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 = '5200' 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 = '5200' 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 2007UALA00787Unknown · unknownDOOR 3L WILL NOT ARM. CYCLED ARMING HANDLE, DOOR ARMS NORMALLY. UNABLE TO DUPLICATE PROBLEM. SUSPECT F/A TECHNIQUE PROBLEM.SDR CALA0700091Pan · crackedUPPER FWD PAN CRACKED AT FWD SPLICE. INSTALLED SERVICEABLE PAN.SDR 2007UALA00509Latch · faultyLT OVERWING COMPARTMENT DOOR LATCH FAILED INTEGRATOR TORQUE TEST AT 275 INCH-LBS. REPLACED 4 SLIDE LATCHES PER MM25-65-09. DOOR TORQUE CHECK GOOD. LATCHES CHATTER IN LOCKED POSITION AND A FRET CHANNEL DEVELOPS OVER TIME.SDR VNAA0702012Door · openCREW REPORTED A LOUD NOISE COMING FROM THE RT SIDE ON CLIMBOUT. CREW RETURNED TO GSO AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE GROUND POWER SERVICE DOOR OPEN. MAINTENANCE CLOSED AND SECURED DOOR. NO DEFECTS NOTED. AIRCRAFT WAS RELEASDR P5CA0701514Handle · unsecureHIGH SPEED REJECT DUE TO OVERHEAD DOOR OPEN INDICATION. INSIDE HANDLE WAS AJAR. CHECKED OPERATION OF HANDLE AND HATCH. OPERATION NORMAL.SDR 2006UALA02107Door Frame · crackedFWD CARGO DOOR FWD AND AFT FRAMES CRACKED AT LOWER STOP FITTINGS. INSTALLED NEW FRAME SECTIONS. REFERENCE SRM 51-40-02.SDR 2006FA0000821Hinge · corrodedTO FIND USED SERVICEABLE HINGES AND HINGE SUPPORT FITTINGS FROM AC SALVAGE COMPANIES, EVERY HINGE THAT WAS RECEIVED, SAME TYPE OF CORROSION, BEARING AND BUSHINGS WERE RUSTED TO HINGE BOLT. BUSHINGS AND BEARING ARE PRESS FIT INTO HINGE SO AS TO ALLOW HINGE ASSDR SIMA200619806Door · openON TAKEOFF AND CLIMB-OUT CREW SUSPECTED COMMUNICATION OR GPU DOOR OPEN. AIRCRAFT RETURNED TO CLE. UPON ARRIVAL TO GATE FOUND GPU DOOR OPEN, INSPECTED AREA AND FOUND NO DEFECTS, GPU DOOR OPERATED NORMALLY. AIRCRAFT RETURNED TO SERVICE. (M)SDR SIMA200619405Door · unsecureFOUND EXTERNAL POWER DOOR WAS LEFT OPEN. RETURNED TO ORD. FOUND EXTERNAL POWER DOOR OPEN. INSPECTED FOR DAMAGE AND NO DAMAGE FOUND. CLOSED DOOR PER STANDARD MAINTENANCE PRACTICES. AIRCRAFT RETURNED TO SERVICE. (M)SDR TRAX200600240Handle · crackedAVIONICS BAY OUTER HANDLE APPEARS CRACKED.SDR VNAA0604003Access Door · openDURING CLIMBOUT THE CREW DETERMINED THE EXTERNAL SERVICE PANEL ACCESS DOOR WAS OPEN. THE FLIGHT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE CONFIRMED THE OPEN DOOR. INSPECTION OF THE DOOR AND FUSELAGE REVEALED NO DEFECTS. THE DOOR WAS PROPERLYSDR C2XA06CL037Door · brokenCLE FLIGHT NR 2541, CREW REPORTED AIRCRAFT WOULD NOT PRESSURIZE. AIR RETURN. MAINTENANCE INSPECTED FOUND AIR SERVICE CHECK VALVE DOOR BROKEN. DOOR ASSEMBLY REMOVED AND REPLACED. ALL OPERATIONAL CHECKS REPORTED GOOD.SDR VNAA0603006Door · openAFTER TAKEOFF THE CREW DETERMINED THE GROUND COMMUNICATION DOOR WAS OPEN. THE FLIGHT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE CONFIRMED THE OPEN DOOR. INSPECTION REVEALED NO DISCREPANCIES. THE DOOR WAS PROPERLY SECURED AND THE AIRCRAFT WAS SDR VNAA0602005Door · openDURING CLIMBOUT THE CREW REPORTED AN OPEN ACCESS DOOR. THE FLIGHT RETURNED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE SERVICE PANEL DOOR OPEN. THE DOOR AND FUSELAGE WERE INSPECTED. NO DISCREPANCIES WERE FOUND. THE DOOR LATCHES OPERATIONALLYSDR MASA200600387Ring · missingASH 7163 IAD - FLIGHT DECK DOOR LOWER HINGE EXTRACTION RING MISSING AND LEFT OVERWING EXIT HANDLE COVER LOOSE. MX INSTALLED A NEW RING TO THE LOWER HINGE PIN AND SECURED THE PANEL WITH NEW VELCRO.SDR USAA060182Door · corrodedR3 DOOR DELAMINATION. NEW TOP SHEET INSTALLED PER TYP REP 53-02-01, DEFECT SIZE: 15 X 15 INCH.SDR UPS06146042Intercostal · bentINSPECTION TYPE:5YR APPROX FROM FS 85 TO 86 INTERCOSTAL JUST AFT OF 310 ACCESS DOOR IS BENT. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-00.SDR VNAA0512021Access Door · openDURING CLIMBOUT THE CREW REPORTED AN OPEN ACCESS DOOR. THE FLIGHT RETURNED TO SRQ AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AC ELECTRICAL GROUND POWER DOOR OPEN. THE DOOR WAS INSPECTED AND NO DAMAGE WAS FOUND. THE DOOR WAS PROPERLY SECURED AND THESDR 05FDEA04284Repair · unknownFOUND MAIN CABIN CTR FUSELAGE R-3 DOOR AFT JAMB HAS AN EXTERNAL DOUBLER BOTTOM PART DIM 11" BY 12" STA 1311. PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 53-50-00 FIG 19 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2.SDR ASAA0540683Access Door · crackedYXX - E/E COMPARTMENT ACCESS DOOR OUTER SURFACE IS DENTED/CRACKED. OUTER SURFACED REPAIRED IAW B737-400 SRM 52-00-01 FIG 201. (M)SDR QXEA200501502Latch · inoperativePDX FLIGHT NR 2208 - GALLEY BREAKER PANEL DOOR INOP. MAINTENANCE RELATCHED GALLEY BREAKER DOOR AS REQUIRED. NO PARTS REPLACED. OPERATIONAL CHECK GOOD.SDR 05FDEA03459Access Door · out of positionA/C TOOK OFF AND RETURNED TO GATE. FLT CREW SAID THE A/C WOULD NOT PRESSURIZE. MAIN ENTRY DOOR WAS CLOSED DOOR WAS JAMMED WOULDN'T OPEN. REMOVED DOOR SLIDE DOOR TRIM FOUND THE AFT ROLLERS WERE NOT IN THE ROLLER GUIDES OR IN THE CAMS. FOUND SOLID BULKHEAD ASDR VNAA0510005Door · openSHORTLY AFTER TAKEOFF THE CREW REPORTED A LOUD POPPING NOISE NEAR THE NOSE OF THE AIRCRAFT. THE FLIGHT RETURNED TO CLT AND LANDED SAFELY. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE EXTERNAL SERVICES PANEL DOOR OPEN AND A HEADSET PLUG ADAPTOR PLUGGED INSDR 2005UALA01036Door · separatedDIVERTED TO YQX DUE TO AIRFRAME VIBRATION. RAM AIR INLET DOOR ASSY WAS FOUND WITH FORWARD INLET DOOR ASSY P/N 213T3010-1 MISSING. AFT HINGE ASSY P/N 213T3108-4 ATTACHING THE FORWARD AND AFT INLET DOOR ASSY WAS ALSO MISSING. FORWARD HINGE ASSY P/N 213T3109-4SDR MASA200500747Access Panel · unsecureASH 7102 BNA - CREW O2 ACCESS PANEL OPENED IN FLIGHT. MX INSPECTED PANEL FOUND NO DAMAGE AND RESECURED IT.SDR ASAA0580479Door · dentedOKC - DURING C-CHECK, FOUND PREVIOUSLY REPAIRED AREA OF FUSELAGE BELOW EXTERNAL POWER DOOR IS DENTED. REMOVED DAMGAED AREA. INSTALLED REPAIR DOUBLER. (M)SDR ASAA0580475Access Panel · interferenceSEA LINE CHECK - WHILE ATTEMPTING TO GAIN ACCESS TO A PANEL ON THE UPPER SURFACE OF THE LEFT WING VIA ONE OF THE OVERWING EMERGENCY EXIT DOORS, IT WAS DETERMINED THAT NOT ONLY WAS THAT DOOR DIFFICULT TO OPEN, BUT THAT ALL OVERWING DOORS WERE DIFFICULT TO OPEN.SDR ABXA050186Access Door · unlatchedON T/O, NO PRESSURIZATION, CABIN CLIMBED AT SAME RATE AS AIRCRAFT. AC PACKS SHOWED 27 PSI ON BOTH SIDES, CABIN FLOW CONTROL VALVE WAS FULLY CLOSED. INSPECTED A/C FOUND ALL EXTERIOR DOORS CLOSED. FOUND AFT BULKHEAD ACCESS DOOR UNLATCHED. RESECURED DOOR. SDR VNAA0507016Door · openTHE CREW REPORTED A LOUD NOISE ABOVE 210KTS DURING CLIMBOUT. THE FLIGHT RETURNED TO CLT WHERE MAINTENANCE DISCOVERED THE EXTERNAL SERVICE PANEL DOOR OPEN. THE DOOR WAS INSPECTED AND OPERATIONALLY CHECKED. NO DAMAGE WAS FOUND AND THE LATCHES FUNCTIONED PROPESDR VNAA0506010Access Door · openAFTER TAKEOFF THE CREW HEARD SOUNDS FROM THE RT SIDE OF THE FWD FUSELAGE THAT INDICATED AN ACCESS PANEL WAS OPEN. THE FLIGHT RETURNED TO CLT. MAINTENANCE FOUND THE GROUND SERVICE PANEL (HEADSET) ACCESS DOOR OPEN. THE DOOR WAS VISUALLY INSPECTED. NO DAMAGE SDR VNAA0505014Access Door · openDURING CLIMB THE STALL FAIL WARNING MESSAGE ILLUMINATED. THE CREW RETURNED TO CLT. MAINTENANCE INTERROGATED THE MDC AND FOUND NO FAULT CODES. THE STALL WARNING SYSTEM OPERATIONALLY CHECKED GOOD. THE OXYGEN SERVICING DOOR WAS FOUND OPEN ON THE RIGHT SIDE OFSDR 05FDEA00526Skin · damagedREPAIR AT STN 2135 FS 38.1 STN 2188 FS 38.2 STR 49 LT, AIR CONDITION ACCESS DOOR. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-72-10 AND 51-40-21.SDR COMA0560150Door · openFLIGHT 5554 LOUD SQUEAL FROM NOSE AREA OF AIRCRAFT. FOUND 02 SERVICE DOOR OPEN. INSPECTED FOR DAMAGE AND CLOSED 02 SERVICE DOOR.SDR DHL2004809505Door · crackedEXTERNAL FUSELAGE D-BELLY DOOR FWD UPPER CORNER JAMB CRACKED 0.750, STA 1400.000 L-26.5R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW AD2004-06-06, SB DC8-53-078 REV-1, DWG SRO8530019 CONFIGURATION G, DWG 5750776. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMSDR USAA041062Skin · crackedCLT - FOUND SKIN CRACKED .375 INCH, LOWER FORWARD CORNER OF AFT CARGO DOOR, 2ND HOLE FROM LEFT. INSTALLED DOUBLER IAW EA 96069. (M)SDR 2005FA0000003Door Frame · crackedDURING AIRCRAFT 4000 LANDING INSPECTION, FOUND APPROX A 1 INCH CRACK AT THE UPPER FORWARD RADIUS OF DOOR FRAME. STOP DRILLED CRACK AND REPAIRED WITH AN OVERLAY DOUBLER IAW THE SRM. OVERLAY INSTALLED (WET) WITH PRC 1440. (K)SDR VNAA0411005Access Door · openAFTER TAKEOFF THE CREW OF FLIGHT 2302 NOTICED A LOUD WHINE FROM THE FIRST OFFICERS SIDE PANEL AREA. THE AIRCRAFT RETURNED TO CLT WHERE MAINTENANCE FOUND THE AC ELECTRICAL-GROUND POWER ACCESS DOOR OPEN. THE DOOR WAS INSPECTED IAW CRJ 200 AMM 52-45-00-210-801 SDR 04319639Access Panel · openEVENT SUMMARY STATED THAT MX ACCESS PANEL DOOR OPEN. INSPECTED PANEL AND DEFECTS FOUND TO DOOR OR AIRFRAME. OK TO CONTINUE SERVICE.SDR VNAA0410011Warning Light · false activationDURING CRUISE THE CREW REPORTED A CARGO DOOR CAS MESSAGE. MAINTENANCE CONTROL DEFERRED THE CARGO DOOR INDICATION SYSTEM WITH THE CREW PER MEL 52-70-04 CODE-C.SDR 72300216Skin · corrodedCORROSION ON INTERIOR DOOR SKIN.SDR UPS04243236Door · crackedINSPECTION TYPE:C, SUSPECT CRACK AT ATTACH LUG OF TAIL SKID DOOR AND STRUT. HFEC CARRIED OUT IAW NDT MANUAL 51-00-00. RESULT - CRACK CONFIRMED. INSTALLED NEW TAIL SKID DOOR IAW MM 32-71-61. TAIL SKID TESTED SATISFACTORY IAW MM 32-71-01.SDR ABXA040303Rib · crackedP-DOME PLUG DOOR NR 9 STOP SUPPORT RIB CRACKED. REPAIRED AREA IAW DC-9 SRM 52-05.SDR IXXA0400090SAccess Door · damagedDURING ROUTINE C CHECK INSPECTION, FOUND FWD FUSELAGE (02 EA) INTERIM REPAIRS ON EXHAUST DOOR SYSTEM CORNERS AT STA 40,000 L-31L. REPAIRS WERE ACCOMPLISHED BY PERFORMING THE FOLLOWING REPAIRS IAW DC8 SRM 53-2-0 FIG 13. REMOVED INTERIM REPAIR IAW DC8 SRM 51-1SDR 2004FA0000146Hinge · wornTHE ORIGINAL HINGE MFG OF ALUMINUM WORE OUT AND DROPPED PIECES IN THE INTAKE, CAUSING DAMAGE TO THE TURBOCHARGER. SERIOUS DAMAGE WAS AVOIDED BY A TIMELY INSPECTION. THE NEW SUPPLIED PART IS STAINLESS STEEL WITH A HINGE PIN SECURED BY CRIMPING. THIS AREA IS SDR DL76L040151Latch · corrodedDURING OFFWING SLIDE COMPARTMENT DOOR LATCH INSPECTION OPN 5894AD, MISC HARDWARE FOUND TO BE CORRODED. REPLACED DELTA PART NUMBERS: 251211768, 011216100, 251210507, 251210349, 011214656, MFG 416T2824-3, 416T2075-1, 416T2836-9, NAS43HT4-10, BACT32G64-1072, 251SDR ABXA040046Hinge · crackedFITTING ABOVE UPPER HINGE ON AFT PRESSURE BULKHEAD DOOR WAS CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR USAASB03215Door Seal · failedDURING CRUISE, EN ROUTE FROM IND-CLT AT FL290, A LOUD BANG WAS HEARD FROM THE FORWARD GALLEY AREA, FOLLOWED BY THE CABIN ALTITUDE CLIMBING UNCONTROLABLLY. CREW REPORTED THE OUTFLOW VALVE WAS IN THE FULL CLOSED POSITION. THE OXYGEN MASKS DEPLOYED AND BOTH TE SDR ASOA03646Fitting · crackedDURING A C-CHECK IN MCN, THE FORWARD CABLE ANCHOR MOUNT FITTING ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE FORWARD CABLE ANCHOR MOUNT FITTING ON THE PASSENGER DOOR. (M)SDR ASOA03597Anchor · crackedDURING HANGAR MAINTENANCE IN MCN, THE AFT ANCHOR ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFT ANCHOR ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)SDR ABXA030400Door · crackedAFT PRESSURE BULKHEAD DOOR CRACKED AT LOWER HINGE. REPLACED AREA NOTED IAW DC-9 SRM 52-05, 51-30-5 AND 51-30-1.
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