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 = '5711' 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 = '5711' 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 COEA2025061815913Spar · corrodedHEAVY CHECK COE/MAJOR REPAIR: R/H WING REAR SPAR UPPER CHORD STRIP SLAT HAS LEVEL 2 CORROSION BETWEEN RIBS 13RH-13LH. CORRECTIVE ACTION: REPAIRED PER SRAS ES_00254441_01...25315 ISSUE A, DATED 5/27/2025.SDR COEA2025061713913Spar · corrodedHEAVY CHECK COE/MAJOR REPAIR: R/H WING AFT SPAR UPPER CHORD RIBS 13-18.SDR COEA2025061110913Spar · corrodedHEAVY CHECK COE/MAJOR REPAIR: RT WING AFT SPAR UPPER CHORD RIB 20-21 UPPER SURFACE HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED PER SRAS S572R0391. 14113 ISS D, DATED 2/14/2025.SDR COEA2025060608913Spar · corrodedWO 262004 NR 500020 HEAVY CHECK COE/MAJOR REPAIR: L/H WING FWD SPAR LOWER FLANGE RIB 13-14 HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED PER SRAS ES_00254433_01...24979 ISS A, DATED 2/26/2025.SDR DALA2025010300041Spar · buckled(LOG 0742065) LEFT WING REAR SPAR BUCKLED JUST OTBD OF RIB 26. REAR SPAR REPAIR ON ERA 622413-14 REV ORIG.SDR COEA2025060405913Spar · corrodedWO 262004 NR 500019 HEAVY CHECK COE/MAJOR REPAIR: L/H WING FWD SPAR UPPER FLANGE AT RIB 21 HAS LEVEL 2 CORROSION UNDER 2 NUTPLATES. CORRECTIVE ACTION: REPAIRED PER SRAS S572K0042...25110 ISS A, DATED 5/20/2025.SDR DALA2025020500872Spar Cap · cracked-AD- LEFT WING REAR SPAR LOWER CAP IB OF FLAP TRACK. CRACK INDICATION IN HOLE THAT IS 2 HOLES IB OF EXISTING CRACK, XRS 164. REF PRI 621050-14 REV 1 STEP 11 AND FIGURE 3. SUMMARY SEE NRC 006-0001:10-0557-8-8910/002 00039: REFERENCED PRI 621050-14 ALL REVISIONSSDR DALA2025020500871Spar · cracked-AD- VISIBLE CRACK FOUND ON LEFT WING REAR SPAR LOWER CAP IB OF FLAP TRACK, OB OF THE TE RIB CLIP BETWEEN XRS 150.450 AND XRS 164.000. SUMMARY SEE NRC 006-0001:10-0557-8-8910/001 00017: COMPLIED WITH PRI 621050-14 REV 0, REV 1, REV 2, REV 3, REV 4, REV 5, REV SDR JGVR20241216001Spar · damagedR&R FASTENERS AS REQUIRED, BLENDED 9 AREAS OF CORROSION ON LH WING AFT SPAR, LOWER CLIP, FWD SIDE, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED AND PRIMED BLENDED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR DALA2024123112105Spar · crackedCRACK AT LEFT WING REAR SPAR, PRI 623253-14 REV 0 ISSUED. REMOVE TANK PLATES 520FT, 520CB, AND TWO FUEL LINES FOR MAINTENANCE. REMOVED AND REINSTALLED L/H OVER WING BOOST PUMP PANEL TO F.O.M. PER B717 AMM 28-00. RE-INSTALLED TANK PLATE 520CB PER B717 AMM 28-00SDR DALA2024122712030Spar Cap · crackedCRACKS FOUND DURING INSPECTION OF LH WING REAR SPAR LOWER CAP RADIUS. CONTACT LIASON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT. FC 5720-01103 2ND FASTENER INBOARD OF FLAP HINGE FITTING EXTERIOR FROM TRAILING EDGE THROUGH FASTENER INTO RADIUS. MSDR 2024FA0000962Spar Cap · corrodedREPAIRED CORRODED AREA ON THE LH LOWER WING SPAR CAP LOCATED IN THE LH MLG WHEEL WELL BEHIND PANEL 730DL, BY R&R FASTENERS AS NEEDED, MECHANICAL BLENDS, PERFORMING NDT AND REPORTING FOR REPAIR DISPOSITION. CLEANED, TREATED, PRIMED AREAS ACCEPTABLE AREAS AS-IS.SDR FDEA202412061777Spar Cap · corrodedRH WING REAR SPAR UPPER CAP - CORROSION AT STA XORS 783 (AREA MARKED) REPAIRED RIGHT WING REAR SPAR UPPER CAP AT STA XORS 783 REF EA# 1-5710-T0376494 TITLED: WINGS - BASIC WING STRUCTURE - RH WING REAR SPAR UPPER CAP AFT LEG - REWORK. MAJOR REPAIR.SDR DALA2024112711257Spar · cracked-AD- WORKING PRI 615810-14AD REV 0. LH WING SPAR CRACK FUEL LEAK. ACCOMPLISHED PRI 615810-14AD REVISION D, REV 3. VERIFIED ERA 615810-14AD REV D SECTION VI TIME LIMITED REPAIR III MATCHES COMPLETED PRI 615810-14AD REV 0, 1, 2, AND 3. ASSOCIATED ER/A 14-615810 SDR 2024FA0000859Spar · corrodedLH MLG WHEEL WELL AFT SPAR, FWD FACE HAS 1 AREA OF CORROSION INBD OF WS 37.00. MECHANICALLY REMOVED CORROSION LOCATED IN LH MLG WHEEL WELL, AFT SPAR, FWD FACE INBD OF WS 37.00 APX 21 INCHES IAW C680 SRM 51-70-02. FOUND CORROSION BLEND TO BE BEYOND LIMITS IAW CSDR DALA2024111911037Spar · crackedTRANSFERRED FROM PAPER NON-ROUTINE CRACK FOUND AND VERIFIED BY HFEC ON RH WING AFT SPAR IB OF FLAP TRACK #4. C/A: SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 007-0001:5957917/001 00001 REPAIRED RH WING AFT SPAR PER PRISDR JR2R20241114888Spar · crackedLH WING O/B SPAR WHERE WINGLET ATTACHES IS CRACKED. REPLACED.SDR DALA2024111811011Spar Cap · corroded(LOG 0658652) DURING HCK AT QRO, WHILE PERFORMING THE FINAL INSPECTION CONDUCTED BY WC 5700-2101, EXFOLIATION WAS FOUND AFFECTING THE LH WING FRONT SPAR ATTACH LOWER STRAP, LOCATED BETWEEN OSS 60.69 & 75.0. DAMAGE REPAIRED PER ERA 601633-14.SDR 2024FA0000831Spar · corrodedREPAIRED 5 CORRODED AREAS ON THE FWD AFT SPAR FACE INBOARD OF WS 37.00, 1 AREA INSIDE BAY 720DR UPPER SPAR CLIP, INBOARD CORNER AND 2 ADDITIONAL AREAS ON WING AFT SPAR LOWER SPAR CLIP INSIDE RH GEARWELL, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAISDR CALA2024111302846Spar · corrodedUNDER PANEL 521LB FRAME IS CORRODED (REF AAR NR 1000020593) PERFORMED REPAIR ON LH WING UNDER PANEL 521LB, IAW B737-800, ECR A 5720-0379, EO-240615, P1 AND P2, SRM 57-20-01-2R-3. THIS REPAI R REQUIRE INSPECT AS GIVEN IN ECRA 5720-03479, PART 1 STEP 2:AFT ER APSDR VNAA20241213004Spar · corrodedDISCREPANCY: REPAIR TO WING INBD AUX/SPAR BETWEEN WS 24.5 - WS 34, RHS, REPLACE OR REPAIR THE DISCREPANT ITEM
SDR DALA2024111911030Spar · crackedSHIP 3235 DISC: DTE REQUIRED. ER/A 618844-14 ISSUED FOR CRACK ON THE MIDDLE REAR SPAR LOWER FLANGE BETWEEN RIB 19 AND 20 ON THE RH WING. FOLLOW ON DTE IS REQUIRED. C/A: DTE REQUIRED. SECTION I REPAIR IS LIMITED TO 6 MONTHS. ADDITIONAL ENGINEERING AUTHORIZATIONSDR DALA2024112111101Spar · cracked-AD- LH WING REAR SPAR XRS 164 CRACKED. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) REQUIRED FOR CONTINUED SERVICE BEYOND 06NOV2024 (AD EFFECTIVE DATE). A NEW FAA FORM 8100-9 AND AMOC APPROVAL TO AD 2024-21-01 IS REQUIRED FOR CONTINUED SERVICE BEYOND SDR 2024F00255Spar Splice · crackedCRACK INDICATIONS, CENTER WING, CENTER SPAR SPLICE W.S 37 REF FIELD REPAIR FR680-0126-13812 REV-SDR SWIA20241203009Spar · corrodedSTRUCTURAL CORROSION ON MATING SURFACES INSIDE AUXILIARY SPAR SECTION BEHIND PANEL 642AZ. (C-CHECK RO 11/30/2024) REMOVED CORRODED AND INSTALLED NEW RETAINING ANGLE PN CC670-10338-2 FOR PANEL 642AZ AT R/H WING AUX SPAR PER CRJ700 SRM TASK 51-42-21-001-0SDR DALA2024100709763Bushing · corrodedSHIP 3143 CORROSION FIXED BUSHING I/B SIDE CENTER HINGE REAR SPAR ON SPOILER 3 RH WING REFER TO AMDS CARD 5770-1010-RT-DE FOR RII. CORRECTIVE ACTION: REPLACED FIXED BUSHING (1 EA) ON ATTACH FITTING I/B SIDE REAR SPAR OF SPOILER 3 RH WING. AS PER A319 SRM 51-72SDR 2024FA0000746Spar Cap · corrodedDEFECT WAS DISCOVERED WHILE CONDUCTING A 100HR/ANNUAL INSP. R/H WING INBOARD LOWER AFT SPAR CAP HAS INTERGRANULAR/ EXFOLIATION CORROSION. DEFECT IS APPROXIMATELY LOCATED AT RWS 30.0" AND MEASURES APPROX. 3.00" LONG, WHERE EXFOLIATION HAS OCCURRED. AIRCRAFT SDR DALA2024100209620Spar Cap · crackedCRACK IN LH WING REAR SPAR LOWER CAP RADIUS. REFERENCE AA NUMBER FC 5720-01103. CRACK LOCATION IS XRS 156.950. SUMMARY NRC 010-0001:5720-01103-01A/001 00001 COMPLIED WITH PRI 621210-14 REV 0 AND REV 1 AND ENSURED IT MATCHES ERA 621210-14 REV ORIG SECTION 1 STESDR SWAA2024100439180Spar · corrodedLT. WING LOWER FRONT SPAR CHORD AT OFSS 298 CORRODED.<[01] 'THE DAMAGE WAS REPAIRED PER EA 24-157-02568. CONTINUED AIRWORTHINESS REQUIREMENTS ARE TRACKING ON EA 24-157-02568-DTI.';[02] VERIFIED CORRECTIVE ACTION 1SDR SWI2024F01230Spar · damagedINSIDE FUEL PANEL 541BB, REAR WING SPAR HAS TOOLING DAMAGE AROUND NUMEROUS FASTENERS WHERE SEALANT HAS BEEN REMOVED (MARKED) (C-CHECK RO 11/11/2024) REPAIRED REAR WING SPAR AT WS27.96 ON LEFT WING REF REO 690-57-21-490 REV -- DATED 2024-09-27. COMPLIEDSDR FDEA202409111279Spar Cap · corrodedLEFT HAND WING TRAILING EDGE LOWER SPAR CAP FOUND WITH CORROSION AT STATION XORS 1070. LEFT HAND WING TRAILING EDGE LOWER SPAR CAP CORROSION AT STATION XORS 1070 REMOVED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-00-10-1A ALLOWABLE DAMAGE 1. CORRODED LOWSDR NACA2024090500002Spar · corrodedFOUND OUT LH WING IB FWD FLAP REAR SPAR LOWER CHORD CORROSION AT 34 INCHES TO OB EDGE. FLAP CHORD REPLACED TO REMOVE CORROSIONSDR 2024F00201Spar Cap · corrodedCORROSION WAS FOUND ON THE 6922435-4 REAR SPAR CAP, LOWER FORWARD ANGLE-RH, NEAR RWS 41. ACCOMPLISHED FIELD REPAIR: FR-680-0116-1466 REV -, FIELD REPAIR-CORROSION, RH WING LOWER AFT SPAR CAP, RWS 39.4-43.2.THE DAMAGE WAS BLENDED OUT AND THE REMAINING THICKNESSSDR SWIA20241115823Spar · gougedRH WING AFT SPAR AILERON HINGE FITTING #4 GOUGE ON LOWER OUTBOARD SIDE (C-CHECK RO 10/26/2024) (FILED CLOSED)COMPLIED WITH ALL STEPS OF MHIRJ REO 601R-57-51-1056 REV -- DATED 2024-09-09 IN THE REPAIR OF THE RH WING AFT SPAR AILERON HINGE FITTING #4 ON THE LOWESDR SWIA202411150023Spar · gougedLH WING AFT SPAR AILERON HINGE FITTING #3 GOUGE BETWEEN LUGS AND ON LOWER OUTBOARD SIDE (C-CHECK RO 10/26/2024) (FILED CLOSED)REPAIRED LH WING AFT SPAR AILERON HINGE FITTING #3 IAW REO 601R-57-51-1055 REV --, DATED 2024-09-07, SEE CONTINUATION CARD FOR FURTHERSDR SWAA2024100228391Frame · crackedLH WING FWD WTB FAIRING STRAKELET MIDDLE SECTION FRAME COMMON TO UPPER HAS A CRACK. (MARKED)<[01] LH WING FWD WTB FAIRING STRAKELET MIDDLE SECTION FRAME FOUND OUT OF LIMITS; IAW SRM 57-41-01-1A-1 ALLOWABLE DAMAGE 1; AND WAS REMOVED AND REPLACED IAW SRM 51-40-0SDR SWAA2024100228400Frame · crackedRH WING FWD WTB FAIRING STRAKELET MIDDLE SECTION FRAME COMMON TO UPPER HAS A CRACK. (MARKED)<[01] VERIFIED;[02] RH WING FWD WTB FAIRING STRAKELET MIDDLE SECTION FRAME FOUND OUT OF LIMITS; IAW SRM 57-41-01-1A-1 ALLOWABLE DAMAGE 1; AND WAS REMOVED AND REPLACED ISDR SWAA2024092325856Spar Web · corrodedCORROSION ON LH WING REAR SPAR WEB AT UPPER END OF CUTOUT FOR #1 FUEL TANK AFT BOOST PUMP<[01] VERIFIED APPLICABILITY OF SRM 57-20-10-1A-3 PER STC ST00830SE;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.;[03] REMOVED CORROSION ON LH WING REAR SPAR WEB AT UPPER END OSDR DALA2024081107983Spar Splice · unknownSHIP 3235 DISC: RI 619729-14 FOR RH REAR SPAR SPLICE REPAIR PART FABRICATION. C/A: ACCOMPLISH PRI 619729-14 REV 3 STEP 12 PRIMER APPLICATION OF RH REAR SPAR SPLICE REPAIR PARTS ASSOCIATED ER/A 14-619729 ADDED FOR AC 3235. COMPLIED WITH PRIMER APPLICATION OF RHSDR DALA2024081107982Spar Splice · unknownSHIP 3235 DISC: PRI 619729-14 FOR RH REAR SPAR SPLICE REPAIR PART FABRICATION. C/A: ACCOMPLISH PRI 619729-14 REV 3 STEP 11 ANODIZATION OF RH REAR SPAR SPLICE REPAIR PART(S). COMPLIED WITH STEP 11 CHROMIC ACID ANODIZATION FOR RH REAR SPAR SPLICE REPAIR PART(S) SDR DALA2024081107981Spar Splice · unknownSHIP 3235 DISC: PRI 619729-14 FOR RH REAR SPAR SPLICE REPAIR PART FABRICATION. C/A: ACCOMPLISH PRI 619729-14 REV 3 STEP 10 PRIMING OF RH REAR SPAR SPLICE REPAIR PART. COMPLIED WITH PRIMING OF RH REAR SPAR SPLICE REPAIR PART IAW PRI 619729-14 REV. 4 STEP 10. PRSDR DALA2024081107980Spar Splice · unknownSHIP 3235 DISC: PRI 619729-14 FOR RH REAR SPAR SPLICE REPAIR PART FABRICATION. C/A: ACCOMPLISH PRI 619729-14 REV 3 STEP 9 ANODIZATION OF RH REAR SPAR SPLICE REPAIR PART. ASSOCIATED ER/A 14-619729 ADDED FOR AC 3235. COMPLIED WITH CHROMIC ACID ANODIZATION OF RH SDR ASAA2024072652145Spar · corrodedL/H WING I/B FLAP, AFT SPAR HAS CORROSION ON LOWER LEG INNER SURFACE. GROUNDED - YES. EVALUATED CORROSION, FOUND TO BE 100% MATERIAL LOSS. TRIMMED OUT CORRODED AREA 19.05MM X 298.45MM IAW A320 SRM 51-74-00/001 REV 149-01MAY2024. L/H WING I/B FLAP REMOVED AND RSDR 2024FA0000511Spar · corrodedMECHANICALLY REMOVED 2 EA AREAS OF CORROSION ON LH WING AFT SPAR, LOWER CLIP INBD SIDE OF WS 37.00 IAW C680 SRM 51-70-02. EVALUATED AND FOUND BLENDED AREAS TO BE OUT OF LIMITS IAW CESSNA 680 SRM 51-70-02. COMPLIED WITH TEXTRON FIELD REPAIR FR-680-0089-13574, RSDR IPXA2024081466845Spar · crackedR/H WING STA : OLES 1581 FRONT SPAR SURFACE ONE HI-LOCK COLLAR CRACK (AGING A/C INSPECTION). (REPLACE) REVIEWEDSDR DALA2024071807239Skin · corrodedSHIP 3140 CORROSION EXTERNAL SKIN TRAILING EDGE AREA BETWEEN RIB20 AND RIB 21 ON RH WING. CORRECTIVE ACTION: PERFORMED REPAIR AREA LOC.ON TRAILING EDGE AREA ON LOWER SURFACE OF UPPER SKIN AT LEVEL RIB 20 AND RIB 21 ON RH WING AS PER A319 SRM 51-74-00. (0452484SDR SWIA20240920028Spar · gougedRH WING AFT FACE OF REAR WING SPAR HAS GOUGES AROUND 2ND LIGHTNING HOLE BETWEEN WS350.25 AND WS370.25 (C-CHECK RO 9/19/2024) COMPLIED WITH REPAIR TO RH WING AFT FACE OF REAR WING SPAR BETWEEN WS350.25 AND WS370.25 REF REO 670-57-21-987 REV-- DATE 2024-0SDR FDEA202407060949Plate · corrodedLEFT WING LEADING EDGE LOWER SPAR CAP STRAP PLATE FOUND WITH CORROSION AT STATION XOS 473. LEFT HAND WING LEADING EDGE LOWER SPAR CAP STRAP PLATE CORROSION AT STATION XOS 473 REPAIRED AS PER E.A.#: 1-5720-T0379764. TITLE: WING SECONDARY WING STRCT RESDR 2024FA0000503Spar Cap · crackedSTRUCTURAL CRACKS WERE DISCOVERED DURING GENERAL VISUAL INSPECTION ("GVI") AND CONFIRMED WITH NON-DESTRUCTIVE TESTING ("NDT") EDDY CURRENT METHOD, AFTER REMOVING THE LEFT HAND LOWER SPAR CAP. SUBSEQUENT DAMAGE WAS LOCATED BEYOND THE SPAR CAP IN VARIOUS ADJACENSDR SWAA2024071006278Spar · corrodedFOUND CORROSSION ON RIGHT WING; FORWARD SPAR; LOWER CHORD AT WS 290. REF. TTG8Q00U749A.<[01] FAULT RESOLVED ON EA 24-157-01775-WIP1 AND WIP2;[02] AUDIT C/W
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