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 CA041206008Spar · cracked(CAN) DURING LANDING PHASE AIRCRAFT ROLLED TO LT WHEN APPROACH FLAPS WERE SELECTED. ROLL RESPONSE WAS CORRECTED WITH AILERON TRIM INPUT. FURTHER FLAP DEPLOYMENT DID NOT CREATE ANY FURTHER CONTROL DIFFICULTY. MAINTENANCE INSPECTED AIRCRAFT AND DISCOVERED THAT SDR CA051108009Fitting · cracked(CAN) DURING A ROUTINE PHASE INSPECTION OF THE WING AND CENTER SECTION OF THE AIRCRAFT, SMALL CRACKS WERE FOUND IN THE RT WING AFT SPAR WING TO FUSELAGE ATTACH FITTINGS (PN 27-22136-006 AND 27-22135-006). THE CRACKS WERE FOUND VISUALLY AND CONFIRMED USING EDSDR CA041119001Spar · crackedWHILE DOING A 100HR INSPECTION ON THE AIRCRAFT, AME'S NOTICED BELLY SKIN ON LOWER RT SIDE WRINKLED. FURTHER INSPECTION REVEALED THAT THE WEB SKIN ON THE REAR OF THE FUSELAGE FRONT SPAR SKIN WAS CRACKED. THE PROTECTIVE TOP CAP OF CARPET WAS REMOVED AND IT WASSDR USAA040972Spar · crackedPIT - Q4 - LT SPAR UPPER CHORD, .0625 INCH CRACK; NR 2 HOLE VERTICAL LEG OF LT SPAR UPPER CHORD AT MLG SUPPORT. INSTALLED FATIGUE ENHANCEMENT PLATE IAW EA 79286A.SDR 2005FA0000809Spar · corrodedUPPER SPAR CAP WAS FOUND WITH SEVERE EXFOLIATION CORROSION BEHIND THE FUEL TANK. TANK WAS PULLED TO COMPLY WITH SB. THERE WAS NO INDICATION OF CORROSION SWELLING ON THE SURFACE OF THE WING. THE AREA WHERE THE CORROSION OCCURRED IS NOT VISIBLE FROM INSPECTIOSDR UPS04843560Spar · crackedINSPECTION TYPE: C1, CENTER WING REAR SPAR LOWER CORD CRACKED IN RT W/W, STA 857, OB CORNER. NDT MAPPED CRACK REF SPMSPM06-10-01.001. STOP DRILLED AND VERIFIED BY NDT. FABRICATED AND INSTALLED REPAIR PARTS PER SRO8570009SDR UPS04443491Spar · crackedINSPECTION TYPE:C, RIGHT WING - MID SPAR UPPER CHORD FASTENER 2EA EDGE FOUND CRACK BETWEEN WS 440 - WS 460. RIGHT WING - MID SPAR UPPER CHORD REPAIRED AS PER SRM 57-10-06 FIG 5, JUST AT WS 440 - 460.SDR UPS04443490Spar · crackedINSPECTION TYPE: C, RIGHT WING - MID SPAR UPPER CHORD FASTENER (1EA) EDGE FOUND CRACK BETWEEN WS 382 TO WS 411. RIGHT WING - MID SPAR UPPER CHORD REPAIRED AS PER SRM 57-10-06 FIG 5, JUST AT WS 382-411.SDR UPS04443481Spar · crackedINSPECTION TYPE: C, LT WING MID SPAR UPPER CHORD FASTENER (1EA) EDGE FOUND CRACK BETWEEN WS 382 TO WS 411. LEFT WING - MID SPAR UPPER CHORD REPAIRED AS PER SRM 57-10-06 FIG 5, JUST AT WS 382-411.SDR 72300084Spar · corrodedA 3 X 3 INCH AREA OF CORROSION ON SPAR CHORD VERT FLANGE.SDR 2004UALA00952Spar · damagedDAMAGE FOUND AT WBL 265 WING FRONT SPAR AT THE DRY BAY ACCESS HOLE NUT PLATE ATTACHMENT. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED FREEZE PLUGS IN 3 HOLES AND INSTALLED NEW DOUBLER.SDR 2004FA0000839Spar Cap · corrodedDURING OUR INITIAL INSPECTION OF THIS AIRCRAFT, DISCOVERED SEVERE INTERGRANULAR CORROSION ON UPPER AND LOWER REAR SPAR CAPS. THE AREA OF CORROSION IS LOCATED INSIDE THE MAIN GEAR WELL ON BOTH LEFT AND RT WINGS. NOTE: THIS AIRCRAFT IS OPERATED IN A SALT AIR SDR 2004FA0000838Spar Cap · corrodedDURING OUR INITIAL INSPECTION OF THIS AIRCRAFT, DISCOVERED SEVERE INTERGARNULAR CORROSION ON UPPER AND LOWER REAR SPAR CAPS. THE AREA OF CORROSION IS LOCATED INSIDE THE MAIN GEAR WELL ON BOTH LEFT AND RIGHT WINGS. NOTE: AIRCRAFT IS OPERATED IN A SALT AIR ENSDR UPS04843457Frame · crackedINSPECTION TYPE: C3, LT WING LEADING EDGE OUTER SECTION STA XFS-759 UPPER FORMER HAS A CRACK AT AFT FASTENER. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-3-0 FIG19, 51-1-20D &51-1-21.SDR 0401949609Spar Cap · corrodedDURING M-CHECK FOUND CORROSION ON RT WING SPAR CAP AT XRS 267. REPAIRED PER EA 96-200541.SDR MW82004F00001Plate · corrodedSPAR KIT PN 58-4008-9S WAS ORDERED FROM MFG AND UPON INSPECTION OF KIT, PITTING WAS NOTICED ALONG THE EDGE OF THE LT PLATE PN 36-430056-6. AFTER CLEANING SOME OF THE PRIMER OFF, THE PITTING WAS NOTICED ON THE ALUMINUM ITSELF. THIS COULD POSSIBLY BE FROM CORRSDR P5CA0401237Spar · corrodedLT WING REAR SPAR LWR FIXED T/E PANEL I/B LWR BEAM AT WBL 128 HAS CORROSION AT FWD TENSION TRES. REMOVE CORRODED DOUBLER, INSTALLED NEW DOUBLER, TREATED & PRIMED PER SRM 51-40-02.SDR 04FDEA02848Spar · crackedFUEL LEAK LT WING REAR SPAR AREA AT XORS STATION 346 LOWER CHORD ANGLE. INSPECTED AREA WITH HFEC AND DETECTED A CRACK INDICATION ALONG HORIZONTAL FLANGE INTO RADIUS AND UP VERTICAL FLANGE. TOTAL LENGTH OF CRACK IS APPROXIMATELY 4.650 INCH.SDR UPS04443318Spar · crackedINSPECTION TYPE:C, CRACK FOUND ON LT BS 1241 WL 170 TO 180 WING REAR SPAR WEB AT KICK FITTING AREA AT HOLE NR 2 BY APPROX .0625 INCH RUNNING O/B & DOWN. HOLE REWORKED AND OVERSIZED AS PER EO B747-5740-17032.SDR UPS04443317Spar · crackedINSPECTION TYPE:C, LEFT BS 1241 WL 180 UPPER WING REAR SPAR CHORD FOUND CRACK AT HOLE NR 10 RUNNING FORWARD APPROX .0625 INCH. CRACKED HOLE REWORKED AS PER EO 5740-17032.SDR UPS04443316Spar · crackedINSPECTION TYPE:C, LEFT BS 1241 WL 180 WING REAR SPAR KICK FITTING NR 1 FASTENER HOLE CRACK REVEALED AT WEB FORWARD LAYER APPROX .0937 INCH IN LENGTH RUNNING O/B AND LOWER. LEFT BS 1241 WING REAR SPAR KICK FITTING NR 1 FASTENER HOLE REWORKED AS PER EO 5740-17SDR UIEA200400169Spar · corrodedFOUND DURING SCHEDULED MAINTENANCE, CORROSION ON FRONT SPAR WEB, FSS 979.27, LOWER CHORD, LEFT SIDE. BLENDED OUT CORROSION WITH 125 RT FINISH. HFEC INSPECTED OPEN FASTENER HOLES, TO ENSURE DEFECT FREE CONDITION. FLAP PEEN BLENDED SURFACES. FABRICATED AND ISDR UIEA200400161Spar · corrodedDURING SCHEDULED MAINTENANCE, CORROSION WAS FOUND LEFT WING SKIN FORWARD OF FRONT SPAR OLES 1378-1387, 1410, 1438-1447. CORROSION WAS REMOVED BY BLENDING. NDT INSPECTED TO CONFIRM DAMAGE FREE CONDITION. BLENDED AREAS WERE FLAP PEENED, ALODINE 1200 AND BMS 1SDR ABXA040339Spar Cap · crackedRIGHT WING REAR SPAR UPPER CAP WAS CRACKED RIGHT BUTT LINE 2. REPAIRED AREA IAW DC-9 SRM.SDR USAA040658Spar · crackedPIT - FOUND UPPER CHORD CRACKED MORE THAN .343, BUT LESS THAN .6285, NR 2 HOLE, LEFT REAR SPAR UPPER CHORD AT RSS 224.14. OVERSIZED HOLE, INSTALLED FILLER, INSTALLED WING SKIN DOUBLER PER EA 78987. (M)SDR SWAA042671Spar · crackedDURING SCHEDULED D-CHECK, FOUND RT WING UPPER REAR SPAR CHORD AT RSS 285, CRACKED. REMOVED AND REPLACED CHORD PER BAC DRAWING, ER, SRM.SDR ABXA040331Spar · crackedRIGHT WING INTERNAL FUEL TANK AT STA XRS 172 LOWER CENTER SPAR AND WEB HAD CRACK AND CORROSION AT SPAR CAP CRACK. CUT OUT DAMAGED AREA OF CENTER SPAR AND WEB IAW REA D857-49982MR. FABRICATED REPAIR PARTS IAW DAC DWG'S 5613912, 3642213, 3644709 AND SRO8570015SDR UPS04243245Spar · corrodedINSPECTION TYPE:C, EVIDENCE OF INTERGRANULAR CORROSION ON REAR SPAR UPPER CHORD, RIGHT WING BETWEEN WS 290-320 APPROX. REPAIR CARRIED OUT IAW UPS EO B727-5710-17848-B APPROX C AND AAAE EO 200 4-083-004 (727-5710-21057).SDR UPS04243220Spar · corrodedINSPECTION TYPE:C EVIDENCE OF INTERGRANULAR CORROSION ON REAR SPAR UPPER CHORD LEFT WING AT WBL 245. HFEC CARRIED OUT IAW B727 NDTM 51-00-00 PT 6 FIG 4. CORROSION MARKED ON AIRCRAFT. REPAIR OF AREA CARRIED OUT IAW EO B727-5710-17848 APPENDIX C AND AAAE EO 2SDR DHL2004801526Frame · crackedLT WING CENTER L/E UPPER FORMER CRACKED 0.500, STA XFS 366.500. REMOVED FASTENERS IAW SRM 51-1-20D PG. 21, SRM 51-1-21 PG.1. FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG.9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLESDR ACE09042004Spar · corrodedWHILE REPAIRING A FUEL LEAK IN THE RIGHT WING MAIN FUEL TANK, FOUND CORROSION ON THE MAIN SPAR LOWER CAP FORWARD FLANGE REQUIRING MAJOR REPAIR. THIS AREA WAS IDENTIFIED AS A SUSPECT CORROSION LOCATION IN RAYTHEON COMMUNIQUÉ NR 71.SDR DHL2004801527Frame · crackedNR. 1358: RT WING CENTER L/E UPPER FORMER CRACKED 0.500, STA. XFS 379.000. REMOVED FASTENERS IAW SRM51-1-20D PG. 21, SRM 51-1-21 PG.1. FABRICATED ANGLE DOUBLER (2024-T3 0.032)IAW SRM 57-2-0 PG. 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED ASDR ABXA040313Spar Cap · damagedFRONT SPAR CAP AT NR 3 PYLON, INSIDE NR 4 MAIN TANK, HAD 3 EACH OVERSIZE HOLES. REPAIRED IAW REA D857-50013MR.SDR 2004F00425Spar · crackedDURING REPLACEMENT OF THE WING REAR SPAR LOEWR CHORD SPLICE PLATE FITTING H-11 BOLTS AS P[ER BOEING SB 747-57A2309, CRACK WAS FOUND COMMON TO THE RIGHT WIND REAR SPAR LOWER CHORD ONLY AT FASTENER CODE 'C' LOCATION. HOLE 'C' REAMED TO 1.316 INCH DIAMETER. NDTSDR DL73S040785Stiffener · crackedWING CENTER SECTION REAR SPAR STIFFENER FOUND CRACKED AT RBL 6.15. REPAIRED IAW ERA 092296-14.SDR 04FDEA02524Spar · corrodedRT WING, REAR SPAR, LOWER CHORD AT XORS= 600 TO XORS= 620 FOUND WITH CORROSION. RT WING, REAR SPAR, LOWER CHORD AT XORS= 600 TO XORS= 620 CORROSION REMOVED PER SRM 51-31-01 VOLUME II COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SDR 04FDEA02523Spar · corrodedRT WING, REAR SPAR, UPPER CHORD AT XORS= 585 FOUND WITH CORROSION. RT WING, REAR SPAR, UPPER CHORD AT XORS= 585 CORROSION. REMOVED PER SRM 51-31-01 VOLUME II COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB, CORROSION ANSDR 04FDEA02522Spar · corrodedRT WING, REAR SPAR, UPPER AND LOWER CHORD AT XORS= 550 FOUND WITH CORROSION. RT WING, REAR SPAR, UPPER AND LOWER CHORD AT XORS= 550 CORROSION. REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX E NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPASDR 04FDEA02521Spar · corrodedRT WING, REAR SPAR, FROM XORS= 917 TO XORS= 1042 FOUND WITH CORROSION. RT WING, REAR SPAR, FROM XORS= 917 TO XORS= 1042 CORROSION. REMOVED PER SRM 51-31-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB, COSDR 04FDEA02520Spar · corrodedRT WING, REAR SPAR, UPPER CHORD AT ABOUT XORS= 598 FOUND WITH CORROSION. RT WING, REAR SPAR, UPPER CHORD AT XORS= 598 CORROSION. REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB, CORRSDR 04FDEA02519Spar · corrodedRT WING, REAR SPAR, UPPER CHORD AT ABOUT XORS= 720 FOUND WITH CORROSION. RT WING, REAR SPAR, UPPER CHORD AT XORS= 720 CORROSION. REMOVED PER SRM 51-31-01 VOLUME II COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB, CORROSSDR 04FDEA02518Spar · corrodedRT WING, REAR SPAR, UPPER CHORD AT ABOUT XORS= 703 FOUND WITH CORROSION. RT WING, REAR SPAR, UPPER CHORD AT ABOUT XORS= 703 CORROSION REMOVED PER SRM 51-21-01 VOLUME II COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB, SDR 04FDEA02517Spar · corrodedRT WING, REAR SPAR, UPPER CHORD AT XORS= 633 FOUND WITH CORROSION. RT WING, REAR SPAR, UPPER CHORD AT XORS= 633 CORROSION REMOVED PER SRM 51-21-01 VOLUME II COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB, CORROSION ANSDR 04FDEA02516Spar · corrodedRT WING, REAR SPAR, LOWER CHORD AT XORS= 622 TO XORS= 642 FOUND WITH CORROSION. RT WING, REAR SPAR, LOWER CHORD AT XORS= 622 TO XORS= 642 CORROSION. REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWERSDR 04FDEA02515Spar · corrodedLEFT WING, REAR SPAR, XORS= 1020 FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 1020 AREA CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LOWER REAR SPAR, CORROSION AND CRACK REPAIR.SDR 04FDEA02514Spar · corrodedLEFT WING, REAR SPAR, XORS= 540 LOWER CHORD AREA FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 540 LOWER CHORD CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LOWER REAR SPAR, CORROSION ANDSDR 04FDEA02513Spar · corrodedLEFT WING, REAR SPAR, XORS= 585 LOWER CHORD AREA FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 585 LOWER CHORD AREA CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LOWER REAR SPAR, CORROSSDR 04FDEA02512Spar · corrodedLEFT WING, REAR SPAR, XORS= 613 LOWER CHORD AREA FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 613 LOWER CHORD CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LOWER REAR SPAR, CORROSION ASDR 04FDEA02511Spar · corrodedLEFT WING, REAR SPAR, XORS= 620 TO XORS= 633, UPPER AND LOWER CHORD AREA FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 620 TO XORS= 633 UPPER AND LOWER CHORD AREA CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, SDR 04FDEA02510Spar · corrodedLEFT WING, REAR SPAR, AT XORS 680 TO XORS 687 LOWER CHORD AREA FOUND WITH CORROSION. N1819 ¾ LEFT HAND WING, REAR SPAR, XORS= 680 TO XORS= 687 UPPER AND LOWER CHORD AREA CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WI
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