NTSB investigations
125 cases where NTSB found Fuselage.
Cases per year
| 1979 | 1 |
|---|---|
| 2008 | 8 |
| 2009 | 16 |
| 2010 | 12 |
| 2011 | 11 |
| 2012 | 4 |
| 2013 | 8 |
| 2014 | 3 |
| 2015 | 5 |
| 2016 | 7 |
| 2017 | 5 |
| 2018 | 8 |
| 2019 | 8 |
| 2020 | 5 |
| 2021 | 4 |
| 2022 | 2 |
| 2023 | 6 |
| 2024 | 5 |
| 2025 | 4 |
| 2026 | 3 |
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 f.case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_findings.parquet' f WHERE starts_with(f.\"findingCode\", '010353')) 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", '010353')) 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 ERA26LA289Accident · No injuriesClass 4 · LimitedFinal reportBeech A36 · Weston, CTThe in-flight opening of the engine cowling, which resulted in engine baffling separating from the airplane and impacting the right elevator.NTSB DCA26LA142Accident · No injuriesClass 4 · LimitedFinal reportBoeing 787 · Houston, TXThe captain’s inadvertent activation of the takeoff/go around switch at touchdown that caused an increase in the airplane pitch attitude that was not corrected before the lower fuselage contacted the runway.NTSB DCA26LA115Accident · No injuriesClass 4 · LimitedFinal reportAirbus A321-271NX · San Francisco, CAThe first officer’s excessive aft sidestick input combined with decaying airspeed during initiation of a go-around, resulting in an increase in the airplane pitch attitude and subsequent lower fuselage contacting the runway.NTSB ERA25LA337Accident · No injuriesClass 4 · LimitedFinal reportLarocca Roch B Eracer MK II · Mount Pleasant, SCThe failure of the nose gear actuator bolt during the landing roll, which resulted in the collapse of the nose landing gear and subsequent runway excursion.NTSB ANC25LA096Accident · No injuriesClass 4 · LimitedFinal reportCessna A185F · Haines, AKThe pilot’s selection of an unsuitable landing area resulting in an on-ground collision with an obscured log and a main landing gear separation.NTSB ERA25LA114Accident · No injuriesClass 3 · LimitedFinal reportCessna 172P · Clarksville, TNThe flight instructor’s inadequate preflight inspection of the airplane, which allowed the partially secured engine cowl to separate in flight.NTSB DCA25LA085Accident · No injuriesClass 4 · LimitedFinal reportBoeing 767 · San Bernardino, CAEncounter with windshear during landing which resulted in a tailstrike.NTSB DCA25LA061Accident · No injuriesClass 3 · LimitedFinal reportLockheed 382G-44K-30 · St. Mary's, AKThe fatigue failure of the forward pressure bulkhead canted web that originated from stress corrosion cracking areas. Contributing to the failure were inspection procedures and intervals inadequate to identify the fatigue cracks.NTSB WPR24LA319Accident · No injuriesClass 3 · LimitedFinal reportBell 206L · Fern Prairie, WAAn aeroelastic interaction between the helicopter’s main rotor blades and nodal beam system, which resulted in oscillations that exceeded the design limits of the tailboom. Contributing to the accident was the failure of the main rotor blade manufacturer to…NTSB CEN24LA342Accident · No injuriesClass 3 · LimitedFinal reportPiper PA-28R · Crystal, MNThe failure of the engine mount under normal operating loads due to the fracture of a vertical tube that was weakened by corrosion and fatigue of the internal surfaces.NTSB ENG24LA012IncidentClass 3 · LimitedFinal reportBritish Aerospace BAE 146 Series 200A · Missoula, MTThe use of a new long term fire retardant with a chemical composition incompatible with the retardant previously in use for the integration-operational field evaluation without adequate testing and qualification.NTSB DCA24MA063Accident · Minor injuriesClass 1 · MajorFinal reportBoeing 737-9 · Portland, ORthe in-flight separation of the left mid exit door (MED) plug due to Boeing Commercial Airplanes’ failure to provide adequate training, guidance, and oversight necessary to ensure that manufacturing personnel could consistently and correctly comply with its…NTSB ENG23LA045IncidentClass 3 · LimitedFinal reportBell 407 · Linden, NJThe fracture of the upper-left tail boom attachment bolt due to abnormal loading of the bolt caused by a gap and misalignment between the upper-left longeron and the tail boom. Contributing to this incident was the lack of a check to verify the absence of…NTSB CEN23LA405Accident · No injuriesClass 3 · LimitedFinal reportAlisport Silent 2 Electro · Giddings, TXThe glider’s encounter with flutter during cruise flight that resulted in structural damage to the fuselage.NTSB DCA23LA409AccidentClass 4 · LimitedFinal reportBoeing 767-322 · Chantilly, VAImproper overhaul of the trunnion cross-pin hole that resulted in the development of stress corrosion cracking and eventual failure of the right forward trunnion.NTSB CEN23LA319Accident · No injuriesClass 3 · LimitedFinal reportAlisport Silent 2 Electro · Wallis, TXThe failure of the tail boom structure due to cyclic torsion overloading as of a result of flutter in the empennage. The reason for the flutter could not be determined.NTSB CEN23LA295Accident · No injuriesClass 3 · LimitedFinal reportBell UH-1H · Woodlawn, ILThe separation of the tail boom from the fuselage for reasons that could not be determined.NTSB ANC23LA038Accident · No injuriesClass 4 · LimitedFinal reportAerospatiale AS350B2 · Honolulu, HIThe instructor pilot’s inadequate supervision of the pilot receiving instruction, which resulted in a hard landing, and substantial damage to the tail boom.NTSB ANC22FA041Accident · Serious injuriesClass 3 · FieldFinal reportBell 407 · Kalea, HIThe in-flight separation of the tail boom as a result of abnormal loading and fracture of the upper-left tail boom attachment bolt due to a gap between the upper-left longeron and aft fuselage bulkhead.NTSB WPR22FA169Accident · 2 fatalClass 3 · FieldFinal reportBearhawk LSA · Kalispell, MTAn excessive pitch control input for undetermined reasons while the airplane was operating above maneuvering speed, which led to a structural failure of the right wing during cruise flight. Contributing to the accident was the poor construction quality of 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 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 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 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 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 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 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 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 DCA20CA050Accident · No injuriesClass 4 · Data collectionFinal reportBoeing 737 · Kansas City, MOa bird strike during descentNTSB GAA19CA506Accident · No injuriesData collectionFinal reportGrob G103 · San Antonio, TXThe failure of the glider tow rope, which lodged in the glider's rudder and resulted in a hard landing. Contributing to the accident was the pilot's failure to properly secure the glider's aft canopy.NTSB GAA19CA517Accident · Minor injuriesData collectionFinal reportCessna 180 · Arlington, WAThe pilot's failure to properly secure the seat before takeoff, which resulted in it sliding back during takeoff and rendering him unable to reach the rudder pedals and throttle lever, a subsequent runway excursion, ground loop, and impact with a berm.NTSB ANC19LA049Accident · No injuriesClass 3 · LimitedFinal reportCessna A185 · Talkeetna, AKA fracture of the right outboard landing gear bracket for undetermined reasons.NTSB ANC19LA024Accident · No injuriesClass 3 · LimitedFinal reportAeronca 7DC · Nome Creek, AKThe failure of the airplane's structural tubing due to corrosion, which resulted in a tailwheel separation and a subsequent loss of control. Also causal was the mechanic's failure to perform a detailed inspection of the aft fuselage during the most recent…NTSB WPR19LA171Accident · No injuriesClass 3 · LimitedFinal reportBeech 35 · Deer Park, WAAn empennage flutter event for reasons that could not be determined based on the available information.NTSB ERA19LA131Accident · No injuriesClass 3 · LimitedFinal reportCessna 182 · Brevard, NCThe mechanic's failure to notice that the left front seat left front roller housing disengaged from the seat rail during recent maintenance, and the pilot's failure to detect the disengaged roller housing during the preflight inspection, which resulted in the…NTSB GAA19CA130Accident · No injuriesData collectionFinal reportCessna 172 · Hanover, VAThe student pilot's improper decision to release the seat latch to adjust the seat position during taxi, which resulted in his inability to reach the rudder or brake pedals and a subsequent loss of directional control and impact with a ditch and fence.NTSB ERA19FA068Accident · 1 fatalClass 2 · FieldFinal reportSaberwing Saberwing · Adel, GAThe in-flight failure of the fuselage, as a result of the pilot conducting maneuvers that exceeded the structural capabilities of the airplane.NTSB WPR19LA020Accident · No injuriesClass 3 · LimitedFinal reportCessna 182 · Burns, ORThe failure of the left main landing gear due to fatigue cracking of a bolt that initiated at a corrosion pit, which formed in the absence of a required protective cadmium coating.NTSB ERA18LA253Accident · Minor injuriesLimited investigationFinal reportCirrus SR22 · Montauk, NYThe pilot's failure to properly secure his seat before initiating the takeoff, which resulted in the seat sliding back as the airplane accelerated during takeoff, his inability to reach the pedals, and the subsequent loss of directional control and impact…NTSB WPR18LA226Accident · Serious injuriesClass 3 · LimitedFinal reportHughes 369 · Riverside, CAThe instructor’s delayed remedial action to an excessive descent rate during a simulated autorotation, which resulted in a hard landing.NTSB ERA18FA180Accident · 1 fatalField investigationFinal reportCessna 150J · Manteo, NCA loss of control due to the banner tow rope becoming entangled with the left horizontal stabilizer in crosswind conditions.NTSB GAA18CA329Accident · No injuriesData collectionFinal reportDobbs George Coot · Malone, WIThe pilot’s improper decision to take off with a known structural issue, which resulted in hull damage.NTSB WPR18FA112Accident · 1 fatalField investigationFinal reportMooney M20E · Marina, CAThe pilot's exceedance of the airplane's critical angle of attack during takeoff, which resulted in an aerodynamic stall/spin.NTSB CEN18LA099Accident · No injuriesLimited investigationFinal reportBeech 35 · Batesville, ARAn in-flight control system flutter encounter during a turbulence encounter; the reason for the flutter could not be determined.NTSB DCA18CA056Accident · No injuriesData collectionFinal reportMcdonnell Douglas DC 9 33F · Bethel, AKfailure of a cargo tie-down fastener, resulting in unsecured cargo striking the pressure bulkhead.NTSB GAA17CA466Accident · No injuriesData collectionFinal reportAB Sportine Aviacija LAK 17 · Uvalde, TXThe ground crewmember’s failure to fully engage the tow hook release arm during preflight, which resulted in the premature release of the glider at insufficient altitude to complete a safe landing.NTSB ERA17LA253Accident · No injuriesLimited investigationFinal reportWaco UPF 7 · Brunswick, GAThe failure of the right main landing gear strut brace for reasons that could not be determined based on the available evidence.NTSB WPR17FA089Accident · 1 fatalField investigationFinal reportAppleby Nieuport 28 · Paso Robles, CAThe failure of unknown personnel to properly safety an elevator control cable turnbuckle, which disconnected in flight resulting in loss of pitch control. Contributing to the accident was the inadequate design of the experimental airplane, which did not…NTSB WPR17FA074Accident · 1 fatalField investigationFinal reportQuicksilver MXL II · Hesperia, CAThe pilot's failure to identify and correct his construction error of a critical structural component, which resulted in a loss of airplane control during takeoff. Contributing to the accident was the pilot's impairment due to his combined use of multiple…