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 = '2810' 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 = '2810' 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 UIEA2024092400936Fuel Cell · leakingRH WING, FUEL LEAK ON LOWER SKIN AND SPLICE BTW WBL 97.95. TO WS 226.3 AND BTW STGR L7 TO L15(<P>FUEL LEAK WAS REPAIRED AND LEAK TEST WAS SATISFACTORY IAW AMM 28-11-00-308-013</P>)SDR UIEA2024092700960Fuel Cell · leakingRH WING, LOWER SKIN BETWEEN WBL 97.95 TO WS 226.3 AND STGR 10 WITH EVIDENCE OF FUEL LEAK(<P>FUEL LEAK WAS REPAIRED IAW AMM 28-11-00-308-013. LEAK CHECK GOOD</P>)SDR SCNA20241019332Fuel Tank · corrodedDEFECT WO FS240124: CORROSION FOUND AT LH SIDE OF THE CENTER TANK OUTER SKIN STA 663.75 UPON REMOVAL OF THE PICKEL FORK NEXT TO O/B UPPER HOLE. - - RESOLUTION: COMPLIED WITH EA 24011 REV IR AT LH SIDE OF THE CENTER TANK OUTER SKIN STA 663.75 NEXT TO O/B UPPERSDR IPXA2024092845296Fuel Tank · faulted*DIVERSION* ALL FOUR INNER TANKS FAULTED AT CRUISE FLIGHT REMOVED AND REPLACED RELAYS 133QA & 154QA PER ESPM 20-46-50. FUNCTIONAL TEST OF FUEL PUMP AUTOFEED SYSTEM OPS CKS GOOD PER A300 AMM 28-21. MEL DMP PROCEDURES REVERSED. THIS CLEARS MEL/PLACARD REMOVED.SDR VNAA202409240033Canister · crackedCRACK ON CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL LH MAIN FUEL TANK. CRACK ON CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577. REV.- -SDR VNAA202409240031Canister · crackedCRACKS ON CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL RH MAIN FUEL TANK. CRACKS ON CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577. REV.- -SDR IPXA2024092466148Fuel Sys · malfunctionedUNCOMMANDED FUEL MIGRATION RIGHT OUTER TANKSDR CALA2024092602483Fuel Cap · missingPDA 2 FUEL CAP FOUND MISSING IN THE MORNING SEE LOG PAGE 9334209 INSTALLED NEW CAP IAW AMM TASK 28-25-41-400-005-A PARTS USED: 31-2825-9-0001,QTY :1 1513309,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1513309 SN OFF 4879SDR N6WA2024091904Canister · crackedCRACK IN WELED CANISTER LOCATED IN RT WING FUEL TANK AT TRACK 1-3 SECTION 651AB. REPAIRED DAMAGE ON WELDED CANISTER LOCATED IN RT WING FUEL TANK TRACK 1-3 SECTION 651AB IAW REO 670-57-42-577.SDR CALA2024091700647Fuel Cap · missingPDA 2 FUEL CAP FOUND MISSING. ITEM PUT ON CDL 28A. REF LP# 9273271.FUEL CAP MISSING.REQUESTING CDL 28A CDL 28A APPLIED DISPATCH DESK: 14 NAME: BB DATE: 16-SEP-24 28A APPROVED.LOCATED MISSING REFUEL COUPLING CAP IN DEN. REINSTALLED REFUEL COUPLING CAP REF IPC SDR CALA2024091800653Fuel Cap · misconfiguredPDA 2 INSTALLED ACFT FUEL CAP NEEDS TO PAINTTHE MARKINGS IN ACCORDANCE WITH UAL DRAWING 1120DD12514 / ECRA5120-01013 REF AMM 28-25-41-200-001-A STEP 5.A.(4). . PAINTED FUEL CAP ALIGNMENT MARKINGS AS PER UAL DRAWING 1120DD12514 / ECRA5120-01013.SDR FDEA202409141323Stringer · crackedCENTER WING UPPER AUXILIARY TANK LEFT HAND COMPARTMENT STRINGER 47 FOUND CRACKED AT STATION XCW 17 APPROXIMATELY 4.75 . CENTER WING UPPER AUXILIARY TANK LEFT HAND COMPARTMENT STRINGER 47 AT STATION XCW 17 CRACKED AREA REPAIR CARRIED OUT AS PER MD-11 SRM 57SDR FDEA202409141322Stringer · crackedCENTER WING UPPER AUXILIARY TANK LEFT HAND COMPARTMENT STRINGER 47 FOUND CRACKED AT STATION XCW 46.5. CENTER WING UPPER AUXILIARY TANK LEFT HAND COMPARTMENT STRINGER 47 AT STATION XCW 46.5 CRACKED AREA REPAIR CARRIED OUT AS PER MD-11 SRM 57-10-03-2R REPAIRSDR 2024F00243Fuel Cap · installedPILOT DEPARTED WITH WATER IN FUEL; DUE TO FUEL TANK CAP IMPROPERLY SECURED, AND HEAVY RAINSDR CALA2024090600579Fuel Cap · missingPDA 2 FUELER REPORTS FUEL CAP MISSING FROM AIRCRAFT UPON ARRIVAL. PLACED ON CDL 28A. DISPATCH DESK: 13 NAME: JG DATE: 04-SEP-24- CDL 28A APPROVED. PLACED ON CDL 28A. FUEL CAP M&E 31-2825-9-0001 IPC 28-25-41-02B ITEM 001B. FUEL CAP M&E 31-2825-9-0001 IPC 28-SDR CALA2024090300540Fuel Cap · missingPDA 2 FUEL CAP MISSING ON ARRIVALFUEL CAP MISSING ON ARRIVAL. NO DAMAGE TO FUEL CAP COUPLING, NO FUEL LEAKING FROM FUELING FILL FITTING. REPLACED FUEL CAP IAW REF. AMM TASK 28-25-41-400-005-ASDR UIEA2024083000882Fuel Tank · leakingFUEL LEAK CENTER TANK AT LBL 60 AND STGR L-11(<P>FUEL LEAK CENTER TANK AT LBL 60 AND STGR L-11, THE SEALANT WAS REMOVED WHERE THE FUEL LEAK WAS FOUND, IT WAS CLEANED PROPERLY, THE SEALANT WAS APPLIED CORRECTLY. THE FUEL LEAK WAS REPAIRED. THE FUEL LEAK TEST WASDR UIEA2024083000880Fuel Tank · leakingFUEL LEAK RH TANK, BETWEEN WS 404.4 AND 433.1 AT STGR L-10(<P>FUEL LEAK RH TANK, BETWEEN WS 404.4 AND 433.1 AT STGR L-10, THE SEALANT WAS REMOVED WHERE THE FUEL LEAK WAS FOUND, IT WAS CLEANED PROPERLY, THE SEALANT WAS APPLIED CORRECTLY. THE FUEL LEAK WAS REPAISDR UIEA2024082800853Fuel · leakingRH WING LOWER SKIN, FUEL LEAK AT STG L-10 BTWN W.STA 284.7 AND 375.8. (RIB 5-8)(<P>RH WING LOWER SKIN, FUEL LEAK AT STG L-10 BTWN W.STA 284.7 AND 375.8. (RIB 5-8). SEALANT WAS REMOVED WHERE THE FUEL LEAK WAS, THE AREA WAS CLEANED AND THE FUEL LEAK WAS REPAIREDSDR UIEA2024082800849Splice · leakingRH WING, LOWER SIDE OF BODY SPLICE PLATES, AT RBL 97.95 AND BETWEEN STRINGER L-14 AND L-16 WITH EVIDENCE OF FUEL LEAKAGE(<P>RH WING, LOWER SIDE OF BODY SPLICE PLATES, AT RBL 97.95 AND BETWEEN STRINGER L-14 AND L-16 WITH EVIDENCE OF FUEL LEAKAGE. THE SEALANT WASDR SWAA2024100435149Support · corrodedCORROSION CENTER TANK ACCESS PLATE 531BB SUPPORT RING. 124-039<[01] REMOVED DAMAGE AT CENTER TANK ACCESS PLATE 531BB SUPPORT RING PER REF SRM 51-10-02-0G-0 FOUND OUT OF LIMITS PER REF SRM 57-20-01-2R-1;[02] RECEIVED NEW FUEL PLATE 531BB SUPPORT RING; PANEL WILSDR SWAA2024100435148Shim · corroded*CORROSION* CENTER TANK ACCESS PLATE 531AB SUPPORT RING. 124-038<[01] REMOVED DAMAGE AT CENTER TANK ACCESS PLATE 531AB SUPPORT RING REF SRM 51-10-02-0G-0 FOUND OUT OF LIMITS PER REF SRM 57-20-01-2R-1;[02] RECEIVED NEW FUEL PLATE 531AB SUPPORT RING; PANEL WILL SDR QMLA2024090320105Drain Valve · unknownFLIGHT MEDIC IN THE BACK OF THE AIRCRAFT STATED THAT HE THOUGHT HE SAW FLUID, WHICH HE THOUGHT WAS OIL, ON ONE OF THE THE CLAMSHELL DOOR WINDOWS. THERE WERE NO UNUSUAL COCKPIT INDICATIONS OR ODORS. WE HAD A BRIEF DISCUSSION ABOUT WHAT HE WAS SEEING AND I DECIDSDR AALA202408279988Sump · leakingAIRCRAFT WAS NOT GROUNDED: FUEL USED/ FUEL ON BOARD DISAGREE, ALTERNATED BETWEEN OVERREAD PROCEDURE AND FUEL LEAK PROCEDURE. FUEL USED AND FUEL ON BOARD MONITORED AND EQUALED TOTAL FUEL AT DEPARTURE GATE THROUGHOUT FLIGHT. MAINTENANCE FOUND THE RIGHT HAND FUELSDR DALA2024082408418Fuel Cell · corrodedAIRCRAFT 9546, CORROSION ON THE LOWER SKIN OF THE CENTRAL TANK APPROX. STA. Y=748 AND STA XCW=-25 AND Z=-29 IN THE FRONT WALL ON RH MLG WHEEL WELL. CORRECTIVE ACTION: LOWER SKIN OF THE CENTRAL TANK APPROX. STA. Y=748 AND STA XCW=-25 AND Z=-29 WAS REPAIRED PER SDR AALA202408213461Fuel Sys · leakingAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: AFTER TAKEOFF SNA TOWER INFORMED US OF LIQUID LEAKING FROM RIGHTSIDE OF AIRCRAFT. ALL COCKPIT INDICATIONS WERE NORMAL. FUEL LEAK QRH PROCEDURE APPLIED, NO FUEL LEAK NOTED; AIRCRAFT DIVERTED TO AND LANDEDSDR CALA2024081902230Fuel Cap · missingPDA 2 REF LOG PAGE 8920951, THE FUELER REPORTED THE FUEL CAP MISSING. CDL 28A ALREADY APPLIED FOR MISSING LANYARD. THE DEFERRAL LOG PAGE WAS UPDATED TO INCLUDE THE CAP.SDR QMLA2024081520100Fuel Cap · not seatedFUEL SMELL IN AFT CABIN. FOUND FUEL CAP NOT SEATED PROPERLY.SDR MPRC202408200001Fuel Sys · contaminatedENGINE STARTED RUNNING ROUGH AT TOD AND STOPPED PRODUCING POWER SHORTLY AFTER. AN EMERGENCY LANDING WAS MADE ON TUNDRA WITH NO DAMAGE. FUEL SUMPS AND GASCOLATOR WERE FOUND TO HAVE WHAT LOOKED LIKE "COTTON OR FILTER LIKE MATERIAL" WHICH WE BELIEVE WAS DRYER LINSDR CALA2024080900399Fuel Cap · missingPDA 2 FUEL CAP MISSING UPON ARRIVAL. FUEL CAP MISSING. VERIFIED NO LEAKS ON FUEL COUPLING. REQUEST CDL 28A. COMPLIED WITH CDL 28A. REF GMM 02-30-95 PARTS DEPARTING AIRCRAFT. NO PARTS RECEIVED. PARTS NIS IN JAX REPLACED FUEL CAP AND LANYARD REF AMM TASK 28-25SDR CALA2024081202189Fuel Cap · missingFUELER REPORT REFILL CAP MISSING UPON AIRCRAFT ARRIVAL VERIFIED NO DAMAGE AND NO LEAKS FROM REFUEL COUPLING. REQUEST CDL COMPLIED WITH CDL 28A.SDR CALA2024080900398Fuel Cap · missingPDA 2 FUEL CAP MISSING. SEAL INTEGRITY GOOD. REQUESTING CDL 28A DISPATCH DESK: 09 NAME: AB DATE: 06-AUG-24- CDL 28A APPROVED PLACARDSSDR SWAA2024080722166Fuel Sys · out of balanceAFTER TAKEOFF UNABLE TO MAINTAIN FUEL BALANCE NORMALLY TOTAL FUEL WAS DEPLETING MORE THAN NORMAL EXPECTED FUEL LEAK AND DIVERTED FLIGHT FUEL IMBALANCE WAS ABOUT #500 LBS IN 10 MINS RIGHT MAIN TANK DROPPING . AFTER REBALANCE OF FUEL QUANTITY WAS NORMAL BEFORE DSDR CALA2024080500358Cap · missingPDA 2 REF LP 8805737 FUELER REPORTED FUEL CAP MISSING UPON ARRIVAL. ITEM PREVIOUSLY PUT ON CDL 28A FOR MISSING LANYARD. REF LP 8805737.SDR CALA2024080500357Cap · missingPDA 2 FUEL CAP FOUND MISSING ON WALK AROUND. INFO INSTALLED NEW FUEL CAP REF AMM 28-25-41. ROTABLE FILLED AS INSTALL ONLY PARTS USED: 31-2825-9-0001,QTY :1 1515361,QTY :1 PARTS USED: 31-2825-9-0001,QTY :1 1515361,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED -SDR 2024FA0000629Fuel Line · broken#1 FUEL INJECTION LINE CAME APART AT SOLDER JOINT BY INJECTOR B-NUT. CYLINDER SHUT DOWN IN FLIGHT AND CAUSED A FUEL LEAK. AIRCRAFT MADE EMERGENCY LANDING AT MILITARY INSTALLATION. PART IS 1029.9 HOURS SINCE NEW FROM FACTORY. REPETITIVE INSPECTION UNDER AD I1SDR UIEA2024072200714Rod · wornLH WING, INNER ACCESS PANEL 521QB, OUTBD REFUEL COUPLING, BEARING ROD ASSY WITH WORN(<P>LH WING INNER ACCESS PANEL 521QB OUTBD REFUEL COUPLING ROD WAS REPLACED IAW AMM 28-21-01-404-010 REV 142 22APR2024 TORQUE APPLIED 100LB-IN TORQUE N/S=0524121894EB-2025. NO SDR UIEA2024072400741Fuel Tank · leakingRH AUXILIARY CENTER TANK AT L-6 AND WBL 97 WITH FUEL LEAK(<P>RH AUXILIARY CENTER TANK AT L-6 AND WBL 97 WITH FUEL LEAK. THE FUEL LEAK WAS EVALUATED, SEALANT REMOVED AND REPAIRED IAW AMM 28-11-00-308-013 REV 142 22APR24. THE TEST WAS SATISFACTORY.</P>)SDR AALA202407305857Fuel Panel · leakingAIRCRAFT WAS NOT GROUNDED: FUEL PANEL 531AB LEAKING FUEL. REMOVED AND CLOSED FUEL PANEL 531AB. LEAK CHECK GOOD. PER AMM 28-11-31.SDR CALA2024072600285Fuel Cap · missingPDA 2 REFUEL CAP MISSING FROM RIGHT WINGSDR AALA202407239998Seal · leakingAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND FUEL PANEL 632AB HAS FUEL LEAK. REMOVED AND REPLACED SEAL (AALA202407239998) AND GASKET (AALA202407232227). PERFORMED SATISFACTORY LEAK CHECK. NO LEAKS NOTED. PER B737 NG AMM 28-11-11.SDR AALA202407232227Gasket · leakingAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND FUEL PANEL 632AB HAS FUEL LEAK. REMOVED AND REPLACED SEAL (AALA202407239998) AND GASKET (AALA202407232227). PERFORMED SATISFACTORY LEAK CHECK. NO LEAKS NOTED. PER B737 NG AMM 28-11-11.SDR YENA2024071901013Probe · failedFLT#8042, DUB-JFK. (ETOPS) 'FUEL (R) OUTER TANK HI TEMP. TEMP WENT UP TO 61 C AND WE SHUT OFF GENERATOR. TEMPERATURE DROPPED TO 49 - -3 C. REPEAT GRIPE. ( CAUTION ON ECAM 2) TK HI TEMP (LEFT, RIGHT WING TANK) ); FUEL TEMP PROBE 54QT2 FAULTING. REMOVED AND REPLSDR VNAA202409010007Duct · crackedCRACK ON AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH. AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH. (SM) WAS REPAIRED PER PER. REO. 690-28-25-023 REV.--SDR UIEA2024070400579Fuel Tank · leakingFUEL LEAK ON LOWER SURFACE OF CENTER TANK RIGHT SIDE AT RBL 97.42(<P>FUEL LEAK ON LOWER SURFACE OF CENTER TANK RIGHT SIDE AT RBL 97.42 WAS REPAIRED IAW AMM 28-11-00-308-013 REV 142 22APR24. THE FUEL LEAK TEST WAS SATISFACTORY.</P>)SDR DALA2024070806934Fuel Cell · damagedSHIP 3132 ELONGATED HOLE FUEL TANK LOWER SURFACE ON CUT OUT LOC. BTW RIB18 /19 ON RH WING. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON FUEL TANK LOWER SURFACE ON CUT OUT LOC. BTW RIB18/19 ON RH WING AS PER A319 SRM 57-21-11-300-002. (0430553)SDR YENA2024071100956Fuel Tank · corrodedDURING HEAVY MAINTENANCE: CORROSION ON UPPER SKIN BTW FR41/FR42 LH SIDE CENTER TANK AREA IN PASS ENGER CABIN; (RESOLVED ON W/O: 1308674 TASKCARD: NR-00050) REF AEROMAN N/R 2024-298788, REMOVED CORROSION MECHANICALLY LOCATED ON UPPER SKIN BTW FR41/FR42 LH SIDE SDR CALA2024070101931Fuel Cap · missingPDA 2 REFERENCE LP 8421939 FOR MISSING FUEL CAP. CONTACTED TOM C NEWMAN REFERENCE LP 8421939.SDR CALA2024062700106Ring · missingREFUEL CAP LANYARD MISSING KEYRING REQUESTING CDL 28A DISPATCH DESK: 31 NAME: SS DATE: 24-JUN-24- / OK TO DEFER PER CDL 28A C/W MAINTENANCE DDP. REMOVED FUEL CAP AND REPLACED CABLE ASSEMBLY REF AMM 28-25-41. REINSTALLED FUEL CAP. NO PARTS SDR CALA2024062701909Ring · missingREFUEL CAP LANYARD MISSING KEYRING REQUESTING CDL 28A C/W MAINTENANCE DDP. DISPATCH DESK: 31 NAME: SS DATE: 24-JUN-24- OK TO DEFER PER CDL 28A REMOVED FUEL CAP AND REPLACED CABLE ASSEMBLY REF AMM 28-25-41. REINSTALLED FUEL CAP. NO PARTS DEPARTED AIRCRAFT.
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