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 LR7A07153Spar Cap · crackedDURING SCHEDULED C-3 CHECK, PER SB382-57-85 R2 FOUND RT LOWER FWD SPAR CAP EYEBOLT HOLE CRACKED AT FS 517, CWS176R, WL257. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-076.SDR SWIA200718987Spar · damagedFORWARD OUTBOARD WING SPAR ON RIGHT WING HAS DAMAGE AT WS 339. REPAIRED WING SPAR DAMAGE AT WS 335-353 IAW CRJ 200 REO 601R-57-21-898.
SDR EPUA120107Spar · crackedDURING ROUTINE SCHEDULED MAINTENANCE, A CRACK WAS DISCOVERED APPROX 6.5" LONG IN A U-SHAPED PATTERN ON THE LT WING MAIN SPAR AT LT CWS 51.00 TO CWS 48.00, EMANATING FROM THE UPLOCK BRACKET ATTACHMENT POINT TO THE MAIN SPAR. THE UPLOCK BRACKETS WERE ALSO BROKESDR DU4R2007188Spar · crackedREPAIRED VERTICAL CRACK FROM HOLE C-DOWN TO EDGE OF CUT OUT OF LT REAR SPAR UPPER CHORD BY OVERSIZING HOLE, FABRICATING AND INSTALLING BUSHING IAW REO-L0152 REV IR DATED 11-21-07 FAA FORM 8100-9. THIS IS A TIME LIMITED REPAIR, REPEAT INSPECTION REQUIRED AT 45SDR 1218367020708Spar · corrodedRIGHT FRONT SPAR AT RIB 12 INBOARD, AND LEFT FRONT SPAR AT RIB 10, BOLTS FOUND CORRODED. REMOVED AND REPLACED BOLTS AT RIB 10 AND 12.SDR USAA920071166Stiffener · crackedMAJOR REPAIR - CRACKED CENTER WING REAR SPAR VERTICAL STIFFENER, BS 663.75, RBL 6.15, WL 170, IN RT MLG WHEEL. REPAIRED IAW USAIRWAYS EA 120397.SDR 07FDEA04795Frame · crackedFRAME 47 FASTENER HOLE INSPECTION, NR 4 RT HOLE HAS INDICATION OF DEFECT. REAMED HOLE TO TRANSITION FITTING IAW FED EX A310-200 SRM 51-40-40 PG14. INSTALLED FASTENER IAW A310-200 SRM 51-40-21 PG 24. BHEC NR 4 HOLE REF EA 6-5710-112994. NO CRACK INDICATION NSDR AMWA1001010ASpar · damagedAT RT WING WS 54.75 FOUND 0.50 INCH HOLE THROUGH SUB SPAR. HOLE HAD EVIDENCE OF POSSIBLE ELECTRICAL ARCING AT WIRING GROUNDING ATTACHMENT. REPAIRED IAW APPROVED DATA AND CLEARED DISCREPANCY.SDR AMWA1019019Spar · crackedDURING DETAIL INSPECTION, RT AFT SPAR FLANGE AT WS117.5 WAS FOUND TO BE CRACKED FROM RIVET TO EDGE OF FLANGE. MAINTENANCE OBTAINED APPROVED DATA, PERFORMED REPAIR AND CLEARED DISCREPANCY.SDR 07FDEA04709Spar Cap · corrodedRIGHT WING REAR SPAR UPPER CAP FOUND WITH CORROSION AT XORS 1044 AND XORS 1046. REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-116512, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR DU4R2007182Spar · cutRT WING REAR SPAR UPPER CHORD CUT APPROX 4 FROM SPAR END FITTING AT WSTA 790. REPAIRED BY CUTTING OUT SECTION OF CHORD, FABRICATED AND INSTALLED CHORD AND SPLICE ANGLES IAW BOEING DWG 112N1006 AND DELTA/TIMCO MRR NR CPZ-LCQ-07-291-67-60001-IR.SDR TRAX200701630Spar · corrodedLEFT WING FROM SPAR UPPER ANGLE TOP SURFACE CORRODED AT RIB 13. CORROSION REMOVED IAW SRM 51-21-42 REPAIR DETERMINED NOT TO BE A MAJOR REPAIR MATERIAL THICKNESS: 0.200 MATERIAL REMOVED: 0.003. WITHIN LIMITS AS PER SRM: 51-10-10.SDR 07FDEA04700Spar Cap · damagedLEFT WING, REAR SPAR UPPER CAP 1EA FASTENER HOLE ELONGATED AT XORS 669. REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-116510, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR CA071026002Spar Cap · cracked(CAN) WHILE PERFORMING AD 92-26R1 IAW SB 215-A454 REV 3, NO DEFECTS WERE FOUND IAW OUTLINED ULTRASONIC INSPECTION PROCEDURES. THE NDI TECH NOTED THAT HE WAS PICKING UP WHAT HE THOUGHT WAS A SUSPECTED CRACK OUTSIDE THE AREA OUTLINED IN THE SB AND PROCEEDED TO ESDR TRAX200701561Frame · crackedRIGHT WING BOX FR 28 CRACKED. REPLACED IAW SRM 51-25-01 REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-25-01.SDR TRAX200701557Frame · crackedLEFT WING BOX FRAME 28A FACE PLATE FOUND CRACKED. REPLACED IAW SRM 51-25-01REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-25-01.SDR TRAX200701556Frame · crackedLEFT WING BOX FRAME 28 CRACKED. REPLACED IAW SRM 51-25-01. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A.SDR COEA0733821Spar · corrodedFOUND DURING HEAVY CHECK. MAJOR REPAIR. CORROSION ON RT WING FWD SPAR ON THE LOWER FWD SPAR FLANGE OB OF WING RIB 10 AND IB OF WING RIB 12. CORROSION REMOVED AND DAMAGES BLENDED IAW REPAIR DO/TS PROCEDURES. SHEET REFERENCE: DO/TS-803/04, 2752 AND JUSTIFICATSDR USAA920071090Spar · corrodedMIA - MAJOR REPAIR - C-2 CHECK - CORROSION ON RIGHT WING LOWER SURFACE FRONT SPAR LOWER CHORD, WS 226.3. REPAIRED RIGHT WING LOWER SURFACE FRONT SPAR LOWER CHORD, WS 226.3 IAW USAIRWAYS EA 136479.SDR KCSA071459Stiffener · corrodedLEFT WING FRONT SPAR VERTICAL STIFFENER HAS CORROSION AT FS 1280.SDR 07FDEA04505Spar · crackedFOUND CRACKS IN SEVERAL HOLES ON CENTER SPAR WEB C 44 REPAIR PERFORMED BY OVERSIZING THE HOLES UNTIL CRACK REMOVAL, BUSH AND NEW FASTENER INSTALLTION IAW EA 6-5710-106488 AND RAS 052365/022/2007 ISS A.SDR AMWA0828013Spar Cap · corrodedBIO CORROSION LT MAIN SPAR, LWR CAP FROM APPROX WS119.5 TO WS122. REPAIRED IAW REPORT NR 6872 REV IR.SDR ECPR466DSpar · corrodedAT APPROX LT WING STA 56.0, THE UPPER OTBD QUADRANT OF AN ELECTRICAL WIRE PASS THROUGH HOLE IN THE WING SPAR WEB WAS FOUND TO HAVE EXFOLIATION CORROSION. THE PASS THROUGH HOLE, WHICH IS IN THE LANDING GEAR WHEEL WELL AREA, HAD A CATERPILLAR GROMMET INSTALLED TSDR 07FDEA04398Spar · damagedSHOULDERED BOLTS FOUND DURING EMBODIMENT OF SB A310-57-2079 AT HOLE NR 21 AND NR 14 RT REAR SPAR AREA OF SPOILER NR 3 RT REPAIR PERFORMED BY REPLACEMENT OF BUSH IAW EA 6-5720-82852 AND RAS /BAE/1000689/2005 ISS A.SDR UIEA200700449Spar Cap · corrodedRIGHT WING FRONT SPAR LOWER CHORD AREA BETWEEN FSSO 1322 AND 1340 CORRODED. CORROSION REMOVED AS PER SRM 51-10-01 AND BOEING MESSAGE 1-638497220-2.SDR UIEA200700415Spar · corrodedRIGHT WING STATION 1337 FRONT SPAR TO REAR SPAR HAS CORROSION EVIDENT. REMOVED CORROSION IAW SRM 51-10-01.SDR UIEA200700411Spar · corrodedRIGHT WING AT WS 917- WS 1141 FRONT SPAR TO REAR SPAR HAS CORROSION EVIDENT. CORROSION REMOVED PER SRM 51-10-01.SDR UIEA200700401Spar · corrodedLEFT WING UPPER SURFACE MID SPAR WS 1112, WS 1280, WS 1330 AND WS 1392 HAS MINOR SURFACE CORROSION EVIDENT. CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.
SDR UIEA200700381Spar · corrodedLHW UPPER SURFACE WS 353 TO WS 586 SPAR SURF CORROSION EVIDENT. CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.
SDR COEA0705919Spar Cap · corrodedFOUND DURING HEAVY CHECK, MAJOR REPAIR, LEVEL 2 CORROSION, CORROSION ON LT WING AFT SPAR UPPER CAP. REMOVED CORROSION AND DAMAGE BLENDED PER SRAS, DO/TS-4213/07. (M)SDR UPS07850989Spar · corrodedINSPECTION TYPE:C1 RIGHT WING FLAP STA 98 ACTUATOR FWD FITTING ON AFT SPAR HAS DEEP PITTING CORROSION ON BOTH LUGS. REMOVED AND REPLACED RIGHT WING FLAP STA 98 FWD FITTING ON AFT SPAR IAW SRM 51-12-2 AND AMM 20-14-00-2.SDR CA071212002Spar · cracked(CAN) DURING ANNUAL INSPECTION, VISUAL INSPECTION OF AREA REVEALED A SUSPECTED CRACK. NOT OF DYE PENETRANT AND EDDY CURRENT CONFIRMED. MFG SERVICE KIT TO INSTALLED. PART LAST NDT INSPECTED 22.1 HRS PREVIOUS AND NO INDICATIONS. (TC NR 20071212002)SDR 07FDEA03692Spar · crackedRIGHT WING NR 6 LEADING EDGE ACTUATOR MOUNT ON FRONT SPAR IS CRACKED IN THE UPPER INBD CORNER (FLAP). REMOVED AND REPLACED NR 6 LEADING EDGE ACTUATOR MOUNT UPPER I/B CORNER (KRUGER FLAP) REF MM 27-81-022, SRM 51-30-2 LEAK CHECK AND OPS CHECKED GOOD.SDR UIEA200700376Spar · corrodedWS 317 - WS 1141, FRONT SPAR TO REAR SPAR CORROSION EVIDENCED. SURFACE CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.SDR KCSA071354Spar Cap · corrodedRIGHT WING FRONT SPAR BOTTOM CAP AT HOLES 1480 HAS CORROSION IN L/E CAVITY.SDR MWEA070206Spar · corrodedLOWER WING AND REAR SPAR HAS CORROSION, CRACK NOTED ABOUT XCW 18-21 OUTBOARD OF CENTER BELLY AREA LEFT SIDE. REMOVED CORROSION AND FABRICATED AND INSTALLED FASTENER.SDR 2007FA0000770Spar · brokenRT WING MAIN SPAR FOUND FRACTURED IB OF STRUT ATTACH. CURRENT AD INADEQUATE TO PREVENT FURTHER FAILURES. THIS AIRCRAFT HAS LESS THAN 14 HR SINCE LAST ANNUAL INSPECTION..SDR 2007FA0000769Spar · fracturedRT WING MAIN SPAR FOUND FRACTURED IB OF STRUT ATTACH. CURRENT AD INADEQUATE TO PREVENT FURTHER FAILURES. THIS AIRCRAFT HAS LESS THAN 14 HR SINCE LAST ANNUAL INSPECTION..SDR 07FDEA03385Spar · corrodedDURING ACCOMPLISHMENT OF EO 6-5710-7-3301 A2 PART 1 FOUND CORRODED HOLE 'D (SEE SB A300-57-6063). REPAIR PERFORMED BY REAM UP AND OVERSIZING HOLE IAW EA 6-5710-95892 AND RAS/BAE/1002151/2006 ISSUE A.SDR COEA0727821Spar Cap · corrodedFOUND DURING HEAVY CHECK. MAJOR REPAIR, LEVEL 2 CORROSION. CORROSION ON RT WING AFT SPAR UPPER CAP SLAT STRIP BETWEEEN RIBS 4 AND 7. REMOVED CORROSION AND DAMAGE BLENDED IAW DO/TS-4073/07-9281 REPAIR INSTRUCTIONS. WO NR 72241/ NR602018. (K)SDR TAMF20070024SSpar · damagedDURING C CHECK INSPECTION (TASK CARD 57-650-00) WAS FOUND LOOSE MATERIAL ON SPLICE PLATE AT FRONT SPAR STA ISS 864.92 873.13 RT. DAMAGED AREA WAS REPAIRED IAW EWO 767-57-028 AND SERVICE REQUEST 1-527347746. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 81SDR TRAX200701296Spar · crackedSDI - CRACK DET-4 LOWER SPAR FASTENERS BETWEEN RIB 13 & 14. COMPLIED WITH UNDER EXELTECH W/O YUL000780 NON-ROUTINE 312. REFER TO THIS NON-ROUTINE FOR MTC ACTION. SUPPLEMENTAL - SDR CLOSED 09/13/07.SDR TRAX200701293Spar · crackedSDI - CRACK DETECT - REAR SPAR LOWER SURFACE FLANGE AT RIB 8. COMPLIED WITH UNDER EXELTECH W/O YUL000780 NON-ROUTINE 214. REFER TO THIS NON-ROUTINE FOR MTC ACTION. SUPPLEMENTAL - SDR CLOSED 09/13/07.SDR TRAX200701288Spar · crackedSDI - CRACK DET - REAR SPAR LOWER SURFACE FLANGE BETWEEN RIB 12 & RIB 13. COMPLIED WITH UNDER EXELTECH W/O YUL000780 NON-ROUTINE 284. REFER TO THIS NONROUTINE FOR MTC ACTION. SUPPLEMENTAL - SDR CLOSED 09/13/07.SDR TRAX200701292Spar · crackedCRACK DETECT - FRONT SPAR LOWER SURFACE FLANGE AT RIB 4. COMPLIED WITH UNDER EXELTECH W/O YUL000780 NONROUTINE 278. REFER TO THIS NONROUTINE FOR MTC ACTION. SUPPLEMENTAL - SDR CLOSED 09/12/07.SDR TRAX200701291Spar · crackedCRACK DETECT - REAR SPAR LOWER SURFACE FLANGE AT RIB 4. COMPLIED WITH UNDER EXELTECH W/O YUL000780 NONROUTINE 280. REFER TO THIS NONROUTINE FOR MTC ACTION. SUPPLEMENTAL - SDR CLOSED 09/12/07.SDR TRAX200701290Spar · crackedCRACK DET - FRONT SPAR LOWER SURFACE FLANGE AT RIB 2. COMPLIED WITH UNDER EXELTECH W/O YUL000780 NONROUTINE 285. REFER TO THIS NONROUTINE FOR MTC ACTION. SUPPLEMENTAL - SDR CLOSED 09/12/07.SDR TRAX200701289Spar · crackedCRACK DET - REAR SPAR LWR SURFACE FLANGE AT WING TO FUSE JUNCTION AT RIB 2. COMPLIED WITH UNDER EXELTECH W/O YUL000780 NONROUTINE 286. REFER TO THIS NONROUTINE FOR MTC ACTION. SUPPLEMENTAL - SDR CLOSED 09/12/07.SDR TRAX200701295Spar · crackedSDI - CRACK DETECT, FRONT SPAR LOWER SURFACE FLANGE AT RIB 10.SDR TRAX200701294Spar · crackedSDI - CRACK DETECT, FRONT SPAR LOWER SURFACE FLANGE AT RIB 12.
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