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 = '7377BC' 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 = '7377BC' 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 2025FA0000288Fuel Cell · damagedNO 5, 7 & 8 AUXILIARY FUEL TANKS FOUND TO HAVE DAMAGE INCLUDING DENTS AND SCRATCHES. AFT AUXILIARY FUEL SYSTEM HAS MISSING HARDWARE & PARTS. BOLT MISSING FROM 9 G STRAP.SDR QV1Y2023062224283Unknown · unknownTHIS REPORT IS SUBMITTED ON BEHALF OF JET AVIATION AG BASEL - FAA APPROVAL NUMBER QV1Y440K. DURING THE CURRENT MAINTENANCE INPUT AT JET AVIATION BASEL, REF. PROJECT BN77Q004, THE FOLLOWING FINDINGS WERE RAISED: WORK ORDER 4020: FLIGHT CREW OXYGEN PRESSURE FSDR 2GYR2020060400001Lock Wire · missingWHILE COMPLYING WITH SERVICE LETTER 737-SL-27-286-A, IT WAS FOUND THAT THE LOCK WIRE FOR THE GROUND SPOILER INTERLOCK VALVE PUSH/PULL CABLE WAS MISSING FOR THE SUPPORT TUBE ASSEMBLY AT THE RIGHT MLG. THE MISSING LOCK WIRE WAS REPLACED WITH REFERENCE TO SERVICESDR YGJR201703010001Flex Hose · brokenA REPLACEMENT FLEXIBLE OXYGEN HOSE WAS PURCHASED FROM A VENDOR. THE PART WAS IN NEW CONDITION IN ORIGINAL PACKAGING WITH TRACEABILITY AS NEW SURPLUS CONDITION WITH CONFORMITY TO THE ORIGINAL VENDOR PURCHASE ORDER REQUIREMENTS AND A MANUFACTURE DATE OF 03/20/2SDR QV1Y20160608002Slide · no testOPERATIONAL TEST OF FWD ENTRY ESCAPE SLIDE: SLIDE DEPLOYED NORMALLY, WHEN DISCONNECTING IT FROM THE AIRCRAFT THE SLIDE OPENED, THE LEFT SIDE SEEM AND DEFLATED. FROM THE SLIDE DATA PLATE, THE MFG DATE IS AUGUST 1999 AND LAST O/H WAS PERFORMED JULY 2013.SDR YGJR2016020300001Satcom · faultedCREW REPORTED THEY WERE UNABLE TO ESTABLISH A CPDLC CONNECTION. THE CREW NOTED THAT AFTER SENDING A WINDS REQUEST THEY SAW THE MESSAGE, SENDING AND THE DATA LINK GETS STUCK IN THAT STATE. WE HAD THE CREW PULL AND RESET THE CMU 900 CIRCUIT BREAKERS. AFTER THESDR BJ6A2009090812901Cover · dislodgedON 9/6/2009 DURING THE TAKEOFF ROLL, CREW NOTICED THE MASTER WARNING LIGHT ILLUMINATED. CREW ABORTED THE TAKEOFF BELOW 80 KTS. ONCE CLEAR OF THE RUNWAY THE CREW DETERMINED THE SOURCE OF THE WARNING WAS THE OFFICE AREA SMOKE DETECTOR. FURTHER INVESTIGATION RSDR BJ6A2009082612701Window · failedNR3 RT WINDOW SHATTERED IN FLIGHT. FOUND THAT THE FRACTURE OF WINDOW INITIATED IN THE STRUCTURAL GLASS PANE AT THE EDGE OF THE SOLDER TAB. THERE WAS NO EVIDENCE OF ARCING OR ELECTRICAL DAMAGE. THE MOST LIKELY CAUSE IS THAT A TINY PIECE OF THE BUSS BAR WAS PSDR BJ6A200712901Charger · failedDURING GROUND OPERATIONAL TEST OF THE EMERGENCY LIGHTING SYSTEM, SEVERAL EMERGENCY LIGHTS AT THE AFT LAVATORY AREA AND L2 DOOR FAILED TO ILLUMINATE. REPLACED EMERGENCY BATTERY CHARGER TO RESTORE NORMAL OPERATION.SDR BJ6A200612903Floorbeam · corrodedGALLEY FLOOR STRUCTURE FOUND CORRODED WHEN GALLEY WAS REMOVED FOR OTHER MAINTENANCE. REPAIRED FLOORBEAM IAW DRAWING 4182527-01 AND SRM 51-10-51. NEW MOISTURE PROTECTIVE BARRIER APPLIED UNDERNEATH FLOORING MATERIAL AND THE FLOORBOARDS. THE CORROSION APPEARS TOSDR SBJ6A12906001Manifold · crackedWHILE PERFORMING RAYTHEON SB 737IGW-35A1 REV 1 AN O2 LEAK WAS DETECTED. FURTHER INSPECTION REVEALED A CRACKED WELD ON THE RT PASSENGER OXYGEN MANIFOLD P/N 97108928-009. THE LINE IS LOCATED ABOVE THE CEILING AT AIRCRAFT STATION 706. THIS IS THE SECOND DISCOVSDR BJ6A200612902Check Valve · leakingFLIGHT CREW REPORTED AFTER A FLIGHT FROM EGGW TO KEWR THAT THE A SYSTEM HYDRAULIC QUANTITY DECREASED FROM 92% TO 63%. THERE IS EVIDENCE OF FLUID IN THE RIGHT MAIN LANDING GEAR WELL AND ON THE AFT LOWER FUSELAGE. MAINTENANCE HAS DETERMINED THE SOURCE OF THE HSDR BJ6A12906001Manifold · crackedPASSENGER OXYGEN SYSTEM DISTRIBUTION MANIFOLD FOUND TO HAVE A CRACK IN THE LINE WHERE A FITTING ATTACHES TO THE MANIFOLD P/N 97108928-013. THE FITTING SEPARATED FROM THE LINE WHEN REMOVING FLEX LINE FOR OTHER MAINTENANCE. IF THIS FITTING HAD SEPARATED AND WASDR 1270601Overheat Sensor · out of toleranceRIGHT WING BODY OVERHEAT LIGHT ILLUMINATED DURING CLIMB THROUGH 10,000 FT CHECKLIST PERFORMED AND LIGHT EXTINGUISHED. AIRPLANE RETURNED TO WSSL AIRPORT. PRELIMINARY TROUBLESHOOTING PERFORMED. OVERHEAT DETECTION MODULE P/N 35008-307 AND SENSOR P/N 35599-2-255SDR 12706001Overheat Sensor · out of toleranceRIGHT WING BODY OVERHEAT LIGHT ILLUMINATED DURING CLIMB THROUGH 10,000 FT. CHECKLIST PERFORMED AND LIGHT EXTINGUISHED. AIRPLANE RETURNED TO WSSL AIRPORT. PRELIMINARY TROUBLESHOOTING PERFORMED. OVERHEAT DETECTION MODULE P/N 35008-307 AND SENSOR P/N 35599-2-SDR 1290503Transmitter · intermittentFLAP POSITION DISAGREE WITH FLAP HANDLE. RT FLAP 0 DEGREES, LT FLAP 5 DEGREES. BECAUSE OF SKEW INDICATION THE FLAP SYSTEM WOULD NOT EXTEND. CREW MADE AN UNEVENTFUL -0- FLAP LANDING. PERFORMED FSEU BITE AND OBSERVED CODE 27-52259 LT FLAP TRANSMITTER SWITCH SDR 1290502Amplifier · failedELECTRICAL ODOR IN DINING/CONFERENCE AREA. SHUT OFF CABIN ENTERTAINMENT & GALLEY POWER. ODOR DID NOT FULLY GO AWAY. ACFT DIVERTED & LANDED. MX DISPATCHED. FOUND SOURCE OF ELECTRICAL ODOR FROM DINING ROOM/CONFERENCE AUDIO AMPLIFIER FOR ENTERTAIN SYS. NO CIRCSDR 1290501O-Ring · cutCOMPLETE A-SYSTEM HYDRAULIC FLUID LOSS IN FLIGHT. REPLACED O-RING P/N NAS 1612-4 ON "A" SYSTEM ELECTRIC MOTOR DRIVEN HYDRAULIC PUMP BLANKING PLUG. RESERVOIR "A" RESERVICED AND LEAK CHECKED SATISFACTORY. A RECORDS REVIEW REVEALED THAT THIS PUMP WAS INSTALLED OSDR N129QS0401Rod · disconnectedDURING TAXI, CAPTAIN REPORTED HIS RT BRAKE PEDAL INOPERATIVE. PEDAL REPORTED AS (HARD). AC RETURNED TO BLOCKS, MECHANIC FOUND CAPTAINS RT BRAKE PEDAL INTERCONNECT TO CO-PILOTS PEDAL DISCONNECTED. HARDWARE FOR THE INTERCONNECT ROD WAS FOUND IN A PARTS BAG ATSDR N171QS04001Connector · arcedNR 2 IDG DROPPED OF LINE. APU USED TO SUPPLY POWER TO BUS. CREW ELECTED TO DIVERT TO PBI FOR REPAIRS. AIRCRAFT ON FAR 91 POSITIONING FLIGHT. REPLACED AFFECTED NR 2 IDG HARNESS AND CONNECTOR. OPS CHECKED SATISFACTORY. SENT HARNESS AND CONNECTOR TO THE BOEING COSDR BJ6ABushing · brokenHOT WATER TANK ATTACHMENT FAILURE DISCOVERED. REVIEW OF FAILED PARTS SHOWED CLEVIS PIN PULLED THROUGH WEB, BUSHING DISLODGED. BUSHING FOUND INTACT ON PIN IN CLEVIS. THE HOLE IN WEB AT FAILURE POINT SHOWED UNDAMAGED WEB MATERIAL GREATER THAN 180 DEGREES AROUSDR 2003F00611Mount · crackedDURING MAINTENANCE IT WAS NOTED THAT THE FORWARD AND AFT MOUNT STRUCTURES FOR THE AFT WATER HEATER WERE FOUND DAMAGED. WATER HEATER IS SUSPENDED AT 6 POINTS. THE REAR MOUNT WHICH PREVENTS LATERAL MOVEMENT AND THE FORWARD MOUNT WAS FOUND TO BE CRACKED. THE H
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