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 VGQY2010080600057Spar · corrodedLEFT WLG WHEEL WELL STA 1241 LBL 10 CENTER TANK REAR SPAR WEB NEAR UPPER CHORD FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-10-01 REV 117. MATERIAL REMOVED= 0.012 INCH, MATERIAL REMAINING= 0.3025 INCH AND FOUND WITHIN LIMITS PER SRM 57-10-01 REV 117. REWSDR FDEA201007302728Spar Cap · damagedRIGHT HAND WING, DURING REMOVAL OF FASTENERS AT WING REAR SPAR LOWER CAP, FOUND 01 EACH HLT339-12 FASTENER NOT STATED INSIDE E.O. 8-5710-7-5007 PART 2. COMPIED WITH E.A. 8-5710-140422, REPAIR IS CLASSIFIED MAJOR PER GMM 6-2-100 REVISION 110.SDR USAA2010072391486Spar · damagedBFM - Q5 - MAJOR REPAIR - ELONGATED HOLE ON THE REAR SPAR TO RT MLG FITTING FASTENER UPPER INBOARD AT RSS 206, WL 172, WBL 135.5. REPAIRED HOLE ON THE REAR SPAR TO RT MLG FITTING FASTENER UPPER INBOARD AT RSS 206, WL 172, WBL 135.5 IAW EA 134289.SDR FDEA201007222646Spar Cap · crackedRT WING SPAR LOWER CAP AT STA XORS 345.750; ALL (6) HOLES SHOW CRACK INDICATIONS. COMPLIED WITH EA 8-5710-123545,SDR AALA20100721TUL13Spar · corrodedCORROSION AT RIGHT WING FORWARD BOOST PUMP BONDING STRAP TO SPAR BEYOND SRM LIMITS. REPAIRED PER EA B737-57-011819 AND SRM 51-10-02.SDR FDEA201007172572Spar Cap · crackedDURING PERFORMING E.O. E8-5710-7-5007 PART 1, RIGHT HAND WING REAR SPAR LOWER CAP HFEC OPEN HOLE INSPECTION 01 EACH HOLE FOUND CRACKED INDICATION. RT WING REAR SPAR LOWER CAP 01 EACH FASTENER HOLE COLD WORKED REPAIRED TO FINAL HOLE SIZE PER STEP 7 OF E.O.8-571SDR FDEA201007152523Spar Cap · damagedHFEC INSP CARRIED OUT AND FOUND 1 EACH HOLE DAMAGED ON RT WING REAR SPAR LOWER CAP AT XORS 354.750. REPAIR CARRIED OUT IAW EA 8-5710-140422, THIS REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100, REV 110.SDR FDEA201007152522Spar Cap · crackedHFEC INSP CARRIED OUT AND FOUND 1 EACH HOLE WITH CRACK INDICATION ON LT WING REAR SPAR LOWER CAP AT XORS 354.750. REPAIR CARRIED OUT IAW EA 8-5710-140423, THIS REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100, REV 110.SDR FDEA201007152521Spar Cap · damagedHFEC INSP CARRIED OUT AND FOUND 3 EACH HOLES DAMAGED ON LT WING REAR SPAR LOWER CAP AT XORS 354.750. REPAIR CARRIED OUT IAW EA 8-5710-140423, THIS REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100, REV 110.SDR DALA1018939005Spar Cap · crackedREF EA 09-471576-12, REV ORIG ME05 HIDDEN DAMAGE: CRACK OF APROX 3.312 INCH ON THE RT WING LOWER SPAR CAP AT STA XRS=108 REF NRC T0178869 AND T0179341. SLOT CUT CRACK IAW AMR 0907304 REV 3, FAB NEW SPLICES IAW AMR0957304, REV 3 REPAIR INSTRUCTIONS 23 AND 24. TSDR DALA1018919005Spar Cap · damagedREF EA 09-471576-12, REV ORIGINAL ME05 OPN NR0 502 REPAIR (5) CRACKS OF 812, .0.750, 0.125, 1.00 LENGTH ON THE WING REAR SPAR LOWER CAP AFT VERTICAL LEG AT INBD ATTACH POINT_OF THE RT WING FLAP HINGE FITTING XRS=164. GAINED ACCESS IAW AMR 0957304 REV 2 AND DWGSDR IPXA10561263Frame · damagedINSPECTION TYPE:C2, NR 2 PYLON, STA 205 UNDER PNL 445AR RT FWD FRAME CHORD HAS OVERSIZED HOLES FROM WORKING FASTENERS, NO EDGE DISTANCE. R & R CHORD IAW SRM 51-40-05-0G AND SRM51-40-02.SDR R61A20100296Spar · damagedDUE TO A GROUND A/C INCIDENT IN PVD WHERE THE AC SUFFERED WINGTIP DAMAGE WITH ANOTHER AC. PERFORMING A MAJOR REPAIR TO THE RT WING SPAR 11 TIP. MAINTENANCE HAS EVALUATED THE DAMAGE AND REQUESTED EMB ENGINEERING ASSISTANCE, AND WAS INSTRUCTED TO REPAIR THE DASDR TRBACPCP2010039Spar · corrodedLT WING LOWER SKIN REAR SPAR AT RIB 11 CORROSION TITANIUM DOUBLER PERMANENT REPAIR. COMPLIED WITH TDMI 570383 LT WING AFT SPAR LOWER CHORD AT RIB 11. NDT ACCOMPLISHED REF NDT REPORT 100617-13, SRI NR DO/TS-2699/10-13512, SRAS NR DO/TS-3072/08. 4749 ISSUE B,SDR GLBA20100618GSpar · damagedMAJOR REPAIR UPON SUBSEQUENT INSPECTION MAINTENANCE FOUND LEFT FORWARD SPAR AFT LOWER FLANGE FOUND TO HAVE BEEN DAMAGED BY LEFT DRAG BRACE NEXT TO UPLOCK BRACKET IN LEFT WHEEL WELL. DAMAGE AT BL 107.0 TO 99.0 AND 104.5 TO 101.5 DELAMINATION IS APPROX 8 " LONGSDR CA100907006Bolt · missingDURING ANNUAL INSP, DISCOVERED EXCESSIVE FORE AND AFT PLAY IN RT WING, PN 22-5708-00-00WIP. MX RECORD REVIEW INDICATED THAT THE RT WING WAS REPLACED ON 4/25/09. REMOVED WING TO INSPECT. DISCOVERED SPAR, MAIN BOLT, BUSHING, PN 20-5700-01-20 WAS NOT INSTALLEDSDR FDEA201006101929Spar Cap · crackedDURING HFEC OPEN HOLE INSP AT LT WING REAR SPAR LOWER CAP STA XORS = 345.75 INBD FWD FASTENER HOLE FOUND CRACKED INDICATION ON UPPER LAYER. R & R IAW SRM 51-33-01 VOL II, REV 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.SDR SWIA201024710Spar Cap · crackedLEFT WING INBOARD INTERNAL AUX SPAR CAP CRACKED. (C-CHECK) REPAIRED SPAR CAP.SDR KCSA101071Spar Cap · damagedLEFT WING UPPER CHORD BEARING BORE ELONGATED ABOVE NR 4 FLAP TRACK AT WBL 235.20.SDR EE4Y100179Spar · corroded((EE4Y)) LT WING FRONT SPAR LOWER CHORD FLANGE WITH CORROSION AT W STA 460. (WO Y10122, SUB JOB 5, ITEM 1).SDR GUUA94057053110ASpar · damagedSPAR DAMAGED, ACFT REQUIRES D+ INSP ACFT COMPANY KIT 118-4014-0003. COMPLIED WITH D+ INSP COMPANY KIT 118-4014-0003.SDR EE4Y100171Spar · corroded((EE4Y)) LT WING FRONT SPAR LOWER CHORD FLANGE WITH CORROSION AT W STA 602. (W/O Y10122, SUB JOB 5, ITEM 3).SDR EE4Y100170Spar · corroded((EE4Y)) LT WING FRONT SPAR LOWER CHORD FLANGE WITH CORROSION AT W STA 520. (W/O Y10122, SUB JOB 5, ITEM 1).SDR 2010FA0000631Frame · cracked((CNQR)) THE PN 6750743-4 FRAME IS PART OF THE AILERON POWER CONTROL UNIT SUPPORT ASSY AND IS APPLICABLE TO ACFT. DURING SCHEDULED INSP, THE FRAME WAS FOUND TO BE BADLY FATIGUE CRACKED AND APPROACHING FAILURE. FAILURE OF THIS FRAME COULD CAUSE LOSS OF AILEROSDR GUUA93657052510ASpar · damagedSPAR DAMAGED, ACFT REQUIRES D+ INSP ACFT COMPANY KIT 118-4014-0003. COMPLIED WITH D+ INSP COMPANY KIT 118-4014-0003.SDR KCSA101061Spar · corrodedCORROSION ON WING CENTER SECTION REAR SPAR, AFT SIDE, BELOW THE UPPER CHORD AT RBL 95.SDR IPXA10M60274Spar Cap · corrodedINSPECTION TYPE:4C, CORROSION AT LT WING UPPER AFT SPAR CAP AT APPROX STA 1042.350. GAINED ACCESS, REMOVED CORROSION, REPAIRED SPAR CAP REF STA SA EA NR 011-5710-01-A2345 REV IR AND UPS EO MD11-5710-38029-A, RESTORED AREA.SDR FDEA201005121523Spar · crackedRT WING T/E FALSE SPAR CHORD CRACKED, WBL 118. REMOVED LOWER CHORD DIM. 20.5", WEB AND DOUBLER IAW DWG NR SR 27-57-038, REV C. FABRICATED 2 ANGLES FROM 7075-0 .071" DIM. 14.5" X 2.75" AND 12.5" X 2.75" IAW DWG NR SR 27-57-038 REV C. HEAT TREATED ANGLES FROM 7SDR FDEA201005121525Spar · crackedRT WING T/E FALSE SPAR CHORD CRACKED, WBL 118.SDR FDEA201005121521Spar · crackedLT WING T/E FALSE SPAR CHORD CRACKED, WBL 118. REPAIRED LT WING T/E FALSE SPAR CHORD WBL 118 IAW DWG NR SR27-57-038, REV C.SDR IPXA10M60293Spar Cap · corrodedINSPECTION TYPE:4C, EVIDENCE OF CORROSION UNDER WING SKIN AT LT WING REAR SPAR, SKIN BULGING NEAR STA XORS.650. GAINED ACCESS, REMOVED CORROSION, REPAIRED LT UPPER SPAR REF STA SA EA NR 011-5710-01-A2346 REV IR AND UPS EO MD11-5710-38030-A.SDR TRBACPCP2010027Spar · corrodedLT WING FRONT SPAR BETWEEN ENGINE AND FUSELAGE CORROSION AROUND 2 LOCK FASTENER. OPENSDR DALA1310700950Spar Cap · crackedRT WING MAIN FRAME LOWER REAR SPAR CAP XRS-164 CRACK REPAIR IAW ERA 481554-14SDR TRBACPCP2010035SPSpar · damagedINSTALLED REPAIR DOUBLER AT RT WING LWR REAR SPAR IAW AE EO E2-57MR-395. REF ART W/O 11951 NRWC 334519, ART FORM L -004-2R1 AND AMS NDT REPORT 100514-13. THIS ACTION CLOSES TDMI 348570218.SDR SWAA102253Fitting · crackedDURING SCHEDULED 10Y CHECK, FOUND CENTER WING FRONT SPAR CHORD FITTING CRACKED AT BS 540+7, LBL 54. REMOVED AND REPLACED FITTING PER SRM.SDR SWAA102252Fitting · crackedDURING SCHEDULED 10Y CHECK, FOUND CENTER WING FRONT SPAR CHORD FITTING CRACKED AT BS 540+7, RBL 7. REMOVED AND REPLACED FITTING PER SRM.SDR SWAA102251Fitting · crackedDURING SCHEDULED 10Y CHECK, FOUND CENTER WING FRONT SPAR CHORD FITTING CRACKED AT BS 540+7, RBL 54. REMOVED AND REPLACED FITTING PER SRM.SDR FDEA201004161211Spar · crackedCRACKED FALSE SPAR AT NR 8 SPOILER ATTACHMENT, WS 171. REMOVED DOUBLER, TRIMMED WEB 12.2500" X 9.5", LOWER CHORD 20.5" LONG IAW DWG NR SR27-57-038 REV C. FABRICATED CHORD SPLICE ANGLES FROM 7075 - 0 .071" X 6" X 14" (2) RADIUS FILLERS FROM 7075 T6 .SDR CALA2010041400137Stiffener · wornSUPPORT TASK, RT WING FRONT SPAR WEB STIFFENER IS WORN INTO BY BLEED AIR DUCT SUPPORT CLAMP FSS 148.9. REMOVED AND REPLACED RT WING FRONT SPAR STIFFENER AT FSS 148.9 REF ECRA 5710-02179.SDR GUUA93557033110ASpar · crackedRT WING LOWER AFT SPAR FLANGE 2 FASTNER LOCATIONS AT WING STA 115.0 AND 115.5 SHOW NDI INDICATIONS. DRILLED AND REAMED FASTENER HOLES AND INSTALLED SPAR ANGLE REPAIR.SDR IPXA10659155Spar · crackedINSPECTION TYPE:6C, LT WING L/E LES675 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR CLIP FOUND CRACK. LT WIING L/E LES675 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR CLIP REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV 46.SDR SWAA101825Spar · corrodedDURING SCHEDULED 26Y CHECK, FOUND RT WING FRONT SPAR WEB CORRODED AT UPPER INBOARD BOLT COMMON TO NR 2 FUEL TANK FWD BOOST PUMP. REPAIRED SPAR WEB PER ER AND SRM.SDR FDEA201003271019Spar Cap · crackedRT WING REAR SPAR REPAIR IAW EA 8-5710-138106, PART 1 INSTRUCTIONS. INTERIM REPAIR ACCOMPLISHED IAW EA NR 8-5710-138106 PART 1, REPETITIVE INSP AT 1650 FLT CYC INTERVALS AND FINAL RESTORATION TO BE ACCOMPLISHED PRIOR TO ACFT REACHING 39357 FLT CYC REF: EA NSDR AALA20100326TUL05Spar Cap · corrodedCORROSION ON SPAR T-CAP BETWEEN WING STATIONS 190 AND 210. REPAIRED PER EA B757-57-009791 DATED 3/26/2010.SDR AALA20100326TUL04Spar Cap · corrodedCORROSION REAR SPAR UPPER T-CAP INBOARD OF MAIN LANDING GEAR FORWARD TRUNNION. REPAIRED PER EA B757-57-009791 DATED 3/26/2010.SDR GUUA95457032010ASpar · damagedCOMPLIED WITH COLD EXPANSION OF FASTENER HOLES IN THE WING REAR SPAR LOWER CAP IAW FAA APPROVED DATA CONTAINED IN THE ACFT COMPANY KIT 118-4014-0003. NOTE: ACFT DOWN FOR KIT WING REAR SPAR INSTALLATION.SDR FDEA201003180904Spar · crackedRT WING LOWER T/E, FALSE SPAR INBD END IS CRACKED AT WBL 118. TRIMMED OUT DAMAGE, FABRICATED NEW INBD WEB USING 7075T-6 .032 DIMS 12.1250" X 9.5" PO 9009201, FABRICATED NEW INBD LWR CHORD SECTION USING BAC1514-1437 7075T-6 PO 2911884 DIMS 20.5" X 3", FABRICSDR CALA2010031600083Spar · damagedSUPPORT TASK OP 17. RIGHT WING, FWD SPAR AT WS 80-6, MIS-DRILLED DURING DRILL-UP OF RIB 26 P/N 757-3263-1 RIB POST. REF EA 5700-02220, REV E, OP 17, STEP 93 REWORK OPENED DISCREPANT HOLE TRUE AND ROUND TO .6265, INSTALLED A FREEZE PLUG AND MADE FILLERS A & BSDR GUUA93357031310ASpar · damagedCOMPLIED WITH COLD EXPANSION OF FASTENER HOLES IN THE WING REAR SPAR LOWER CAP IAW FAA APPROVED DATA CONTAINED IN THE ACFT COMPANY KIT 118-4014-0003.SDR GUUA94557031110ASpar · damagedCOMPLIED WITH COLD EXPANSION OF FASTENER HOLES IN THE WING REAR SPAR LOWER CAP IAW FAA APPROVED DATA CONTAINED IN THE MFG ACFT COMPANY KIT 118-4014-0003.
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