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 TAMF20070025SSpar · damagedDURING C CHECK INSPECTION (TASK CARD 06-102-01-1) WAS FOUND A LOOSE MATERIAL ON SPLICE PLATE AT FRONT SPAR STA ISS 1009 - 1017 LT. DAMAGED AREA WAS REPAIRED IAW EWO 767-57-027 AND SERVICE REQUEST 1-526643882. THIS REPAIR IS CONSIDERED A MAJOR REPAIR. FORM 810SDR 07FDEA03155Spar Cap · corrodedLEFT WING, TRAILING EDGE REAR SPAR UPPER CAP AT STATION XORS 1042 FOUND CORRODED. COMPLIED WITH FEDEX E.A. 1-5710-115175, CLASSIFIED AS A MINOR REPAIR AS PER FEDEX GMM 6-2-100.SDR CA070912005Spar · corroded(CAN) DURING A MAINTENANCE FUNCTION SEVERE CORROSION WAS DISCOVERED ON THE BOTTOM OF THE WING SPAR ENTRE SECTION. THIS SECTION OF THE SPAR HAS HIGH DENSITY FOAM GLUED TO THE SPAR WHICH PREVENTS ADEQUATE INSPECTION. THE CORROSION WAS SUCH THAT THE WING SPAR CENSDR N14834CASpar · corrodedCORROSION ON RIGHT WING REAR SPAR LOWER HORIZONTAL FLANGE BETWEEN THE WING RIBS 16 AND 19.SDR AMWA25032Spar · damagedRT MAIN SPAR FASTENERS NEAR BL 114.250 AND WS 124.588 HAD (2) OVERSIZED FASTENERS. REPAIRED IAW REPAIR DRAWING 1900UE 159-1 REV 1R, DATED AUGUST 14, 2007.SDR 07FDEA03007Spar · crackedA 1.5 INCH CRACK EXIST AT LT WING REAR SPAR BETWEEN RIBS 8/9 ACCESS PROVISIONS THROUGH PNL 575FB REF 57-00-00-6 ZONE 500. INSTALLED S/B NR A300-57-6064 DOUBLERS AT RIB NR 9 AFT OF REAR SPAR (REINFORCEMENT DOUBLERS) COMPLIED WITH EA 6-5730-110509.SDR IXXA07SMN222SSpar · crackedDURING ROUTINE C CHECK INSPECTION, NR 2 MAIN TANK WEB OF CENTRAL SPAR (LWR SIDE) CRACKED 2 1/2" AT STA XRS 172.000 BETWEEN S-61 AND S-62.SDR IXXA07SMN221SSpar Cap · crackedDURING ROUTINE C CHECK INSPECTION, NR 2 MAIN TANK LOWER CAP OF CENTER SPAR 3" CRACKED AT STA ZRS 172.000 BETWEEN S-61 AND S-62.SDR IXXA07SMN220SSpar · crackedDURING ROUTINE C CHECK INSPECTION, NR 1 MAIN TANK CTR SPAR WEB LWR SIDE, CRACK 4" AT STA XRS 255.000 BETWEEN S-61 AND S-62.SDR IXXA07SMN219SSpar · crackedDURING ROUTINE C CHECK INSPECTION, NR 1 MAIN TANK, CTR SPAR LWR CAP, CRACKED 3" AT STA XRS 255.000 BETWEEN S-61 AND S-62.SDR 07FDEA02946Spar · crackedCRACKS FOUND ON CENTER SPAR WEB AND DOUBLER C44 (AROUND HOLE 1 (LT) ,5 (LT) , 8 (RT)) REPAIR PERFORMED BY REAM UP UNTIL CRACK REMOVAL AND DOUBLER CUT-OUT IAW SB A300-53-242, APPROVED BY EA 6-5710-112510 AND RAS 053726/005/2007 ISS A.SDR 07FDEA02893Spar · crackedCRACKED HOLES AT CENTER SPAR DOUBLER RUN OUT AT C44 LT, RELATED P/N WEB A571-10431-200, HOLE C, D IAW SB 53-242. REPAIR PERFORMED BY REAM UP UNTIL CRACK REMOVAL IAW EA 6-5710-112482 AND RAS/053466/009/2007 ISS A.SDR 07FDEA02892Spar · crackedCRACKED HOLES AT CENTER SPAR DOUBLER RUN OUT AT C44 LT (RELATED P/N TEE A571-10122-200, HOLE C, D IAW SB 53-242). REPAIR PERFORMED BY REAM UP UNTIL CRACK REMOVAL IAW EA 6-5710-112482 AND RAS/053466/009/2007 ISS A.SDR QXEA200701312Spar · corrodedC5 PDX - LEFT WING FRONT SPAR LOWER CAP HAS FRETTING CORROSION AT YW 134.00 - YW 137. REPAIRED IAW RD8-57-1150 AND SRM 51-20-36.SDR TRAX200701140Frame · crackedRIGHT WING BOX FRAME 28A FRAME AND FACING CRACKED. [08-16-07] WING BOX FR28A FRAME REPAIRED AS PER ANA/YUL07/192/375-004 AND FACING REPLACED AS PER SRM 51-25-01 REPAIR DETERMINED NOT TO BE A MAJOR REPAI IAW SP663 AND FAR 43 QAPENDEX A REPAIR ACCOMPLISHED IASDR KCSA071284Spar · corrodedCOMPOSITE FILLER BULGING NEAR AFT SPAR RT WING UPPER SURFACE WS 597.SDR TAMF20070009SSpar · corrodedRT WING FRONT SPAR UPPER FWD CHORD AT STA OSS 456.98 HAS CORROSION. REMOVED CORROSION FROM UPPER FWD CHORD AT RT WING FRONT SPAR, STA OSS 456.98 IAW SRM 51-10-02 PAGE 12-13. THICKNESS FOUND, MAX: 0.078 INCH, MIN: 0.055 INCH. NO CRACKS FOUND. BLENDING LIMITS OSDR DL757070975Spar · damagedDURING REMOVAL OF A RT WING LOWER PANEL, A FASTENER HOLE WAS MISDRILLED AND OVERSIZED THROUGH THE PANEL EXTERIOR SKIN AND THE FRONT SPAR LOWER CHORD. PERMANENT REPAIR WAS ACCOMPLISHED BY ACTS IN VANCOUVER.SDR 2007FA0000859Spar · crackedAC WAS BEING MODIFIED TO INCLUDE THE INSTALLATION OF WING SPAR INSPECTION HOLE KIT IAW STC NR SA005278E. A PORTION OF THE WING LEADING EDGE SKIN WAS REMOVED AND THE WING SPAR WAS VISUALLY INSPECTED AS SPECIFIED IN THE INSTALLATION INSTRUCTIONS SUPPLIED WITH TSDR GUUA07260704Spar Cap · crackedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LT WING REAR SPAR LOWER CAP CRACKED FROM RIVET HOLE TO REAR EDGE AT LWS 117.50. REMOVED DAMAGED SECTION OF LT LOWER AFT SPAR FROM LWS 73 TO LWS 129.86 SPLICED IN NEW SECTION OF SPAR IAW FIELD REPAIR FR-CO-01583 SDR 2007FA0000714Spar · crackedAIRCRAFT WAS BEING MODIFIED TO INCLUDE THE INSTALLATION OF WING SPAR INSP HOLE KITS AS SUPPLIED IAW STC NR SA00527SE. A PORTION OF THE WING LEADING EDGE SKIN WAS REMOVED AND THE WING SPAR WAS VISUALLY INSPECTED AS SPECIFIED IN THE INSTALLATION INSTRUCTIONS SUSDR AMWA06002Spar Cap · corrodedBIO CORROSION LT SPAR, ALT SPAR FLANGE ATTACHMENT OF THE RIB TO THE MAIN SPAR. REPAIRED IAW ENGINEERING REPORT 6799-3 REV 1R.SDR AWXA200700900Spar · corrodedSAL - MAJOR REPAIR - BC-6 CHECK - NR 5964268, 5964269, 5964270, AND 5964344, CORROSION FOUND ON LT WING REAR INNER SPAR, RIB 2 - RIB 5, AREA ON HOLE 52, 53 AND 54 OF MAIN LANDING GEAR ANCHORAGE FITTING. CORROSION REMOVED ON LT WING REAR INNER SPAR, RIB 2 - RISDR 2007FA0000628Nut Plate · damagedWHILE UNDERGOING A ANNUAL INSPECTION INVESTIGATION OF NOISE COMPLAINT FROM THE LANDING GEARBOX IT WAS DISCOVERED THAT THE FOUR AN3-6A BOLTS THAT ATTACH THE PART 5011013-3 (BRACKET ACUATOR MOUNTING) & GEARBOX TO THE FRONT SPAR WAS LOOSE. AN ATTEMPT AT TIGHTEN SDR DHL2007804502Frame · crackedRT OUTER WING INBD L/E UPPER FORMER CRACKED 0.500" STA XFS 691.250. REMOVED FASTENERS IAW SRM 51-1-21. PERFORMED STOP HOLE AND FABRICATED (2EA) ANGLE DOUBLER (AL7075T6 0.032") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER IAW SRM 51-1-8BSDR DHL2007804501Frame · crackedRT OUTERWING INBD L/E CRACKED 0.500" AT LWR FORMER STA XFS 635.000. REMOVED FASTENERS IAW SRM 51-1-21. PERFORMED STOP HOLE AND FABRICATED (2EA) ANGLE DOUBLER (AL7075T6 0.032") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLERS IAW SSDR AMWA15036Spar · corrodedCORROSION LT AND AFT MAIN SPAR FLANGE. REPAIRED IAW ENGINEERING REPORT NR 6772-3 REV A DATED JUN 25, 2007.SDR AMWA28032Spar · shearedSHEARED AND STRETCHED RIVETS AT LT AND RT WS 114.25. REPAIRED IAW ER NR 6699-2 REV 1R.SDR DL76S070850Spar · crackedLT WING FRONT SPAR AT NR 8 RIB POST FOUND 1 FASTENER HOLE CRACKED AT RIB POST. LT WING FRONT SPAR NR 8 RIB AREA REWORKED AND FASTENER INSTALLED PER ERA 461699-14AD REV ORG.SDR 2007FA0000631Spar · cracked(2) LONGITUDINAL CRACKS AT SPAR HINGE FITTING. SHAKING AND EXPANDING OF WOOD FIBERS DUE TO MOISTURE OR LACK OF. RECOMMEND USING ALUMINUM SPARS OF SUFFICIENT SIZE AND STRENGTH. (K)SDR DHL2007785004Spar · crackedRIGHT WING T/E AT RWBL 120, HAS A 1.5" CRACK IN RADIUS OF FALSE SPAR LOWER CHORD ANGLE. CUT OUT DAMAGED CHORD AND WEB SECTIONS, FABRICATED NEW WEB SECTION FROM 7075-T6, .032" BY 12" BY 9.5", PO NR 9003458; REPAIR DOUBLER FROM 2024-T3, .050" BY 11" BY 12", POSDR 07FDEA02281Spar · crackedDAMAGED HOLES (CRACKS IN HOLE 1, 2, 3, 4, 5, 6, 8) ON C44 CENTER SPAR WEB REPAIR PERFORMED BY OVERSIZING THE HOLES UNTIL CRACKS ARE REMOVED IAW EA 6-5710-103327 AND RAS 046993/014/2006 ISS A.SDR CA070621003Frame · separated(CAN) DURING TAXI PILOTS FELT THE RT WING DROP SUDDENLY AND HEARD A TIRE SKIDDING SOUND. THEY IMMEDIATELY STOPPED THE AIRCRAFT. MECHANICS FOUND THE LANDING GEAR A-FRAME HAD BROKEN FREE FROM THE MAIN LANDING GEAR TRUNNION. THE LANDING GEAR DID NOT COLLAPSE BUTSDR 07FDEA02231Spar Cap · corrodedRT WING REAR SPAR UPPER CAP FOUND WITH CORROSION AT XORS 1043 - 1045. [07-09-07] COMPLIED WITH FEDEX E.A. 1-5710-111132. CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.SDR 07FDEA02148Spar Cap · oversizedRT WING TRAILING EDGE UPPER CAP AREA, XORS 577 FOUND HOLE ELONGATED. [06-29-07] REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5710-109910, REPAIR CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.SDR 2007UALA01906Spar · damagedFOUND UPPER FLANGE ON LT SUB SPAR IS DAMAGED. SPAR REPAIRED PER SRM.SDR 07FDEA02054Spar Cap · corrodedRIGHT WING, TRAILING EDGE REAR SPAR UPPER CAP FOUND CORRODED AT XORS 1038. [06-18-07] REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-109902. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR KCSA071175Spar · corrodedRIGHT WING FRONT SPAR LOWER CHORD STRAP CORRODED AT FSSO 1520.SDR 2007UALA01761Spar · damagedRT WING REAR SPAR FITTING REQUIRES FREEZE PLUG INSTALLATION. [06-26-07] MAJOR REPAIR: FABRICATED AND INSTALLED FREEZE PLUG. REFERENCE AAR EA REV IR I070357.SDR SWAA072767Spar · crackedDURING SCHEDULED 22Y CHECK, FOUND LEFT WING REAR SPAR UPPER CHORD CRACKED AT STA 274.14. REPAIRED CHORD PER ER.SDR SWAA072768Spar · crackedDURING SCHEDULED 22Y CHECK, FOUND RIGHT WING REAR SPAR UPPER CHORD CRACKED AT STR 2, STA 114. REPAIRED CHORD PER ER.SDR SWAA072769Spar · crackedDURING SCHEDULED 22Y CHECK, FOUND RIGHT WING REAR SPAR UPPER CHORD CRACKED AT STA 224.14. REPAIRED CHORD PER ER.SDR 07FDEA02038Spar Cap · corrodedRIGHT WING, TRAILING EDGE REAR SPAR LOWER CAP FOUND CORROSION AT XORS 1054. [06-18-07] REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-109898. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 07FDEA02037Spar Cap · corrodedRIGHT WING, TRAILING EDGE REAR SPAR LOWER CAP FOUND CORROSION AT XORS 1067. [06-19-07]SDR 07FDEA02015Spar · corrodedLEFT WING REAR SPAR, BETWEEN OUTBOARD ISLAND MOUNTING BRACKET NR 1 AND NR 2 FROM OUTBOARD, LOWER FACE FOUND CORRODED. REPAIRED AS PER FEDEX E.A. 1-5710-111113. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR DHL2007803508Frame · crackedRT WING OUTBD L/E INNER SECTION FORMER CRACKED 0.250", STA XFS 635.000. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED (2EA) ANGLE DOUBLERS AL7075T6 0.032" IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLERS IAW SRM 51-1-8B. INSTALLESDR DHL2007803505Frame · crackedRT WING CTR L/E LWR FORMER CRACKED 0.250" STA XFS 466.615. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED (2EA) DOUBLER (AL7075T6 0.040") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 51-1-21SDR DHL2007803507Frame · crackedRT WING CTR L/E UPPER FORMER CRACKED, STA XFS 397.750. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. PERFORMED STOP HOLE AND FABRICATED (2EA) DOUBLERS (AL7075T6 0.032" / 0.040") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLERS IAW SRSDR DHL2007803501Frame · crackedRT WING OUTBD L/E INNER SECTION LWR FORMER CRACKED 0.500" AT STA XFS 653.750. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED 2EA ANGLES DOUBLERS (AL7075T6 0.032") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLES IAW SRM 51-1-8B. INSTALLEDSDR DHL2007803503Frame · crackedRT WING OUTBD L/E INNER SECTION LWR FORMER CRACKED 0.500" AT STA XFS 616.250. REMOVED FASTENERS IAW SRM 51-1-21. FABRICATED 2 ANGLE DOUBLERS AL7075T6 0.032" IAW SRM 57-2-0 PG 9-10. CLEANED,TREATED AND PRIMED AREA AND ANGLE DOUBLERS IAW SRM 51-1-8B. INSTALL
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