Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = 'AB139' ORDER BY difficulty_date 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 sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = 'AB139' ORDER BY difficulty_date 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.
SDR AC2A119531Bolt · damagedMECHANICAL DAMAGE BEYOND LIMITS.SDR AC2A021408001Gearbox · making metalIN CRUISE FLIGHT, AT 3500 MSL, THE MGB CHIP SUMP CAS MESSAGE CAME ON. FOLLOWED THE EMERGENCY PROCEDURE. THE CHIP BURNER WOULD NOT CLEAR THE CHIP. LANDED AT AIRPORT WITHOUT INCIDENT. FOUND 3 SMALL FLAKES ON RT LOWER CHIP PLUG. PERFORMED SERVICEABILITY CHECK ANDSDR U0GA118168Fire Warning · false activationDURING A TRAINING MISSION, THE PILOT REPORTED THAT DURING A MISSED APPROACH THE AUDIO ALERT, NR 2 ENGINE FIRE, SOUNDED TWICE JUST AS IT DOES IN A TEST OF THE SYSTEM. NO WARNING/CAUTION LIGHTS OR CAS MESSAGES WERE OBSERVED. THE PILOT LANDED AT HUM AS SOON ASSDR 2007F00057Panel · delaminatedAFT UPPER DECK BETWEEN STATIONS 7920MM AND 7720MM IS DEBONDED. THE AREA IS APPROXIMATELY 800MM WIDE AND 200MM LONG. WATER WAS FOUND INSIDE THE HONEYCOMB CORE.SDR 2007F00053Panel · delaminatedAFT UPPER DECK BETWEEN STATIONS 7920MM AND 7720MM IS DEBONDED.THE AREA IS APPROXIMATELY 800MM WIDE AND 200MM LONG. WATER WAS FOUND INSIDE THE HONEYCOMB CORE.SDR AC2A116357Cowling · burnedCOWLING WAS FOUND BURNED DURING EXHAUST BRACKET REPLACEMENT. BURNED AREA WAS APPROXIMATELY (2) INCHES BY (3) INCHES. COWLING WAS REPAIRED AND RETURNED TO SERVICE. ALL OTHER AIRCRAFT IN FLEET WERE INSPECTED AND FOUND OK PHOTO OF COWLING HAS BEEN SENT TO FSDOSDR 31038042507Window · departedDURING CRUISE FLIGHT AT AN ALTITUDE OF 2000FT, IAS 152KTS,THE CO-PILOT DOOR WINDOW SEPARATED FROM AIRCRAFT.SDR U0GA114871Skin · crackedCRACK FOUND AT STA. 8700 UPPER LEFT HAND CORNER OF FUSELAGE. COMPLIED WITH BT139-015 PART I REPAIRED BY AGUSTA.SDR AC2A2007032871967Screen · brokenNR 1 ENGINE INLET SCREEN HAS BROKEN WIRES.SDR AC2A114524Connector · dirtyWHILE IN FLIGHT, NR 2 SERVO CAS LIGHT ILLUMINATED. ON HYDRAULIC SYSTEM SYNOPTIC PAGE, THE NR 2 FWD, RT, LT AND T/R SERVOS ALL INDICATED JAMS. EMERGENCY CHECK LIST WAS FOLLOWED AND AIRCRAFT RETURNED TO BASE. CLEANED ELECTRICAL CONNECTOR ON SERVO BYPASS SWITCHESSDR CA070514006Fmu · unserviceable(CAN) ENGINE POWER REDUCED UNCOMMANDED IN CRUISE AND THE ENGINE WAS SHUTDOWN IN FLIGHT. THE FUEL MANAGEMENT MODULE (FMM) WAS SUBSEQUENTLY REPLACED. (TC NR 20070514006)SDR AC2A113324Attach Fitting · crackedCRACKS FOUND IN FITTING AT UPPER LT TAILBOOM ATTACHMENT POINT RADIATING FROM LOCK FASTENERS.SDR AC2A113325Attach Fitting · crackedCRACKS FOUND IN FITTING AT UPPER LT TAILBOOM ATTACHMENT POINT RADIATING FROM HI-LOCS.SDR AACSDR121406Longeron · crackedDURING INSPECTION OF THE TAILBOOM ATTACHMENT POINTS, A CRACK ABOUT 1.5 INCHES LONG WAS DISCOVERED ON THE TOP LT LONGERON AT STA 8700MM.SDR U0GA114048Attach Fitting · crackedDURING ROUTINE INSPECTION FOUND A CRACK AT UPPER LT TAILBOOM ATTACHMENT AT STATION 8700. CRACK PROTRUDES FROM RIVET IN STRUCTURE.SDR U0GA114045Attach Fitting · crackedDURING ROUTINE INSPECTION FOUND CRACK AT UPPER LT TAILBOOM ATTACHMENT, STATION 8700. THE CRACK EXTENDED FROM A LOCK FASTNERS IN THE SUPPORT STRUCTURE.SDR AC2A113056Attach Fitting · crackedTHREE (3) CRACKS FOUND IN FUSELAGE TO TAILBOOM ATTACH STRUCTURE ON FUSELAGE SIDE. (1 )CRACK IN THE RADIUS OF THE BULKHEAD AND (2) CRACKS RADIATING FROM HILOK FASTENERS ON OUTER STRUCTURE THAT ENCAPSULATES THE ATTACH FITTING IN THE UPPER LT ATTACH POINT.SDR AC2A112005Scissors · damagedDAMAGED TO SCISSORS FROM CONTACT OF LONG COUPLING, REPLACED SCISSORS.SDR AC2A112002Tire · wornTIRE EXCESSIVELY WORN DOWN TO CORDS, REPLACED BOTH MAIN TIRES.SDR AC2A112003Bonding Strap · brokenTAIL ROTOR BONDING STRAP BROKE OFF IN FLIGHT, REPLACED STRAP.SDR AC2A112004Scissors · damagedDAMAGED TO SCISSORS FROM CONTACT OF LONG COUPLING, REPLACED SCISSORS.SDR AC2A111904Firewall · crackedFOUND FIREWALL CRACKED, REPLACED FIREWALL.SDR AC2A112006Coupling · wornGROOVE WORN IN SHANK, REPLACED COUPLING.SDR AC2A111989Bushing · galledDURING 300 HOUR INSPECTION ROTATING SCISSORS HAD EXCESSIVE PLAY AND WHEN ASSY WAS DISSASSEMBLED THE BUSHINGS WERE GALLED.SDR AC2A111992Scissors · looseDURING 300 HOUR INSPECTION ROTATING SCISSORS HAD EXCESSIVE PLAY AND WHEN ASSY WAS DISASSEMBLED THE BUSHINGS WERE GALLED, REPLACED BUSHINGS.SDR AC2A111381Clamp · crackedTAIL ROTOR DAMPER CLAMP CRACKED, REPLACED CLAMP.SDR AC2A111264Servo · warning messageIN CRUISE, FLIGHT AT 6500 FT, THE NR 2 SERVO CAUTION LIGHT CAME ON. OPENED THE SYNOPTIC PAGE AND FOUND ALL PRESSURE AND TEMPS NORMAL. HOWEVER THE 4 SERVO LIGHTS WERE YELLOW. FOLLOWED THE EMERGENCY PROCEDURES CHECKLIST AND TURNED AROUND. AFTER A FEW MINUTES TSDR AC2A111905Firewall · crackedFOUND FIREWALL CRACKED, REPLACED FIREWALL.SDR AC2A110571Exhaust Stack · crackedDURING NORMAL PROCEDURES COPILOT WAS ASSISTING DEPARTING PASSENGERS AND LUGGAGE, HE NOTICED THE NR 1 EXHAUST STACK CRACKED AND FOLDED BACK. AFTER SHUTDOWN AND FURTHER INSPECTION FOUND THE STACK CRACKED ABOUT 12 INCHES ALONG THE LOWER WELD SEAM AND IB CRACK ABOSDR AC2A110545Exhaust Pipe · crackedEXHAUST NOZZLE HAD 12 INCH CRACK ALONG TACK WELDED SEAM NEAR AFT END OF TAIL PIPE. REPLACED WITH SERVICEABLE EXHAUST NOZZLE.SDR AC2A110529Power Lever · damagedNR 1 ENGINE TRIM WAS INOPERABLE AND ECL 1 CAS MESSAGE. FOUND LEVER PIN SHEARED/REPLACED POWER LEVER QUADRANT.SDR AC2A110236Hose · misinstalledLINES WERE INSTALLED WRONG, CAUSING THEM TO BE KINKED.SDR AC2A110235Hose · misinstalledLINES WERE INSTALLED WRONG, CAUSING THEM TO BE KINKED.SDR AC2A110707Seal · failedSEAL BREAKING DOWN, COMING APART AND LEAVING A GAP, REPLACED SEAL.SDR AACSDR61606Drive Shaft · unbondedNEW AIRCRAFT WAS BEING ASSEMBLED AFTER SHIPPING. DURING ASSEMBLY TAIL ROTOR DRIVESHAFT WAS FOUND SCORED AROUND UPPER FLANGE ATTACHMENT AREA. THIS WAS DIRECTLY BELOW THE TAILROTOR GEARBOX, AT THE TOP OF THE VERTICAL FIN. SCORING WAS CAUSED BY A (CLICK-BOND) TYSDR 2006FA0000483Bolt · gougedUPON RECEIPT OF THE AIRCRAFT, THE MAIN ROTOR BLADE BOLTS WERE REMOVED FOR INSPECTION. IT WAS DISCOVERED THAT ONE BLADE BOLTS HAS A RADIAL GOUGE MARK AT THE LOWER BLADE TO HUB BUSHING LOCATION. THE DAMAGE IS OUTSIDE THE AMM PERMITTED REPAIR LIMITS. THE AC TTSDR 2006FA0000446Bolt · gougedDURING ACCOMPLISHMENT OF THE MAIN ROTOR BLADE REMOVAL, IT WAS DISCOVERED THAT EACH OF THE BLADE BOLTS HAS RADIAL GOUGE MARKS AT THE BLADE TO HUB BUSHING LOCATIONS. THE DAMAGE IS OUTSIDE THE AMM PERMITTED REPAIR LIMITS. (REFERENCE: 39A62221300A286AB) MFG HAS
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