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 = '5240' 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 = '5240' 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 JBXA9900072Latch · not securedEXTREMELY LOUD SQUEAL EMANATING FROM RIGHT NOSE COMPARTMENT IN FLIGHT. FOUND LATCH ON GROUND SERVICE DOOR LOOSE (NOT SECURED), LATCHED DOOR.SDR ASAA9940057Lever · bentPDX - DURING MAINTENANCE CHECK, THE R1 DOOR WOULD NOT STAY OPEN WITH THE LEVER ASSEMBLY. REPLACED HOLD OPEN LEVER ASSEMBLY AND DOOR REMAINS OPEN NORMALLY. (M)SDR TWAA9903207Beam · crackedDURING OP-9, FOUND .5 INCH CRACK IN THE TOP BEAM AFT CORNER OF THE FWD RT SERVICE DOOR. REPAIRED PER THE SRM 52-51.D.SDR UIEA9909Skin · damagedFLT GT065 - ATB - APPROX 3.5 HOURS INTO THE FLIGHT, AND ADDITIONAL CARGO CHECK WAS MADE AN A HOLE APPROXIMATELY 1 FT SQUARE WAS DISCOVERED AT THE BOTTOM LEFT CORNER OF R4 MED. AIRCRAFT WAS AT FL 33, PRESSURIZATION WAS NORMAL (8.3). AFTER AIRCRAFT RETURNED TOSDR ASAA9940054Mechanism · lack of lubeLAX - PRIOR TO FLIGHT 675, THE L2 DOOR WAS REPORTED AS BINDING. LUBRICATED DOOR AND DOOR OPERATED NORMALLY. (M)SDR ABXA9900291Pan · crackedDURING C-CHECK, FOUND CRACK IN FORWARD SERVICE DOOR PAN AT SECOND DOOR STOP FROM BOTTOM, FORWARD SIDE OF DOOR. REPAIRED IAW ABX REA D853-27050MR.SDR SWAA990362Skin · crackedDURING SCHEDULED 1/2D CHECK, FOUND 2 DOOR SKIN CRACKS COMING OUT OF THE SAME RIVET HOLE. FIRST CRACK IS .375 INCH LONG, SECOND IS .75 INCH LONG, AT LOWER AFT CORNER JUST ABOVE LOWER GATE HINGE. REPAIRED CRACK PER SRM.SDR SWAA990361Skin · crackedDURING SCHEDULED C3 CHECK, FOUND FORWARD SERVICE DOOR HAS 1.25 INCH CRACK AT LOWER AFT CORNER. CRACK IS .75 INCH FROM O/B SIDE AND .5 INCH FROM BOTTOM. REPAIRED PER SWA RA 1-753-2024.SDR P2EA99118Mechanism · corrodedSJO - DURING Q-CHECK, THE R2 DOOR HANDLE MECHANISM HOUSING WAS FOUND WITH CORROSION AT THE LOWER TORQUE TUBE POSITION. REWORKED BEARING BORE AND MOUNTING HOLES AS PER OHM 52-46-05. (M)SDR P2EA99117Bearing · corrodedSJO - DURING Q-CHECK, THE R1 DOOR WAS FOUND WITH CORROSION ON THE UPPER TORQUE TUBE BEARING POSITION. THE BEARING BORE AND MOUNTING HOLES WERE REWORKED AS PER OHM 52-46-06. (M)SDR USAA990123Rivet · brokenPIT - DURING C-3 CHECK, FOUND TWO RIVET HEADS POPPED AT NR 1 HORIZ BEAM FORWARD END ON OUTER SKIN OF SERVICE DOOR. REPAIRED AND REPLACED RIVETS PER SRM 52-01 PAGE 1. (M)SDR SWAA990348Gate · bentAT FL330 LOST CABIN PRESS, WARNING HORN SOUNDED AND GAUGE READ 10,000 FT. ATTEMPTED TO RECOVER ALT WITH STANDBY, BUT MANUAL AC WORKED. ALT 3500 FT AFTER EMER DESCENT TO FL240. PACKS HAD TO REMAIN ON HIGH TO KEEP PRESS. SUSPECTED FWD SERVICE DOOR SEAL. FOUSDR UPS99228767Door · corrodedINSPECTION TYPE-C, MGD OUTER SKIN CORRODED BETWEEN LOWER LT FRAME AND PRE-EXISTING REPAIR DOUBLER. FOUND SKIN CRACKED AND BLENDED ALL CORROSION, CUT OUT ALL DAMAGED SKIN, FABRICATED FILLER AND DOUBLER AND INSTALLED IAW SRM 52-00-3.SDR TWAA9902902Beam · crackedFOUND THE FORWARD RIGHT CABIN DOOR HAD THE BOTTOM DOOR BEAM CRACKED. INSTALLED NEW DOOR BEAM PER SRM 51-30-2. CHECK-C 8-27-98 STL.SDR QXEA9900398Frame · damagedPDX - UPPER AFT CORNER OF SERVICE EMERGENCY DOOR SURROUND REQUIRED REPAIR PS REPAIR PATCH. REPAIRED IAW HORIZON AIR EA 4-53-685.SDR QXEA9900399Frame · damagedPDX - FORWARD LOWER CORNER OF SERVICE EMERGENCY DOOR SURROUND REQUIRES REPAIR PATCH. REPAIRED IAW HORIZON AIR EA 4-53-685.SDR QXEA9900397Frame · damagedPDX - AFT LOWER CORNER OF SERVICE EMERGENCY DOOR SURROUND REQUIRES REPAIR PATCH. REPAIRED IAW HORIZON AIR EA 4-53-685.SDR USAA990085Skin · crackedTPA - DURING CX-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN DOOR SKIN FORWARD SERVICE DOOR UPPER HINGE CUTOUT DOOR EXT SKIN. INSTALLED DOUBLER PER SB 737-32-1016, EA 63767 AND TR 52-40-03A. (M)SDR CALA9900095Beam · crackedINSPECTION FOUND A .5 INCH CRACK IN FORWARD SERVICE DOOR NR 4 HORIZONTAL BEAM. THE BEAM WAS REMOVED AND REPLACED IAW SRM 51-30.SDR DHL9980577CDoor · delaminatedAT C-CHECK, RT WING ACCESS DOOR 557A DELAMINATED AT LOWER SURFACE. REMOVED AND INSTALLED SERVICEABLE DOOR PER SRM 51-3-0. N/R 102SDR USAAD99018Seal · malfunctionedCLT-BUF - FLT 1223 - AFTER TAKEOFF, THE CABIN WOULD ONLY PRESSURIZE TO 1 PSI WITH THE OUTFLOW VALVE FULLY CLOSED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED SEALANT FROM THE AFT GALLEY SERVICE DOOR FRAME AND APPLIED FSDR DL72S990137Frame · crackedFOUND AT A-1 LETTER CHECK, .5 INCH VISIBLE CRACK ON AFT FRAME OF R-1 DOOR AT FWD SIDE OF LWR STOP CASTING. REPAIRED PER MM 52-12-0.SDR CA990310028Bolt · snapped(CAN) FORWARD SERVICE DOOR GUST DAMP MOUNTING PLATE BOLTS FAILED. BOLTS REPLACED.SDR CALA9900032Beam · crackedFORWARD SERVICE DOOR NUMBER 4 BEAM CRACKED AT AFT SIDE RADIUS 3/4. INSTALLED NEW BEAM PER SRM 51-30.SDR CALA9900025Beam · crackedFORWARD SERVICE DOOR HORIZONTAL BEAM HAS 4 CRACKS IN RADIUS WHERE LOWER HINGE ATTACHES. REPLACED HORIZONTAL BEAM PER SRM 51-30-2.SDR ABXA9900110Skin · crackedTWO LIGHTENING HOLES IN FORWARD, LEFT SERVICE DOOR STRUCTURE WERE CRACKED. REPLACED SKIN PANEL IAW DC8 SRM 51-1-8, 51-3-0 AND DWG 5755530.SDR ABXA9900109Door · crackedLEFT CENTER SERVICE DOOR HAD CRACK IN STRUCTURE. INSTALLED DOUBLER IAW DC8 SRM 51-1-8 AND 52-2-0.SDR ABXA9900052Structure · crackedLEFT CENTER SERVICE DOOR HAD CRACK IN STRUCTURE. REPAIRED AND INSTALLED DOUBLER IAW DC8 SRM 51-1-8 AND 52-20-0.SDR AU990050Bushing · loose(AUS) RIGHT FORWARD SERVICE DOOR LOWER CONNECTION LINK BUSHING MIGRATED.SDR 9900183263Cylinder · bindingWHILE PREPARING TO CATER AIRCRAFT, IT WAS REPORTED THAT THE AFT RIGHT CABIN DOOR WOULD NOT FULLY OPEN AND LATCH. MAINTENANCE REPLACED THE DOOR DAMPER/ASSIST CYLINDER, OPERATIONAL CHECK OK.SDR USAAD99010Mechanism · out of sequenceCLT/ORD - FLT 1527 - AFTER TAKEOFF, THE CREW WAS UNABLE TO PRESSURIZE THE AIRCRAFT IN EITHER THE AUTO OR MANUAL MODE. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT AFT SERVICE DOOR MECHANISM OUT OF SEQUENCE AND NOSDR DHL9980573CDoor · delaminatedAT C-CHECK, RT WING DOOR ACCESS PANEL DELAMINATED NR 577B. REMOVED, REPAIRED AND REINSTALLED PER SRM 51-3-0. N/R 251SDR DHL9980578CDoor · delaminatedAT C-CHECK, RT WING ACCESS DOOR NR 540 DELAMINATED. REMOVED AND REINSTALLED OVERHAULED DOOR PER MM. N/R 103SDR VNAA9901012Seal · failedTHE AIRCRAFT RETURNED TO THE FIELD DUE TO THE COMMUNICATION DOOR FAILING TO SEAL. MAINTENANCE INSPECTED AND RE-SEALED THE COMMUNICATION DOOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 51-22-00. OPERATIONAL CHECKS WERE SATISFACTORY, AND THE AIRCRAFT WAS RESDR CA990308035Door · not secured(CAN) FUEL PANEL DOOR OPEN LIGHT ON TAKEOFF ABORTED, NR 4 AND NR 8 BRAKES OVERHEATED. LATCHES ON FUEL PANEL DOOR ADJUSTED.SDR USAA990001Pan · crackedPIT - DURING C-CHECK, FOUND 1 INCH CRACK IN FORWARD SERVICE DOOR PAN AFT SIDE AT HORIZONTAL BEAM END NR 6. INSTALLED PAN SPLICE (-39) PER SRM 52-05 FIG 27. (M)SDR USAA990000Pan · crackedPIT - DURING C-4 CHECK, FOUND 1.5 INCH LONG CRACK IN SERVICE DOOR PAN AT NR 6 HORIZONTAL BEAM AFT END. SPLICED IN NEW PAN SECTION PER SRM 52-05 FIG 27 VIEW T-T. (M)SDR DL72S990027Frame · crackedFOUND ON D2 LETTER CK, .75 INCH CRACK IN R-1 DOOR AFT LOWER FRAME. REPAIRED PER MM 52-12-0.SDR VNAA9901001Service Door · lack of lubeA GROUND SERVICE DOOR OPEN WARNING MESSAGE ILLUMINATED DURING THE TAKEOFF. THE TAKEOFF WAS ABORTED, AND THE AIRCRAFT RETURNED TO THE GATE FOR INSPECTION. MAINTENANCE INSPECTED AND LUBED THE GROUND AIR SERVICE DOOR, IN ACCORDANCE WITH STANDARD MAINTENANCE PRASDR ASAA9880265Hook · defectiveSEA - DURING MAINTENANCE CHECK, THE L2 DOOR WOULD NOT LATCH OPEN. REPLACED THE DOOR HOLD OPEN HOOK AND OPERATED NORMALLY. (M)SDR SWAA983053Strap · out of positionAFTER TAKEOFF LOUD BANGING NOISE HEARD BY CABIN CREW IN FWD SERVICE DOOR AREA. NOISE GOT LOUDER WITH INCREASED AIRSPEED. AIRCRAFT RETURNED TO PDX AND FOUND FWD SERVICE DOOR STRAP OUTSIDE A/C THROUGH HINGE. FOUND SIX INCHES OF SAFETY STRAP PROTRUDING FROM LOSDR DL72S982466Skin · crackedREF SHIP 497 TPA LTR CHK C2, TWO SMALL CRACKS UPPER AFT CORNER UPPER HINGE CUTOUT, R1 DOOR SKIN. REPAIRED PER MM 52-11-01.SDR ASAA9880248Mechanism · out of adjustSEA - DURING MAINTENANCE CHECK, THE L2 DOOR WOLD NOT LATCH OPEN. ADJUSTED DOOR HOLD OPEN MECHANISM AND OPERATED NORMALLY. (M)SDR 98UAL900567Mechanism · wornFORWARD SERVICE DOOR LIGHT CAME ON. INSIDE D00R HANDLE POPS TOWARDS OPEN 3 TO 4 INCHES FROM LOCKED POSITION. TRIED TO PUSH HANDLE DOWN BUT IT POPPED BACK UP. DOOR 1R WAS ADJUSTED PER MM/OV 70-52-11-00. UPPER LATCH CAM WAS BACKED UP TWO SERRATIONS TO COMPENSDR P2EA98268Beam · crackedSJO - FORWARD SERVICE DOOR NR 7 BEAM CRACKED, DEFECT SIZE LENGTH .5 INCH. REPAIRED FUSELAGE SKIN FORWARD ENTRY DOOR BEAM NR 7 BETWEEN BS 302 AND BS 309 PER SRM 51-40-3 FIG 1. (M)SDR CKSA98708Gate · corrodedRT NR 1 DOOR UPPER GATE ASSY CORRODED ALONG HINGE AREA. REMOVED CORROSION IAW SRM 51-10-01, FOUND TO BE BEYOND LIMITS. REPLACED UPPER GATE ASSY IAW BOEING ASA CKF-MED-016, SRM 51-30-02 AND ADJUSTED DOOR IAW MM 52-11-01. FOUND DURING ACCOMPLISHMENT OF CARGO SDR SWAA982954Frame · crackedDURING SCHEDULED D CHECK, FOUND FWD SERVICE DOORWAY UPPER FWD FRAME CRACKED AT BS 296, RBL 48, WL 269. REPLACED PER BOEING SRM.SDR COMA9810270Latch · not securedSERVICE DOOR WARNING DURING CLIMBOUT. AIRCRAFT RETURNED TO THE FIELD. CLOSED DOOR AND SECURED LATCH.SDR USAASB98301Arm · out of adjustCLT - FLT 1583 - DURING CLIMB-OUT FROM CLT, AIRCRAFT WOULD NOT PRESSURIZE. THE AUTO FAIL LIGHT ILLUMINATED AND THE SYSTEM SWITCHED TO STANDBY MODE. THE OUTFLOW VALVE INDICATED FULL CLOSE, BUT THE AIRCRAFT WOULD NOT PRESSURIZE. FLIGHT ATTENDANT THEN ADVISED SDR TWAA9818201Beam · crackedDURING CHECK-C MAINT, FOUND ON THE RT FWD SERVICE DOOR THE NR 5 BEAM HAD A CRACK AT THE AFT END OF THE BEAM CLIP AT I/B RIVET HOLE. REPLACED CLIP FASTENER PER SRM 51-30-5 AND SERVICE BULLETIN 52-125 R4.
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