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 04FDEA02509Spar · corrodedLEFT WING, REAR SPAR, AT XORS 690 TO XORS 700 LOWER CHORD AREA FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 690 TO XORS= 700 LOWER CHORD CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LSDR 04FDEA02508Spar · corrodedLEFT WING, REAR SPAR, XORS= 720 UPPER CHORD AREA FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 720 UPPER 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 04FDEA02507Spar · corrodedLEFT WING, REAR SPAR, AT XORS 600 TO XORS 611 LOWER CHORD FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 611 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, CSDR 04FDEA02506Spar · corrodedLEFT HAND WING, REAR SPAR, UNKNOWN TO XORS= 620 UPPER CHORD FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 600 TO XORS= 620 UPPER CHORD CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LOWER SDR 04FDEA02505Spar · corrodedLT WING, REAR SPAR, XORS= 690 UPPER CHORD FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 690 UPPER 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 AND CRACKSDR 04FDEA02504Spar · corrodedLEFT WING, REAR SPAR, AT XORS= 713 UPPER CHORD FOUND WITH CORROSION. LEFT WING, REAR SPAR, XORS= 713 UPPER 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 AND CRACSDR 04FDEA02528Spar · corrodedRT WING, REAR SPAR, UPPER CHORD AREA AT XORS 730 TO XORS 755 FOUND WTH CORROSION. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB - CORROSION AND CRACK REPAIR.SDR 04FDEA02527Spar · corrodedRT WING, REAR SPAR, UPPER CHORD AREA AT XORS 680 TO XORS 690 FOUND WTH CORROSION. CORROSION REMOVED PER SRM 51-31-01 VOLUME II. COMPLIED WITH FEDEX EA 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB - CORROSION AND CRACK REPAIR.SDR 04FDEA02526Spar · corrodedRT WING, REAR SPAR, LOWER CHORD AT XORS 650 AREA FOUND WITH CORROSION. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB - CORROSION AND CRACK REPAIR.SDR 04FDEA02525Spar · corrodedRT WING, REAR SPAR, UPPER CHORD AT XORS 600 TO XORS 650 FOUND WITH CORROSION. CORROSION REMOVED PER SRM 51-31-01 VOLUME II. COMPLIED WITH FEDEX EA 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB - CORROSION AND CRACK REPAIR.SDR UPS04243081Spar · corrodedINSPECTION TYPE: C, CRACK INDICATION AT WS 205 ON LT UPPER CHORD REAR SPAR. REPAIR CARRIED OUT IAW AAAE EO 2004-077-005. REF UPS EO B727-5710-20995.SDR 04FDEA02481Spar · corrodedRT WING, REAR SPAR UPPER CHORD XORS= 1079 FOUND WITH CORROSION. RT WING, REAR SPAR UPPER CHORD XORS= 1079 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 AND CRACSDR 04FDEA02480Spar · corrodedRT WING, REAR SPAR UPPER CHORD XORS= 1042 FOUND WITH CORROSION. RT WING, REAR SPAR UPPER CHORD XORS= 1042 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 AND CRACKSDR 04FDEA02479Spar Cap · corrodedRT WING, WING PLANK, UPPER SURFACE, MOST OUTBOARD AFT CORNER ABOUT XORS= 1090 TO XORS= 1094 FOUND WITH CORROSION AND FIXED TRAILING EDGE PANEL FOUND BULGING. RT WING, WING PLANK, UPPER SURFACE, MOST OUTBOARD AFT CORNER XORS= 1090 TO XORS= 1094 CORROSION REMSDR USAA040416Spar · crackedPIT - FOUND REAR SPAR UPPER CHORD CRACKED .1888 INCH, RIGHT WING, REAR SPAR, UPPER CHORD AT RSS 224.14 AT SECOND HOLE. INSTALLED DOUBLER PER EA 78782. (M)SDR USAA040415Spar · crackedPIT - FOUND REAR SPAR UPPER CHORD CRACKED .1888 INCH, AFT WING, REAR SPAR, UPPER CHORD AT RSS 224.14 AT SECOND HOLE. INSTALLED FREEZE PLUG PER EA 78781. (M)SDR USAA040504Spar · crackedPIT - FOUND LEFT WING SPAR CRACKED .09375, AFT SPAR LEFT MAIN GEAR AREA. REWORKED HOLE PER EA 78859, REAMING HOLE AND INST BUSHING. (M)SDR HYTA2004007Spar · chafedLOWER SURFACE OF LT AND RT FORWARD WING SPARS AND LIFT STRUT ATTACH FITTINGS HAVE BEEN CHAFED BECAUSE OF CONTACT WITH THE LIFT STRUT UPPER FAIRING/COVER. WORST DAMAGE WAS LESS THEN .005 INCH IN DEPTH AND WAS EASILY BLENDED OUT. APPLIED VINYL CHAFE TAPE TO SPSDR UPS04842914Spar Cap · crackedINSPECTION TYPE:C1 WING CENTER SPAR LOWER CAP AT WING STATION XCW 36 IS CRACKED. STOP DRILLED CRACK NDT VERIFIED STOPDRILLS TERMINATED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER, TRIPLER AND REPAIR ANGLE IAW SAA SK 802-190 AND UPS EO DC8-5710-20888-A.SDR DHL200474005Spar · corrodedDURING AN (A) CHECK, INTERIM REPAIR INSTALLED ON LT WING STA.137.8 LOWER FRONT SPAR CHORD PLATE. REMOVED INTERM REPAIR AND TRIMMED OFF 3.7500 INCH IB END SECTION OF LT WING FRONT SPAR LWR CHORD PLATE FROM WS 136.00 T0 139.75 DUE TO CORROSION DAMAGE BEYOND ALLSDR GTIA040670Frame · crackedDTW - FOUND 2 RIGHT WING LEADING EDGE FORMERS AT APPROX STATION 351 CRACKED. (M)SDR DL767040663Fitting · damagedLEFT WING FRONT SPAR OUTBOARD PITCH LOAD FITTING HAS TWO DAMAGED HOLES DUE TO TOOLING WHILE ACCOMPLISHING EO 01-074906-03AD. REPAIR IAW ERA 091345-14AD.SDR CA040720002Spar · wornDURNG 100 HOURS INSPECTION, RT WING REAR SPAR ATTACHMENT BOLT P/N NAS464P6LA6 FOUND LOOSE. BOLT WAS REMOVED AND FOUND SEVERLY DAMAGED (DEFORMED) AND BOTH SPAR FITTINGS P/N 68621-003 AND 66762-000 BOLT HOLES FOUND ELONGATED. BOTH SPAR FITTINGS WERE REPLACED, SDR 2004FA0000562Spar · crackedLT AFT WING SPAR HAD A VERTICAL COMPRESSION CRACK AT THE OB EDGE OF THE LIFT STRUT PLATE. ALSO, IT WAS CRACKED HORIZONTALLY FROM THE COMPRESSION CRACK TO THE OB LIFT STRUT ATTACHMENT POINT. ALSO, ALL FOUR SPARS WERE CRACKED AT THE IB WING ATTACHMENT BOLT HOLSDR ASOA04543Frame · crackedDURING A C-CHECK IN YUL, THE RIGHT WEB WING BOX AT FRAME 28A WAS FOND TO BE CRAKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT WEB WING BOX AT FRAME 28A IAW SRM 51-25-01. (M)SDR ABXA040254Cap · crackedTRAILING EDGE FITTING CRACKED AT INBOARD SPOILER INBOARD END STOP PAD. REPLACED FITTING IAW DC-9 MM.SDR DHL2004745537Spar · crackedDURING A C-CHECK, 4 INCH CRACK ON DOUBLER FWD OF FWD EDGE OF UPPER MAIN SPAR LOCATED ABOVE NR 5 FLAP ACTUATOR AFT END RWS 147 (RIGHT WING). CUT OUT SKIN SPLICE SIZE 10.25 X 2.5 INCH ON L/E SKIN ABOVE NR 5 FLAP ACTUATOR AFT END RWS 147 IAW B727 SRM 51-10-1. FSDR 04FDEA01934Spar · damagedRIGHT HAND WING STATION XW255.000, LOWER SPAR BEAM OUTBOARD HOLE "C" ON PAGE 9 OF 18 OF EO 8-5750-7-5001 PART 2, HOLE HAS TOOLING DAMAGE. REAMED HOLE TO FINAL SIZE OF 1.0022, ALODINE BORE IAW EA 8-5710-77571, FABRICATED BUSHING IAW EA 8-5710-77571, PERFORMED SDR 04FDEA01935Spar · damagedRT WING STATION XW255.000, LOWER SPAR BEAM OUTBOARD HOLE "C" ON PAGE 9 OF 18 OF EO 8-5750-7-5001 PART 2, HOLE HAS TOOLING DAMAGE. REAMED HOLE TO FINAL SIZE OF 1.0022, ALODINE BORE IAW EA 8-5710-77571, FABRICATED BUSHING IAW EA 8-5710-77571, PERFORMED FPI INSPSDR C2XA04SH452Spar · crackedDURING C-CHECK EDDY CURRENT INSPECTION USING EDDY CURRENT PROBE TEST BLOCK TB-M030B AS A STANDARD, LT WING SPAR 3 UPPER O/B HOLE FOR TORQUE BOX 1 ATTACH REVEALED A CRACK. MX REAMED HOLE TO 8.382MM(.330) AND REINSPECTED. CRACK WAS NOT REMOVED. HOLE WAS REAMESDR DHL2004804506Frame · crackedRIGHT WING CTR L/E UPPER FORMER CRACKED 1.000, XFS 316.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLER (AL 2024-T3 0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER IAW SRM 51SDR DHL2004804515Frame · crackedLEFT INNER WING L/E OUTBOARD SECTION FORMER CRACKED 0.500, STA XFS 641.250. REMOVED FASTENERS IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 21. PERFORMED STOP HOLE IAW DC8 SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024-T3 0.032) IAW DC8 SRM 57-2-0 PSDR DHL2004804514Frame · crackedLEFT OUTER WING L/E OUTBOARD SECTION FORMER CRACKED 0.500, STA XFS 860.000. REMOVED FASTENERS IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 21. PERFORMED STOP HOLE IAW DC8 SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024-T3 0.032) IAW DC8 SRM 57-2-0 PSDR AMTA200400801Plate · crackedFOUND RIGHT WING T/E LOWER SPAR WIGGLE PLATE CRACKED AND PULLED FASTENERS BETWEEN WS 328 TO WS 336. FOUND CRACK TO BE OUT OF LIMITS. REMOVED AND REPLACED THE RT WING T/E LOWER SPAR WIGGLE PLATES FROM WS 328 TO WS 336 IAW SRM 51-40-02 AND SRM 51-40-05. (M)SDR DHL2004804503Frame · crackedLEFT JOINT FLAP FORMER CRACK, STA XW 122.000. FABRICATED ANGLE DOUBLER (2024T3 0.050) IAW DC8 SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW DC8 SRM 57-2-0 PG 9-10, DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-21A PG SDR AALA20040751Spar · puncturedAFW - RIGHT WING FORWARD SPAR PUNCTURED AT STATION 1028. AREA IS 1 INCH BY 0.125 INCH. TRIMMED OUT THE DAMAGED PORTIONS OF SPAR WEB BETWEEN FSS 1022 AND 1032 AND SPLICED IN A NEW WEB SEGMENT FABRICATED FROM 0.140 INCH THINK 2024T3 ALUMINUM. TWO 0.080 INCH TSDR QXEA200400469Spar · corrodedPDX - CORROSION ON FRONT SPAR LOWER AFT FLANGE UNDER PANEL 625 AT ONE INCH AFT OF FRONT SPAR VERTICAL PANEL AT RIGHT HAND WING STATION 423.00. REPAIRED IAW DHC-8-200 MM 57-20-00, TASK 57-20-00-400-801.SDR GTIA040660Frame · crackedFTW - FOUND LT WING FIXED LEADING EDGE COMPARTMENT XFS 267 TWO EACH, FRAME CRACKED. STOP DRILLED CRACKS. FABRICATED TWO REPAIR DOUBLER. INSTALLED TWO FORMER REPAIR DOUBLER AND L-ANGLE. (M)SDR GTIA040664Frame · crackedFTW - FOUND LOWER FIXED LEADING EDGE COMPARTMENT XFS 330 LEADING EDGE FRAME CRACK. STOP DRILL CRACK AT FORMER. FABRICATED 3 AND DRILLED REPAIR FORMER. INSTALLED REPAIR PARTS. (M)SDR 2005FA0000189Spar Cap · corrodedWHILE PERFORMING A 3 YEAR INSPECTION OF THE WING CENTER SECTION IAW AD, NOTE: 2002-26-02 AND MFG SB NR 31, THE FORWARD UPPER SPAR CAPSTRIP, PN 415-13027 WAS FOUND TO HAVE AN AREA OF INTERGRANULAR (IG) CORROSION NEAR THE UPPER WING ATTACH FITTING. THE CORROSIOSDR 2004FA0000574Spar · damagedTWO SPARS SPLIT AT WING ROOT WING ATTACH FITTINGS, ONE SPAR SPLIT AT WING LIFT STRUT ATTACH FITTING. SPLITS FOUND DURING ANNUAL INSPECTION. PROBABLE CAUSE: DRYING AND SHRINKAGE.SDR 04FDEA01863Spar Cap · crackedWING LEFT REAR SPAR AFT LOWER CAP CRACK AT XORS 412. THE CRACK EXTENDS INTO THE VERTICAL LEG AND FWD HORIZONTAL LEG. PERFORM PERMANENT REPAIR SIMILAR IN CONCEPT TO DWG SR10570019 WITH DIFFERENT FASTENER CALL OUTS TO COMPENSATE FOR PREVIOUS REWORK IAW EA 8-57SDR 04FDEA01779Spar Cap · crackedDURING C-CHECK AT OAN, INSPECTION FOUND A CRACK IN THE REAR SPAR LOWER CAP AT XORS 412. THE CRACK EXTEND INTO THE VERTICAL LAG AND FWD HORIZONTAL LAG, AND IS CONSISTENT WITH CRACKING DESCRIBED IN S/B DC10-57A137.SDR 2005FA0000695Spar · crackedA CRACK IN THE REAR SPAR OF THE RT WING WAS FOUND. THIS CRACK IS RUNNING WITH THE WOOD GRAIN, AND APPROX 13 INCHES LONG. THE CRACK IS EMANATING LT AND RT OF CENTER FROM THE UPPER BOLT HOLE OF THE MOST IB COMPRESSION STRUT. AFTER DISASSEMBLY IT WAS DETERMINSDR AUS20040460Spar · cracked(AUS) LT AND RT FORWARD AUXILIARY SPARS CRACKED AT IB LOWER RAD II LOCATED AT STN 27. CRACKS EXTEND FOR APPROXIMATELY 12.7MM(0.5IN) OB OF THE END OF THE SPAR IN A HORIZONTAL PLANE.SDR SWIA200413412Spar Cap · crackedLEFT WING LOWER SURFACE OUTBOARD OF LEFT NACELLE FUEL LEAKING NEAR SKIN JOINT. FOUND WING LOWER FORWARD SPAR CRACK CRACKED. REPAIRED SPAR CAP IAW EMB SRM 57-20-05.SDR AUS20040446Spar · corroded(AUS) RT WING MAIN SPAR ANGLE CONTAINED EXFOLIATION CORROSION IN AREA OF WING ATTACHMENT ANGLE.SDR ABXA040197Spar Cap · corrodedWING FRONT SPAR LOWER T-CAP CORRODED BETWEEN LONGERON 30 AND LONGERON 29 LEFT UNDER THE ANTI-ICE DUCT. REPLACED T-CAP IAW DWG 5914865.SDR 2004FA0000544Spar · damagedA LONGITUDINAL CRACK WAS FOUND AT OB AILERON ATTACH FITTING OF THE REAR WOOD SPAR. THE CRACK IS LOCATED ON RT WING REAR SPAR, OB AILERON ATTACH POINT EMANATING FROM LOWER BOLT HOLE ON FORWARD SIDE OF SPAR. THE CRACK WAS FOUND DURING ANNUAL INSP WHILE COMPLINSDR DHL2004803548Spar Cap · crackedBOLT HOLE OUTBD END OF LT WING INBD LWR AUX SPAR CAP WITH 1.000 AND 2.250 LENGTH CRACKS IN IT (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-1-0 PG 1. REMOVED CRACKED LT INBD LWR AUX SPAR CAP IAW DC8 SRM 51-1-20D PG 21, DC8 SRM 51-3-0 PG 1. CLEANED,
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