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 UPS03841545Bolt · shearedINSPECTION TYPE:C2 STRINGER END FITTING BOLT IS SHEARED OFF AT XCW 69 AT STRINGER 54 IN RT CENTER TANK. REMOVED AND REPLACED BOLT IAW UPS ENGINEERING FILE NUMBER DC8-57- 20098A DATED 11/03/03,AND SAA SK 867-195 DATED 11/05/03SDR QXEA200301314Rivet · loosePDX - ROW OF SIX (6) SMOKING RIVETS AT INBOARD END OF LEFT HAND ELEVATOR LOWER SURFACE. REPAIRED IAW DHC-8 SRM 51-40-00.SDR Z1R2003F00003Screw · brokenBLACK BLADE (COLOR CODED) TIP CAP SCREWS M/R LEADING EDGE AND BOTTOM ROW. NR 1 SCREW BROKEN. CORROSION AROUND SHANK OF SCREWS (ALL) SCREW HAD BEENN WORKING WITH BREAK ABOUT 90 PERCENT THROUGH THE SCREW WITH THE LAST 10 PERCENT BREAKING WHEN SCREW REMOVED. FSDR Z1R2003F00002Screw · brokenBLUE BLADE TIP CAP M/R SCREW. CORROSION AROUND ALL SCREWS, FIRST TWO THREADS. SEVERAL SCREWS APPEARED TO NO HAVE A FLUSH MOUNTING UNDER THE SCREW END. LENDING EDGE TOP SCREW HAD DEVELOPED A CRACK ( 90 PERCENT THROUGH SCREW) AND BROKE UPON REMOVAL. LARGE SCSDR Z1R2003F00001Screw · corrodedRED BLADE M/R TIP CAP SCREWS: LARGE SCREWS HAD DEVELOPED CORROSION AROUND TOP TWO THREADS. INSTALLATION, TORQUED LARGE SCREW 100 IN/LBS. REMOVAL (LARGE SCREWS) TORQUE 150-130 IN/LBS. SMALL SCREWS (INSTALL) TORQUE 30 IN/LBS. SMALL SCREWS (REMOVAL) TORQUE 7SDR Z1R2003F00000Screw · corrodedYELLOW BLADE(COLOR CODE) TIP CAP M/R SCREWS. FORWARD PAR OF ALL SCREWS HAVE A .002 INCH GAP BETWEEN THE HEAD OF SCREW AND MATING SURFACE. (AS MEASURED) SCREW IS NOT CONTACTING COMPLETELY AROUND THE HEAD OF SCREW. CORROSION IS APPEARING AT THE FIRST THREE THSDR UPS03441523Fastener · crackedINSPECTION TYPE:C RIGHT BS 1480 BULKHEAD ONE EACH FASTENER NR 5 WAS CRACKED AT SPLICE FITTING AREA RUNNING AFT APPROX 0.065 INCH LONG. RIGHT BS 1480 BULKHEAD SPLICE FTG NR 5 HOLE OVERSIZED TO 0.625 INCH & HFEC CONFIRMED NO CRACK. REPAIR BUSHING FABRICATED & SDR UPS03441522Fastener · crackedINSPECTION TYPE: C, RT BS 1480 BULKHEAD - ONE EACH FASTENER NR 5 WAS CRACKED AT EXTENSION FITTING AREA RUNNING AFT APPROX 0.040 INCH LONG. REF RS R53-43-35093 & EO B747-5310-19423A RT BS 1480 BULKHEAD SPLICE EXTENSION FTG NR 5 HOLE OVERSIZED TO 0.625 INCH & SDR C2XA03TY180Nut Plate · corrodedTYS DURING A SCHEDULED 2C INSPECTION THE CENTER SERVICE DOOR SILL NUT PLATES WERE CORRODED. MAINT REPAIRED THE CENTER DOOR SILL IAW EMB 135/145 GST-1927-02A AND SRM 51-21-05;06. ALL WORK WAS ACCOMPLISHED AND WILL BE REL UPON COMPLETION OF ALL WORK.SDR 03FDEA01746Bolt · corrodedSTA 1183, FORWARD BULKHEAD LOWER TENSION FITTINGS STR 26L, 27L, 26R, 27R, AND 29R HAVE CORRODED .3750 INCH BOLTS. REMOVED AND REPLACED BOLTS IAW WORK CARD 71C716-00SDR 2003FA0001085Rivet · looseTHE RIVETS THAT ATTACH THE RUDDER TORQUE TUBE TO THE BELLCRANK ADDAPTOR PLATE BECAME LOOSE. THIS CAUSED THE RUDDER TO DEFLECT AS MUCH AS FIVE DEGREES FROM ITS PROPER POSSITION.SDR 2003FA0001084Rivet · looseTHE RIVETS THAT ATTACH THE RUDDER TORQUE TUBE TO THE BELLCRANK ADDAPTOR PLATE BECAME LOOSE. THIS CAUSED THE RUDDER TO DEFLECT AS MUCH AS FIVE DEGREES FROM ITS PROPER POSSITION.SDR 2003FA0001139Rivet · misinstalledSMOKING RIVETS OBSERVED AT WS122-140 PROX DURING SCHEDULED INSPECTION. THESE RIVETS ARE CRITICAL TO WING INTEGRITY. IT APPEARS THAT THE RIVETS DID NOT PROPERLY ENGAGE THE HOLE DURING OEM INSTALLATION. SUGGEST ALL WING BOXES WITHIN 10 SERIAL NUMBER RANGE BE SDR AALA20031105Dome Nut · leakingAIRCRAFT EN ROUTE PDX-ORD OBSERVED FUEL LEAK IN THE LEFT WING ROOT. DECLARED EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT NOT OVERWEIGHT. MAINTENANCE SEALED UPPER WING TANK PLATE DOME NUT AND LEAK CHECKED. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR QXEA200301264Rivet · looseEIGHT RIVETS ON TOP FORWARD NACELLE JUST AFT OF TOP FORWARD MOUNT ARE LOOSE AND STICKING UP. REPAIRED IAW DHC-8 SRM 51-40-00.SDR ABXA040023Bolt · brokenRIGHT MAIN LANDING GEAR ACTUATOR ATTACH FITTING AT REAR SPAR AREA HAD BROKEN BOLT HEADS, 2 EACH, AT AFT AND FRONT OUTBOARD SIDE OF ACTUATOR. REMOVED AND REPLACED FASTENERS AT REAR SPAR IAW BOEING SRM 51-00-00.SDR 03266319Roll Pin · brokenDURING TAXI/GROUND HANDLING THE CREW ATTEMPTED TO ENGAGE THE PARKING BRAKE. CREW RETURNED TO GATE UNEVENTFULLY AND PASSENGERS WERE DEPLANED NORMALLY. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE PARKING BRAKE HANDLE ROLL PIN. A SATISFACTORY OPERATIONAL CHSDR 2004FA0000617Bolt · corrodedDURING ANNUAL INSPECTION THE STABILATOR WAS REMOVED FOR FURTHER INSPECTION. THIS IS DUE TO PREVIOUS PROBLEMS ON OTHER PA24 AND PA30/39 AIRCRAFT WITH STABILATOR TORQUE TUBE AND ATTACHMENT BOLTS WITH EXCESSIVE CORROSION. BOTH BOLTS AN175C33A THAT ATTACHES THE SDR I122003F00001Rivet · failedRIVETS UNDERNEATH WING TIP TANK ACCESS PANEL FAILED. THESE MS426AD3 RIVETS SECURE SEALED NUTPLATES THAT HOLD THE ACCESS PANEL ATTACHMENT SCREWS. DURING THE MANUFACTURING PROCESS, THESE RIVETS WERE SHAVED FLUSH WITH THE ACCESS PANEL RECESS ON THE TIP TANK ANDSDR QXEA200301084Nut Plate · corrodedCORRODED NUTPLATE ON BOTTOM SIDE OF AFT FLOOR SUPPORT FOR PANEL 144AZ AT STATION Y21L. REPAIRED IAW DHC-8 SRM 51-20-36, 51-20-11, 51-20-16 AND 51-40-00.SDR QXEA200301103Nut Plate · corrodedCARGO COMPARTMENT FLOOR PAN HAS A CORRODED NUTPLATE ON BOTTOM SIDE ALONG AFT ROW OF 144.HZ APERTURE. REPAIRED IAW DHC-8 SRM 51-20-16, 53-00-16, 51-20-36, 51-40-00 AND 51-20-51.SDR QXEA200301015Bolt · wornPDX- FUEL DRIPPING FROM NR 4 FLAP HANGER NACELLE ON LEFT WING. FOUND LEAK AT NR 4 FLAP CANOE FORWARD FLAP HINGE BOX BRACKET INBOARD FORWARD BOLT HEAD. REMOVED AND REPLACED BOLT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.SDR BAQA088806Bolt · mismanufacturedBOLTS JUST PURCHASED, BUT THE COTTER PINS HOLES ARE DRILLED WRONG, MAKING THE BOLTS UNUSEABLE. REQUEST WARRANTY CREDIT ON THESE BOLTS.SDR DHL2003742013Fastener · looseNR 3 DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED (P6-3 PANEL). INSPECTED FIRE LOOP ON NR 3 ENGINE. FOUND LOOSE FASTENER AND SECURED IAW B-M/M 20-80-1. NO DEFECTS NOTED.SDR 2003FA0000942Nut · looseINSTRUMENT NUT CAME OFF VSI AND SHORTED FROM AM/FM RADIO CASE TO TOP TERMINAL OF CIRCUIT BREAKER FOR THE TURN BANK INDICATOR, CAUSING WIRE FROM BUS TO CIRCUIT BREAKER TO BURN. CHECK ALL INSTRUMENTS FOR MISSING SCREW AND REMOVE AM/FM RADIO FROM AIRCRAFT.SDR QXEA200300993Bolt · loosePDX- ELEVATOR GUST LOCK JO-BOLTS CONNECTING THE ARM ASSEMBLY TO THE BUMPER STEP ASSEMBLY IS LOOSE. REPAIRED IAW DHC-8 RD 8-55-112 AND SRM 27-70-11.SDR 03FDEA01271Bolt · looseNR 3 ENG UPPER PYLON HAS NUMEROUS 1/4 BOLT LOOSE ON LT, RT, FWD AND AFT SIDE OF FWD AND AFT THRUST LINK FITTING (MARKED WITH RED). REPLACED (24) LOOSE BOLTS AND TORQUED REMAINING FASTENERS REF SRM 51-31-01 AND M/M 20-50-02-2. HFEC INSPECTED AROUND NEW BOLTSDR 03FDEA01272Bolt · looseNR 1 PYLON, TOP PYLON COVER PLATE (AFT OF FWD PYLON MT TO AFT PYLON TO WING MT), BOLTS ARE LOOSE.SDR IXXA0300055OScrew · missingAFTER TAKE OFF FROM KPHL TO KTOL AND DURING GEAR RETRACTION CREW EXPERIENCED A NOISE AND VIBRATION COMING FROM THE NOSE GEAR AREA. THE GEAR WAS LEFT DOWN FOR THE REMAINDER OF FLT AND MADE AN UNEVENTFUL LANDING IN KTOL. MAINTENANCE FOUND SCREWS MISSING FROM RIGSDR CA030825009Bolt · broken(CAN) UPON LANDING AT YCG THE FLT CREW EXPERIENCED A SEVERE SHIMMY FROM THE LANDING GEAR. THE AIRCRAFT WAS BROUGHT TO A STOP ON THE RUNWAY WITHOUT THE USE OF BRAKES. THE CREW WAS INFORMED BY RADIO THAT THE RT MLG WAS NOT TRACKING STRAIGHT. AFTER ENSURING THERESDR AUS20030793Bolt · sheared(AUS) HORIZONTAL STABILISER RT REAR PIVOT ATTACHMENT BOLT SHEARED.SDR AUS20030807Bolt · fractured(AUS) MAIN LANDING GEAR TORQUE LINK BOLT FRACTURED CAUSING TORQUE LINK TO FRACTURE AS WELL.SDR HEEA088540Fastener · mismarkedPAPERWORK SHOWS CORRECT P/N, PART IS NOT CORRECT.SDR QXEA200300944Nut Plate · strippedPDX- RED ANTI-COLLISION LIGHT HAS TWO NUT PLATES STRIPPED OUT. REPAIRED IAW Q400 SRM 51-42-05.SDR QXEA200300894Nut Plate · spinningPDX- FIVE NUTPLATES UNDER RED ROATING BEACON ARE SPINNING. REPLAIRED IAW Q400 SRM 51-42-05.SDR AMWA27Rivet · looseWHILE PERFORMING AN ABC STRUCTURAL INSPECTION, TWO RIVETS WERE FOUND TO BE LOOSE ON THE RIGHT SIDE OF THE FUSELAGE AT APPROXIMATELY FS 220.75, STRINGER 5R. REPAIR ACCOMPLISHED. NO TEAR DOWN REPORT WILL BE REQUIRED.SDR G6OA071Bolt · wornAIRCRAFT PERFORMED AN AIR RETURN SAFELY DUE TO UNABLE TO PRESSURIZE AFTER TAKE OFF. DURING TROUBLESHOOTINGFOUND GROUND SENSE ROD LOOSE. R/R UPPER BOLT PER MM 32-21-01SDR QXEA200300937Bolt · loosePDX- GUST LOCK BUMPER STOP ASSEMBLY MOUNTING PLATES ON LEFT HAND AND RIGHT HAND SIDES HAVE LOOSE MOUNTING JO BOLTS. REPAIRED IAW DHC-8 RD 8-55-112.SDR QXEA200300853Nut Plate · brokenPDX- ON NO.3 VHF ANTENNA FOUND FORWARD RIGHT HAND AND MIDDLE LEFT HAND NUT PLATES ARE BROKEN. REPAIRED IAW Q400 SRM 51-42-05.SDR QXEA200300850Bolt · looseBOI- ON FLIGHT 2364 DURING LINE CHECK, PULLING ALTERNATE RELEASE HANDLE, LEFT MAIN LANDING GEAR DOORS WOULD NOT OPEN. INSPECTED LINKAGE, PIVOT ASSMEBLIES, AND VALVES. SECURED LOOSE BOLT. NO PARTS REPLACED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICESDR A6WA200340113Fastener · looseLEFT INBOARD FLAP VANE HAS A PROTRUSION THAT IS CHAFING THE FLAP STUB WING STRUCTURE. PERFORMED A MAJOR REPAIR TO THE LEFT FLAP VANE BY REPLACEMENT OF LOOSE FASTENERS. WORK ACCOMPLISHED IAW WEST VIRGINIA AIR CENTER EO 601R-57-4131. (M)SDR UPS03241062Fastener · crackedINSPECTION TYPE: C, FOLLOWING HFEC INSPECTION AROUND FASTENER HOLES IN O/B FLANGES OF VERTICAL FIN FRONT SPAR FORGING, 2 CRACKS FOUND COMING FROM FASTENER HOLES ON LEFT SIDE. CRACKS STOP DRILLED IAW DRG 65-81528. REFERENCE SMRO EO 2003-041-001 FOR REWORK. RSDR 03FDEA01104Bolt · looseNR 1 ENGINE EXHAUST NOZZLE HAS LOOSE AND MISSING HARDWARE AROUND THE ATTACH POINT TO CASE. CLOSING ACTION ON 06/16/03. ON N/R S00104. REPLACED LOOSE AND MISSING BOLT'S AND TORQUED IAW M/M 78-11-02-2.SDR 2003UALA00556Bolt · looseFLAPERON BOLT LOOSE.SDR MALA030336Bolt · brokenRT SEPARATION BOLT (ON MAIN LANDING GEAR) BROKE. MAINTENANCE REPAIRED WIRING AT CONNECTOR GB602-20 AND WIRE GB604-20 IAW SAAB WM 20-20-35. REFER LOG PAGE 177372 FOR DETAIL.SDR QXEA200300813Rivet · poppedPDX - RIGHT HAND WING UPPER TRAILING EDGE BOTTOM SIDE HAS TWO POPPED RIVET HEADS AT APPROXIMATELY WS199. REPAIRED IAW CRJ 700 SRM 51-25-01. AND SRM 51-42-06.SDR 2004FA0000616Bolt · corrodedDURING ANNUAL INSPECTION THE STABILATOR WAS REMOVED FOR FURTHER INSPECTION. THIS IS DUE TO PREVIOUS PROBLEMS ON OTHER PA24 AND PA30/39 AIRCRAFT WITH STABILATOR TORQUE TUBE AND ATTACHMENT BOLTS WITH EXCESSIVE CORROSION. BOTH BOLTS AN175C33A THAT ATTACHES THE SDR 2004FA0000613Bolt · corrodedDURING ANNUAL INSPECTION THE STABILATOR WAS REMOVED FOR FURTHER INSPECTION. THIS IS DUE TO PREVIOUS PROBLEMS ON THE PA24 AND PA30/39 AIRCRAFT WITH STABILATOR TORQUE TUBE AND ATTACHMENT BOLTS WITH EXCESSIVE CORROSION. BOTH BOLTS AN175C33A THAT ATTACHES THE STSDR CA030702001Bolt · wrong part(CAN) BOLTS ORDERED FROM CESSNA AIRCRAFT COMPANY UNDER PROPRIETARY PN S346151 WERE RECEIVED AND DETERMINED TO BE INCORRECT. THE ORIGINAL BOLTS REMOVED FROM THE ENGINE MOUNT INSTALLATION WERE STAMPED WITH PN NAS464P864. REPLACEMENT BOLTS ORDERED FROM CESSNA UNDSDR SIMA200317607Rivet · lightning strikeABI - DURING A LIGHTNING STRIKE INSPECTION ONE RIVET AT STRINGER 6R, 2 INCHES FORWARD OF FRAME 34 WAS FOUND DAMAGED. REMOVED DAMAGED RIVET AND PERFORMED A CIRCULAR CUTOUT .6 INCHES IN DIAMETER. FABRICATED A REPAIR PLUG, REPAIR DOUBLER. REPAIR DONE IAW BME I
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