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 jasc_code = '1430' 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 jasc_code = '1430' 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 AALA20050219Fastener · crackedAFW - SEVEN LOCK FASTENER COLLARS CRACKED INSIDE FUEL TANKS AT WING STATION 261.2 LEFT HAND 394.2 LEFT HAND, 308.1 RT, 798.2 RIGHT HAND. REPLACED SEVEN EACH LOCK FASTENER COLLARS. NO LOOSE OR LEAKING LOCK FASTENERS AFTER REPLACEMENT OF COLLARS. SYSTEM GROUNSDR SIMA200507001Bolt · brokenDURING PHASE 2A INSPECTION, FOUND RIGHT AILERON DAMPER ROD END BOLT BROKEN. REMOVED AND REPLACED BOLT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR SWAA050722Bolt · wornDURING SCHEDULED C4 CHECK, RT ELEVATOR TAB FAILED THE FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB CONTROL PUSHROD BOLTS & SPACERS PER MM.SDR CA050308008Collar · cracked(CAN) 8 COLLARS WERE FOUND CRACKED ON THE RT WING FORWARD SPAR AT EXTENSION SPLICE YW 490.00, ANOTHER 2 OF THE SAME COLLARS WERE ALSO CRACKED ON THE SAME LOCATION ON THE AFT SIDE. INSPECTION OF THE LT WING IN THE SAME YW 490.00 LOCATION REVEALED FURTHER TWO FSDR 2005FA0000399Screw · backed outROLL SERVO HAD SCREW COME LOOSE AND MADE CONTACT WITH CIRCUIT BOARD CAUSING SHORT AND BURNING UP COMPONENTS ON BOARD. RECOMMEND TO USE LOCTITE ON SCREWS TO PREVENT SCREWS FROM BACKING OUT OF HOLES. (K)SDR QXEA200500470Fastener · looseYYC - LEFT HAND WING UPPER SURFACE TRAILING EDGE HAS LOOSE FASTENERS AT STATION 170 AND 232. REPAIRED IAW CRJ7, SRM 51-25-01-001-001-A01 AND SRM 51-42-06-001-001-A01.SDR QXEA200500438Rivet · looseYYC -FUSELAGE EXTERIOR HAS LOOSE RIVETS AT FS800 BETWEEN STRINGER 16 RT AND STRINGER 17 RT, AT WING TO BODY FAIRING ATTACH. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01.SDR QXEA200500437Rivet · looseYYC - FUSELAGE EXTERIOR HAS LOOSE RIVETS AT FS800 BETWEEN STRINGER 16 LT AND STRINGER 17 LT, AT WING TO BODY FAIRING ATTACH. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01.SDR ASAA0540145Nut · missingPDX- FOUND R1 DOOR WOULD NOT OPEN. FOUND UPPER GEAR CONTROL ROD RETAINING NUT MISSING AND BOLT FELL OUT. SECURED UPPER CONTROL ROD BOLT AND RETAINING NUT. ALL RIG AND OPS CHECKS GOOD.SDR CA050223004Nut · fractured(CAN) DURING CPCP AND SID INSPECTION, THE WING LOWER ATTACH STRUT BOLT AND NUT WERE REMOVED FOR INSPECTION AND THE NUT WAS FOUND FRACTURED THROUGH. THE COTTER KEY WILL HOLD THE NUT/BOLT IN PLACE. THE FRACTURE WAS LOCATED THRU THE MFG IDENTIFICATION STAMPS ON TSDR AWXA200500342Bolt · corrodedMCN - FLIGHT CONTROL - DURING C-14 CHECK GALVANIC CORROSION WAS FOUND ON LT HORIZONTAL STABILIZER UPPER REAR BOLT. MAINTENANCE REMOVED AND REPLACED LT HORIZONTAL STABILIZER UPPER REAR BOLT IAW T/C I6C55307.SDR QXEA200500282Rivet · looseYYC - RT WING UPPER SKIN TRAILING EDGE HAS LOOSE FASTENERS AT STATION 170 AND 231.23. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A021 AND 51-25-01-001-001-A01.SDR QXEA200500254Rivet · shearedYYC - PASSENGER DOOR AFT NEWEL ATTACH POINT FOR PITT PIN HAS SHEARED RIVET AND BRACKET HAS BEEN BUMPED OUT OF POSITION. REPAIRED IAW CRJ700 SRM 51-42-13-001-001-A01 AND 51-42-06-001-001-A01.SDR SWAA050384Bolt · wornDURING SCHEDULED C2 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BOLT PER MM.SDR CA050216007Rivet · loose(CAN) DURING AME DAILY INSPECTION LT HORIZONTAL STABILIZER FOUND TO HAVE APPROXIMATE 1 INCH VERTICAL DISPLACEMENT AT TIP. RIVETS THAT SECURE THE OUTER SHIM HAD SHEARED ALLOWING BUSHING MOVEMENT. SB 55-001 TO BE INCORPORATED , NOT PREVIOUSLY COMPLIED WITH. TO SDR QXEA200500243Nut · brokenYYC - AFT RAD ALT ANTENNA AT STATION 1102, STRINGER 26L TO 27L HAS A BROKEN A- NUT AT AFT LEFT CORNER. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01.SDR AMTA200500135Fastener · lightning strikeLIGHTNING STRIKE DAMAGE TO FASTENER IN THE FS 900 BUTT JOINT BETWEEN THE S4R LAP SPLICE AND STRINGER S3R. COMPLIED WITH ERA.SDR A6WA200540040Fastener · mislocatedUNABLE TO ACHIEVE EDGE DISTANCE ON JOINT STRAP (PN 601R1004654) WHILE COMPLYING WITH SB 601R57037 DUE TO EXISTING FASTENER BEING MISLOCATED. PERFORMED A MAJOR ALTERATION TOO, BY SHIFTING THE CUTLINE TO PROVIDE MINIMUM EDGE DISTANCE ON THE EXISTING FASTENERS, SDR AWXA200500267Bolt · corrodedMCN - MAJOR REPAIR - DURING C-16 CHECK, CORROSION WAS FOUND ON RT OUTBOARD VERTICAL STABILIZER ATTACH BOLT AND WASHERS BS 1016, STR 2 RT. MAINTENANCE REMOVED AND REPLACED CORRODED RT OUTBOARD VERTICAL STABILIZER ATTACH BOLT AND WASHERS IAW BMM 55-30-00.SDR SWAA050212Bolt · wornDURING SCHEDULED C4 CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT TAB HARDWARE PER MM.SDR DL76L050054Bolt · shearedMLG WHEEL TIE BOLT SHEARED. REPLACED WHEEL ASSY.SDR ASOA05046Nut · missingDURING A GROUND INSPECTION, THE FORWARD EMERGENCY FLOOR LEVEL FLOODLIGHT BY THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND A NUT MISSING ON THE GROUND STUD TO THE FORWARD EMERGENCY FLOOR LEVEL FLOODLIGHT BY THE PASSENGER DOOR. OPERATIONAL SDR 2005FA0000363Bolt · wornTOP RUDDER HINGE BOLT LOOSENED FROM THE SELF LOCKING NUT PLATE AND CAME OUT CAUSING THE RUDDER ASSEMBLY TO DETACH FROM THE AC COMPLETELY DURING FLIGHT AT 2000 AGL. THIS BOLT SHOULD HAVE SOME TYPE OF RETAINING MECHANISM IN ADDITION TO THE SELF LOCKING NUT PLATSDR 2005FA0000024Bolt · loose3 OF THE 4 BOLTS THAT ATTACH THE METAL PLATE THAT THE ACTUATOR IS MOUNTED ON TO THE WASTEGATE BODY WERE MISSING. FOURTH BOLT WAS BACKED OUT ABOUT HALF WAY. ALL THREE BOLTS FOUND LOOSE IN ENGINE COMPARTMENT. WASTEGATE ASSEMBLY ONLY 287 FROM OVERHAUL BY MAIN SDR X6PA200500001Bolt · brokenPILOT'S SEAT BACK ADJUST BOLTS BROKE, ALLOWING SEAT BACK TO RECLINE.SDR AMTA200500049Fastener · lightning strikeLIGHTNING STRIKE DAMAGED 2 FASTENERS FORWARD AND ADJACENT TO THE L1 DOOR. REPAIRED DAMAGE BY REPLACING DAMAGED FASTENERS IAW PART 1 OF ERA. (K)SDR CA050113001Bolt · loose(CAN) DURING A POST FLT WALKAROUND MX DISCOVERED DAMAGE ON LT OUTBOARD WING LOWER SPAR CAP, AFT OF THE NR 6 LEADING EDGE SLAT. FURTHER INSPECTION REVEALED A LOOSE UNATTACHED BOLT PRESENT IN THE AREA. THIS BOLT CREATED FOD DAMAGE TO THE SPAR WHEN THE NR 6 SLSDR SWAA050045Fastener · missingL1 DOOR EVAC SLIDE MOUNTING FASTENER MISSING. REMOVED AND REPLACED FASTENER PER MM.SDR USAA050046Rivet · loosePIT - FOUND LT WING FOREFLAP 42 LOOSE RIVETS, LT WING OUTBOARD FOREFLAP APPROX 42 INCHES. DEFECTIVE PART REPLACED WITH IDENT PART. (M)SDR QXEA200500073Nut Plate · strippedPDX - FUSELAGE PANEL HAS FOUR STRIPPED OUT NUTPLATES. REPLACED OLD NUTPLATES WITH NEW NUTPLATES.SDR NACA20040065Bolt · shearedRIGHT FLAP OUTBOARD ACTUATOR BOLT SHEARED. REPLACED BOLT AND INSPECTED FLAP AND CARRIAGE SYSTEM, OK FOR SERVICE. INSTALLED NEW NUT AND WASHER. OP CHECKED GOOD.SDR 270112Bolt · chafedTHE BOLT (P/N 3-34) THAT SERVES AS THE PIVOT FOR THE ALTERNATE AIR DOOR IN THE INDUCTION DUCT ASSY (P/N 15708-001) IS BEING CHAFFED BY THE INDUCTION DUCT SUPPORT BRACKET P/N 15671-002. IN ADDITION TO THE CHAFFED BOLT THE PLASTIC DUCT IS SUSCEPTABLE TO CRACKINGSDR 27011204Bolt · chafedTHE BOLT (P/N 3-34) THAT SERVES AS THE PIVOT FOR THE ALTERNATE AIR DOOR IN THE INDUCTION DUCT ASSY (P/N 15708-001) IS BEING CHAFED BY THE INDUCTION DUCT SUPPORT BRACKET P/N 15671-002. IN ADDITION TO THE CHAFED BOLT THE PLASTIC DUCT IS SUSCEPTABLE TO CRACKING ASDR SWAA043666Fastener · brokenDURING SCHEDULED 5Y CHECK, FOUND L2 DOOR EVAC SLIDE GIRT BAR HOLD DOWN BRACKET FASTENER BROKEN. REPLACED FASTENER PER MM.SDR CA041222012Bolt · mismanufactured(CAN) WHEN REINSTALLING THE HORIZONTAL STAB, (AT THE AFT SPAR ATTACH POINT) USING NEW HARDWARE, IT WAS DISCOVERED THAT THE REQUIRED BOLTS WERE LONGER IN TOTAL LENGTH BY 0.1875 AND SHANK LENGTH BY 0.1875, THAN THE ORIGIONAL BOLTS REMOVED. THIS CAUSED THE NUTS SDR 2005FA0000489Rivet · looseUPON X-RAY INSPECTION OF AIRCRAFT FOR A 4000 LANDING INSPECTION, FOUND SEVERAL WORKING RIVETS AROUND CABIN WINDOWS AS INDICATED. LT NR 3 WINDOW; ONE (1) WORKING RIVET, LT NR 4 WINDOW; FOUR (4) WORKING RIVETS, LT NR 5 WINDOW, ONE (1) WORKING RIVET, RT NR 3 WINSDR AALA20041210Fastener · looseSLC - INFLIGHT FUEL LEAKING FROM BOOST PUMP COVER ON RIGHT WING. FOUND FASTENERS LOOSE ON RIGHT FORWARD AND AFT OF BOOST PUMP COVER. RETORQUED LOOSE FASTENERS ON RIGHT FORWARD AND AFT OF BOOST PUMP COVER. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR 2005FA0000096Bolt · corrodedBOLT SHEARED AT THREADS DURING REMOVAL. SIGNS OF INTERNAL CORROSION ON BOLT.SDR QXEA200400872Bolt · backed outYYC - AFT BAGGAGE DOOR FORWARD BOTTOM STOP FITTING HAS ONE BOLT THAT WILL NOT GRIP AND HAS BACKED OUT. REPAIRED IAW HORIZON EA 6-52-360, RD 8/4-52-178 AND SRM 52-31-23-400-801.SDR QXEA200500076Nut Plate · spinningPDX - PANEL 121AR HAS A SPINNING NUTPLATE. REMOVED NUTPLATE AND INSTALLED A NEW NUTPLATE WITH RIVETS.SDR QXEA200500075Nut Plate · spinningPDX - PANEL 122BL HAS A SPINNING NUTPLATE. REMOVED NUTPLATE AND INSTALLED A NEW NUTPLATE WITH RIVETS.SDR SWAA043524Bolt · wornDURING SCHEDULED C1 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT NR 1 HINGE TAB BOLT PER MM.SDR 26251204Bolt · chafedTHE BOLT (P/N 3-34) THAT SERVES AS THE PIVOT FOR THE ALTERNATE AIR DOOR IN THE INDUCTION DUCT ASSY (P/N 15708-001) IS BEING CHAFED BY THE INDUCTION DUCT SUPPORT BRACKET (P/N 15671-002). IN ADDITION TO THE CHAFFED BOLT THE PLASTIC DUCT IS SUSCEPTIBLE TO CRACKISDR CA041202005Bolt · cracked(CAN) DURING ANNUAL INSPECTION THE HORIZONTAL STABILIZER STRUT ATTACH BOLTS WERE REMOVED FOR INSPECTION. THE LOWER RH BOLT WAS SUSPECTED OF BEING CRACKED. THE BOLT WAS LPI INSPECTED AND THE CRACK WAS VERIFIED. ALL AIRCRAFT IN OUR FLEET WILL HAVE THE BOLTS INSDR DL767041075Bolt · misinstalledFOUND BY FAA INSPECTOR, RIGHT MLG WING DOOR LOWER AFT MOUNT BOLT INSTALLED INCORRECTLY. BOLT IS DAMAGED AND CENTER SHIMS ARE MISSING. INSTALLED NEW BOLT AND HARDWARE PER AMM 32-12-06 AND IPC32-12-01-05 RIGHT MLG WING DOOR LOWER AFT MOUNT INSTALLATIONS NOW COSDR 04FDEA03271Screw · brokenAFTER TAKEOFF, THE FLAP HANDLE COULD NOT BE MOVED PAST THE FLAPS 0 DEGREES, NOR COULD MOVE IT PAST THE FLAPS 20 DEGREE POSTION. THE FLAPS DID MOVE FROM THE 20 DEGEES TO 15 AND BACK. FOUND SPECIAL-SCREW ITEM 161 REF A310-200 IPC 53-11-31-13 BROKEN. PARTS NEESDR CA041129016Bolt · sheared(CAN) DURING ANNUAL INSPECTION THE IB FORWARD AUX FIN ATTACH BOLT WAS FOUND SHEARED AT THE HEAD. IT APPEARS THAT THE FIN WAS INSTALLED WITH A PRE LOAD CAUSING THE BOLT TO FAIL. SUB-CONTRACTOR HAS BEEN NOTIFIED OF THIS OCCURRENCE AND IS CURRENTLY INVESTIGATINSDR 25921104Bolt · chafedTHE BOLT (P/N AN3-34) THAT SERVES AS THE PIVOT FOR THE ALTERNATE AIR DOOR IN THE INDUCTION DUCT ASSY (P/N 15708-001) IS BEING CHAFED BY THE INDUCTION SUPPORT BRACKET (P/N 15671-002). IN ADDITION TO THE CHAFED BOLT THE PLASTIC DUCT IS SUSCEPTIBLE TO CRACKING ARSDR 04FDEA03207Fastener · wrong partDURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND AT INSP HEAD MARKINGS OF FASTENERS ON THE VERTICAL TAIL IS INSTALLED FASTENER P/N HL221-8. REMOVE EXISTING FASTNERS AND REPAIR BY SB 55-023 GROUP 1.SDR 2004UALA01152Bolt · misalignedAFTER DIFFICULTY RAISING GEAR HANDLE, GEAR DID NOT INDICATE RETRACTED. LOUD AIR NOISE FURTHER INDICATED THAT GEAR WAS NOT UP. MLG SHOCK ABSORBER MESSAGE DISPLAYED. AIRCRAFT ARRIVED WITH LARGE AMOUNT OF ICE ON NLG AND SENSORS. CFDS SHOWS NLG FAULTS. CLEANE
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