraction due to the opening of the baggage door.NTSB CEN22FA070Accident · 1 fatalClass 3 · FieldFinal reportCessna 310J · Inola, OKThe loss of airplane control for reasons that could not be determined based on the available evidence.NTSB ERA22LA084Accident · No injuriesClass 4 · LimitedFinal reportCessna 172S · Midland, VACollision with a bird in flight, which resulted in damage to the right-wing leading-edge spar.NTSB DCA22LA038Accident · No injuriesClass 4 · LimitedFinal reportBoeing 747-4B5F · Miami, FLIncorrect lubrication of the foreflap fitting assembly.NTSB WPR22FA048Accident · 1 fatalClass 3 · FieldFinal reportZenith Zodiac CH601XL · Temecula, CAThe failure of the airplane’s canopy latch system, which resulted in the canopy opening in flight and a loss of airplane control. Contributing to the accident was the lack of a secondary canopy latch as recommended by the kit manufacturer.NTSB ERA22FA036Accident · 1 fatalClass 3 · FieldFinal reportVans RV4 · Chattahoochee, FLThe pilot’s failure to properly secure the canopy before takeoff, allowing the canopy to open and then separate in flight, which resulted in the pilot’s failure to maintain control of the airplane for reasons that could not be determined based on the…NTSB ERA22FA009Accident · 4 fatalClass 3 · FieldFinal reportCessna P210 · Atlanta, GAThe pilot’s failure to ensure that his seat was properly secured before initiating the takeoff, which resulted in a loss of control during the initial climb. Contributing to the accident was the lack of an installed secondary seat stop, and the airplane’s aft…NTSB CEN22LA006Accident · Minor injuriesClass 4 · LimitedFinal reportRobinson Helicopter R66 · Delta, MOThe pilot’s inadequate inflight planning and his failure to see and avoid a wire which resulted in contact with the wire and subsequent ground impact.NTSB ERA21LA379Accident · No injuriesClass 3 · LimitedFinal reportHawker Beechcraft 400A · Charleston, SCThe in-flight separation of the left engine’s four-panel cowling for reasons that could not be determined based on the available evidence.NTSB CEN21LA420Accident · Minor injuriesClass 3 · LimitedFinal reportQuad City Ultralight Challenger II · Rogers City, MIThe separation of the right wing’s forward lift strut from the fuselage due to a missing nylon-insert lock nut. Contributing to the accident was the noncertificated pilot’s decision to operate the airplane even though a condition inspection had not been…NTSB WPR21LA324Accident · No injuriesClass 4 · LimitedFinal reportCessna 172 · Athol, IDThe failure of the windshield during spin recovery for reasons that were not determined.NTSB CEN21FA360Accident · 3 fatalClass 3 · FieldFinal reportMooney M20M · Victoria, MNThe pilot’s loss of airplane control due to spatial disorientation during final approach, which led to a spiral dive that overstressed the airplane and resulted in an in-flight breakup.NTSB ERA21LA371Accident · No injuriesClass 4 · LimitedFinal reportMooney M20K · New Shoreham, RIThe pilot’s improper decision to reject the takeoff at an excessive speed, resulting in a runway excursion and collision with a fence. Contributing to the accident was the pilot’s failure to lock the door as required by the placarded door closing procedures.NTSB ANC21LA064Accident · No injuriesClass 3 · LimitedFinal reportPiper PA-14 · Anchorage, AKThe fatigue fracture of the American Iron and Steel Institute (AISI) 1025 carbon steel rudder post, which resulted in structural failure of the rudder. Contributing to the fatigue failure was the post’s susceptibility to fatigue cracking under normal service…NTSB CEN21LA450Accident · No injuriesClass 4 · LimitedFinal reportCessna 140 · Caddo Mills, TXThe missing vertical stabilizer hardware, which resulted in a severe uncommanded yawing motion that necessitated an emergency landing, during which the airplane nosed over and sustained substantial damage to the vertical stabilizer.NTSB CEN21FA314Accident · 1 fatalClass 3 · FieldFinal reportPZL Mielec M18 · Seiling, OKThe pilot’s in-flight loss of control due to the structural failure of a wing fitting and separation of the outboard wing section. Also causal were the inadequate wing fitting inspections, which failed to detect the initial corrosion and crack before it…NTSB WPR21FA266Accident · 2 fatalClass 3 · FieldFinal reportBeech C90 · Wikieup, AZThe failure and separation of the left wing’s outboard section due to a fatigue crack in the lower spar cap. Contributing to the accident was the operator’s decision to repair the wing spar instead of replacing it as recommended by the aircraft manufacturer.…NTSB ERA21LA247Accident · Minor injuriesClass 3 · LimitedFinal reportGarrison Ronald L Zodiac 601 XL · Cumberland, MDAn inadvertent release of the canopy, which allowing the canopy to open during flight and led to an inflight loss of airplane control. Contributing to the accident was the lack of any safeguard to prevent the inadvertent opening of the canopy.NTSB ERA21FA233Accident · 4 fatalClass 3 · FieldFinal reportBhi H60 Helicopters UH-60A · Leesburg, FLThe failure of the water tank snorkel support structure, which allowed the snorkel to contact the main rotor blades. Contributing to the accident was insufficient Federal Aviation Administration oversight of the supplemental type certificate process for the…NTSB CEN21LA236Accident · No injuriesClass 4 · LimitedFinal reportBerry TX-11C · Longmont, COThe pilot’s loss of directional control when his foot became stuck on a protruding bolt in the airplane’s floorboard.NTSB WPR21LA204Accident · Serious injuriesClass 3 · LimitedFinal reportMcclure B J Glasair III · Eugene, ORThe pilot’s loss of airplane control during the approach to landing due to an asymmetrical flap deployment for reasons that could not be determined based on the available evidence.NTSB CEN21FA199Accident · 1 fatalClass 3 · FieldFinal reportCirrus Design SR22 · Port Aransas, TXThe pilot’s failure to maintain adequate airspeed during the go-around, which resulted in the airplane exceeding its critical angle of attack and a subsequent aerodynamic stall.NTSB ERA21LA177Accident · No injuriesClass 3 · LimitedFinal reportForisch Edward Bushby Mustang M II · Worcester, MABinding of the left aileron bellcrank push/pull rod, which resulted in an uncommanded right turn.NTSB ENG21LA023IncidentClass 3 · LimitedFinal reportBombardier CL-600-2C10 · North Canton, OHMoisture ingression thru the window humpseal coming into contact with the terminal block braid wires.NTSB ERA21LA396Accident · No injuriesClass 4 · LimitedFinal reportSonex Waiex · Doylestown, PAThe pilot’s failure to maintain a proper glidepath during landing. Contributing to the accident was his failure to ensure the canopy locks were properly configured prior to flight.NTSB WPR21LA142Accident · No injuriesClass 3 · LimitedFinal reportDavis Dan B Lancair Evolution · Phoenix, AZA malfunction of the main cabin door latching mechanism for reasons that could not be determined based on the available information.NTSB ERA21FA142Accident · 1 fatalClass 3 · FieldFinal reportLuscombe 8E · Jupiter, FLThe pilot’s exceedance of the airplane’s critical angle of attack, which led to an aerodynamic stall and loss of control. Contributing to the accident was the pilot’s inadequate preflight inspection of the airplane, resulting in an unsecured engine cowl that…NTSB CEN21LA132Accident · No injuriesClass 3 · LimitedFinal reportBeech B100 · Lubbock, TXThe failure of the right-side window inner pane for reasons that could not be determined based on available evidence.NTSB WPR21LA108Accident · No injuriesClass 3 · LimitedFinal reportAbbett Gerry Lancair Evolution · Saratoga, WYA windshield failure during cruise flight due to stress concentrations in the bond area as a result of improper assembly of the windshield.NTSB ENG21LA013IncidentClass 3 · LimitedFinal reportBoeing 767-338 · Ontario, CAThe fatigue fracture and liberation of two airfoils from a low pressure turbine stage 5 nozzle segment that impacted and damaged the downstream low pressure stage 5 blades creating an initial imbalance load in the engine’s low pressure turbine rotor…NTSB ERA21LA106Accident · No injuriesClass 3 · LimitedFinal reportAmerican AA5 · Leesburg, VAThe weakened structure of the left horizontal stabilizer, which resulted in elevator flutter and subsequent partial separation of the left elevator in flight. Contributing to the accident were the lack of elevator authority while landing due to the damaged…NTSB ERA21LA238Accident · No injuriesClass 3 · LimitedFinal reportPiper PA46R-350T · York, PAAn improper weld repair of the engine mount, which resulted in a fatigue failure of the mount and subsequent nose landing gear collapse. Contributing to the accident was maintenance personnel’s failure to accomplish the manufacturer’s service bulletin…NTSB ERA21LA051Accident · Serious injuriesClass 4 · LimitedFinal reportJ&J Ultralights Sea-Wing · Placida, FLThe pilot/owner’s improper preflight inspection of the weight-shift trike, which resulted in a loss of control at takeoff due to an improperly adjusted wingtip.NTSB WPR21LA037Accident · No injuriesClass 3 · LimitedFinal reportRemos Aircraft Gmbh Flugzeugbau GX · Glendale, AZThe material overstress failure of the airframe’s aluminum carry-through of the main landing gear.NTSB ERA21LA014Accident · No injuriesClass 4 · LimitedFinal reportPipistrel Alpha Trainer · Rural Hall, NCThe pilot’s failure to maintain airplane control and improper recovery from an unusual attitude, which resulted in an in-flight breakup.NTSB ANC20LA098Accident · No injuriesClass 3 · LimitedFinal reportCessna 182 · King Salmon, AKThe fatigue fracture failure of the left main landing gear U-bolt during landing, which resulted in the collapse and separation of the left main landing gear spring.NTSB ERA20LA315Accident · 2 fatalClass 3 · LimitedFinal reportVans RV9 · Steinhatchee, FLThe failure of the air traffic controller to provide hazardous weather information to the pilot, resulting in the flight’s encounter with strong updraft conditions, an inflight loss of airplane control, and an in-flight breakup. Contributing was the pilot’s…NTSB ANC20LA089Accident · No injuriesClass 3 · LimitedFinal reportEurocopter AS 350 · Fort Greely, AKFailure of the door lock due to interference between the door and a cargo box.NTSB CEN20LA378Accident · No injuriesClass 3 · LimitedFinal reportCessna 340 · Oklahoma City, OKA failure of the windscreen for reasons that could not be determined based on available evidence.NTSB ERA20CA303Accident · No injuriesClass 4 · Data collectionFinal reportZenith CH601 · Punta Gorda, FLAn inadvertent opening of the airplane’s canopy on takeoff, which resulted in a loss of control and runway excursion.NTSB CEN20LA327Accident · Serious injuriesClass 3 · LimitedFinal reportGrumman G164 · Alicia, ARInadequate maintenance of panel fasteners, which led to a side panel coming loose during takeoff and the pilot having to make a subsequent forced landing to a flooded rice field when the airplane became difficult to control.NTSB CEN20LA294Accident · No injuriesClass 3 · LimitedFinal reportRockwell S2R · Harlan, IAThe fatigue fracture of the upper rudder hinge that resulted in a partial separation of the rudder from the airplane during a spray pass.NTSB WPR20LA224Accident · 1 fatalClass 3 · LimitedFinal reportHiller UH 12D · Mehama, ORAn in-flight separation of a tail rotor blade due to fatigue cracking and overstress, which resulted in a loss of directional control and subsequent ground impact.NTSB ANC20LA064Accident · No injuriesClass 3 · LimitedFinal reportPiper PA22 · Soldotna, AKThe delamination of the fabric material from the fuselage above the windscreen due to failed adhesive, which resulted in disrupted airflow and a subsequent hard landing.NTSB ANC20LA059Accident · No injuriesClass 3 · LimitedFinal reportPiper PA 12 · Anchorage, AKThe fatigue fracture of the American Iron and Steel Institute (AISI) 1025 carbon steel rudder post, which resulted in structural failure of the rudder. Contributing to the fatigue failure was the post’s susceptibility to fatigue cracking under normal service…NTSB ERA20CA243Accident · No injuriesClass 4 · Data collectionFinal reportPiper PA28 · Greenwood, SCThe pilot's failure to maintain adequate clearance from a parked airplane while taxiing. Contributing to the accident was the parked airplane's position over the double-yellow taxiway edge lines and into the taxiway object-free movement area.NTSB CEN20LA201Accident · 4 fatalClass 3 · LimitedFinal reportPiper PA28 · Carlinville, ILThe pilot’s attempted recovery from a steep descent which inadvertently exceeded the ultimate load factor of the airframe and resulted in a low-level inflight breakup.