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 SWAA031103Rib · crackedDURING SCHEDULED 1/2D CHECK, FOUND BOTH LT/RT WINGS RIBS CRACKED ON THE LOWER SECTION AT WBL 135.5. REPAIRED LOWER CHORDS PER SWA EA.SDR UPS03M41084Spar Cap · corrodedINSPECTION TYPE:C LT WING REAR SPAR AT XORS 772.500 UPPER SURFACE FOUND CORROSION AS MARKED. CORR REMOVED AND REPROTECTED AT REAR SPAR UPP CAP AFT LEG FROM STA XORS 772 TO STA XORS 799 IAW SRM 51-21-01 REV 32 VOL II, MATERIAL REMOVED 0.009, ORG THK 0.266, LEASDR DHL2003604542Frame · crackedRT OUTER WING OB L/E FRAME CRACKED (0.500) STA. XFS.753.000. STOP DRILLED CRACK AT XFS.753.000 AND FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG.9-10. CLEANED,TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SSDR ABXA030173Fitting · crackedRIGHT INBOARD FIXED VANE NR 2 SUPPORT CRACKED. REPLACED BROKEN FITTING IAW DC-9 SRM 51-30-2.SDR DHL2003604541Frame · crackedRT WING OUTBD. L/E FORMER 0.250 CRACKED AT STA. XFS.797.000. STOP DRILLED CRACK AND 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 DOUBLER IAW SRM 57-2-0 PG.9-10, SRM 51-1-20D PG.SDR DHL2003604509Frame · crackedLT WING INBOARD L/E FORMER AT STA XFS 585.000 WITH 0.500 INCH CRACK. STOP DRILLED CRACK AT STA XFS.585.000, FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLESDR DHL2003604508Frame · crackedLT OUTER WING INBOARD L/E FORMER CRACKED 0.500 INCH, STA XFS 622.500. STOP DRILLED CRACK AND 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 DOUBLER IAW SRM 57-2-0 PG 9-10, SRM 51SDR 03FDEA00637Spar Cap · corrodedLT WING, FOUND WING REAR SPAR UPPER CAP UPPER SURFACE WITH CORROSION FROM XORS 830 TO XORS 1090. OUTER LT WING/REAR SPAR TRAILING EDGE - LT REAR SPAR UPPER CAP REPAIRED FROM XORS 830 TO XORS 1090 AS PER FEDEX EA 1-5720-69229, SRM 57-20-00 FIG. 16 VOL. I ANSDR 03FDEA00649Spar · corrodedLT WING FOUND REAR SPAR LOWER CAP WITH CORROSION AT XORS 1090.SDR DHL2003604505Frame · crackedRT WING - CTR L/E INNER PART FORMER CRACKED 1.000, XFS 502.500 (UPPER PART). STOP DRILLED CRACK AND FABRICATED DOUBLER ANGLE (2024-T3 AL0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER ANGLE IAW SRM 51-1-8B. INSTALLED DOUBLER ANGLSDR DHL2003604506Frame · crackedRT WING CTR L/E INNER PART FORMER CRACKED 1.000 INCH, XFS 316.500. STOP DRILLED CRACK AND FABRICATED DOUBLER ANGLE (2024-T3 AL0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER ANGLE IAW SRM 51-1-8B. INSTALLED DOUBLER ANGLE ON RT WISDR UPS03240664Frame · corrodedINSPECTION TYPE: C&SI, FRAME ASSY ON LWR SURFACE OF APU EXHAUST PANEL ON RT WING IS CORRODED. FRAME ASSY REPLACED IAW DRAWING 6562837 & SRM 51-30-32SDR AUS20030598Spar Cap · corroded(AUS) RT WING SPAR CAP RIVET HEADS MISSING. INVESTIGATION FOUND THE SPAR CAP EXTENSIVELY CORRODED.SDR UPS03840682Spar · crackedINSPECTION TYPE: C1, HFEC HOLE INSPECTION DETECTED A CRACK ON THE RT WING FORWARD LOWER SPAR BETWEEN STA. XFS 515-XFS 526.76 IN HOLE NR 8 (PG. 15 OF E.O. DC8-5710-14184-D) COINED 10 EA. HOLES IN CONDITION 1, COLD WORKED 1 HOLE IN CONDITION 2 NDT VERIFIED NOSDR UPS03840635Spar · crackedINSPECTION TYPE: C-3, WHEN INSPECTING LWR FRONT SPAR ON RT WING, FOUND PREVIOUSLY REPAIRED HOLES TO EXCEED LIMITATIONS CALLED OUT IN EO. FABBED & INSTALLED RPR BUSHINGS FOR HOLES 3,5,&11. FABBED RPR ANGLES J060232-53/56/58/60.LOCATED, DRILLED, AND STRESSDR DHL2003801062Frame · crackedLT WING- CTR L/E FORMER CRACKED 0.500 INCH AT XFS 372.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1 AND SRM 51-1-20D PG 21. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9-10. FABRICATED REINFORCING ANGLE (2024-T3 AL0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED ANDSDR DHL2003801063Frame · crackedRT WING CTR L/E FORMER WITH 0.500 INCH CRACK IN STA XFS 410.250. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK AT STA XFS 410.250 IAW SRM 57-2-0 PG 9-10. FABRICATED DOUBLER ANGLE (2024-T3 AL0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PSDR MP011603BSpar · corrodedDURING AD COMPLIANCE, A CLOSE VISUAL AND NDT HFEC INSP OF WING REAR SPAR, A CRACK AND CORROSION WAS FOUND IN THE HEEL OF THE INBOARD PORTION OF THE DETERMINED TO BE OUT OF LIMITS IAW MFG SRM. ENGINEERING WAS CONTACTED AND REPAIRS WERE DRAWN. A SECTION OF THESDR UPS03440543Spar · corrodedINSPECTION TYPE: C, LT WING UPPER SURFACE FRONT SPAR RABBET AREA PANEL FOUND BULGE AT NR 3 SLAT I/B AREA AS MARKED. LT WING UPPER SURFACE FRONT SPAR REPAIRED AS PER RS R57-25-35006 AND ENGINEERING FILE NUMBER 747-57-20040 AT NR 3 SLAT I/B AREA WS 1336SDR UPS03440542Spar · corrodedINSPECTION TYPE: C, LT WING UPPER SURFACE FRONT SPAR RABBET PANEL FOUND BULGE AT NR 4 SLAT O/B AREA AS MARKED. LT WING UPPER SURFACE FRONT SPAR REPAIRED AS RS R57-25-35006 AND ENGINEERING FILE NUMBER : 747-57-20040 AT NR 4 SLAT O/B AREA WS 1294.SDR DL72S030340Spar · crackedTHE LOWER STRUCTURE AND WEB OF THE LT WING AUX SPAR BEAM WERE FOUND CRACKED NEAR THE NR 7 INBD SPOILER ACTUATOR SUPPORT FITTING. THE LOWER STRUCTURE WAS CUT AND THE CRACKED SECTION REMOVED. A NEW SECTION WAS SPLICED IN WITH STEEL REPAIR ANGLES. THE WEB WASDR AUS20030834Spar · corroded(AUS) LT WING MAIN SPAR WEB CORRODED IN AREA BEHIND RIB PN TB20.11.003.100 LOCATED AT WS 660.SDR AUS20030412Spar · corroded(AUS) LEFT WING REAR SPAR HEAVILY CORRODED UNDER THE REAR SPAR ATTACHMENT PLATE.SDR AUS20030381Spar Cap · corroded(AUS) LT WING FORWARD LOWER SPAR CAP CONTAINED TWO AREAS OF EXFOLIATION CORROSION LOCATED BETWEEN RIB 12375 AND RIB 12975. AREAS OF CORROSION APPROXIMATELY 50.8MM BY 25.4MM (2IN BY 1IN) AND 76.2MMBY 25.4MM (3IN BY 1IN).SDR AUS20030676Spar · corroded(AUS) WING SPARS PN 35110061-1 (LT) AND PN 351100612 (RT) CONTAINED EXFOLIATION CORROSION IN THE UPPER AND LOWER SPAR CAPS.SDR FPI2003F00009Spar · crackedAT ANNUAL INSPECTION, CRACKS WERE FOUND IN FORWARD AND AFT CARRY THRU SPAR WEB FACES. THE CRACKS WERE FOUND ABOVE THE INSTALLED WEB REPAIR KITS AT THE UPPER SPAR FITTINGS. THESE NEW CRACKS APPEAR TO HAVE BEEN CAUSED BY THE INSTALLATION OF THE WEB REPAIR ITS SDR FPI2003F00008Spar · crackedAT ANNUAL INSPECTION, CRACKS WERE FOUND IN FORWARD AND AFT CARRY THRU SPAR WEB FACES. THE CRACKS WERE FOUND ABOVE THE INSTALLED WEB REPAIR KITS AT THE UPPER SPAR FITTINGS. THESE NEW CRACKS APPEAR TO HAVE BEEN CAUSED BY THE INSTALLATION OF THE WEB REPAIR KITSSDR USAA030030Spar · crackedPIT - FOUND LEFT REAR SPAR CRACKED .80 INCHES, 2ND FASTENER HOLE AT RSS 224.41. TEMP TIME LIMITED, DOUBLER INSTALLED PER EA 74944. (M)SDR USAA030031Spar · crackedPIT - FOUND UPPER REAR SPAR CRACKED 1 INCH IN LENGTH TWO EACH, RIGHT WING UPPER REAR SPAR AT RSS 224.14. ACCOMPLISHED OVERSIZE OF HOLES AND INSTALLATION OF REPAIR DOUBLER PER EA 75898. (M)SDR ARWA20030308Spar Cap · crackedDURING "C" CHECK INSPECTION THE FOLLOWING WAS FOUND; LT WING STA. XRS 22.000 - STA.XRS 74.000 REAR SPAR UPPER CAP FLANGE WITH 8.00 INCH CRACK.SDR CA030318004Spar · cracked(CAN) 6 CRACKS BETWEEN RIVETS ON VERTICAL FLANGES. BETWEEN WING STA. 35.15 AND 60.0 CRACKS VISUALLY DISCOVERED - CONFIRMED NDT.SDR UPS03440344Spar · corrodedINSPECTION TYPE: C, LT WING MLGWW BS 1241 LBL 'O' PRESSURE BULKHEAD REAR SPAR ATT T-CHORD FOUND SURFACE CORROSION. T-CHORD REPLACED AS PER SRM 51-10-01 PG 8. (DEPTH 0.060 INCH, WIDTH 1 INCH, LENGTH 1 INCH).SDR UPS03240323Spar · crackedINSPECTION TYPE: C, LT WING REAR SPAR HAS ONE CRACK AND 2 CORROSION INDICATIONS AT WS 193 TO 196. REPAIR CARRIED OUT IAW SRM 51-20-04.SDR TIM2003F00000Spar Cap · corrodedDURING AN ANNUAL WING OUTBOARD UPPER AND LOWER MAIN SPAR CAP INSPECTION SEVERAL SMALL SPOTS WERE NOTICED. FURTHER INVESTIGATING REVEALED CONSIDERABLE CORROSION.SDR 0300316744Web · crackedDuring "H" check found cracks in two fastener holes #37 & #39 at right and left wing upper mid spar web between MSS 387.99 & 417.20. Repaired per EA 67-165047.SDR AMWA15Spar · chafedUPON A ROUTINE INSPECTION MAINTENANCE DISCOVERED THE RIGHT SPAR CHAFED ON THE FORWARD SIDE. ALSO THE RT WING MAIN SPAR CHAFED BY FUEL PRESSURE. THE CORRECTIVE ACTION WAS THAT THEY BLENDED OUT THE CHAFFED AREA IN ACCORDANCE TO RAYTHEON FIELD REPAIR. NO TEARDOWNSDR ABXA030276Spar · damagedRIGHT FORWARD LOWER SPAR HAD EXISTING CUTOUT THAT EXCEEDED THE LIMITS OF THE SERVICE REWORK DRAWING SR-8570012. FABRICATED FILLER IAW ABX REA D857-46655MR. ALODINED AND PRIMED IAW DC-8 SRM 51-1-8. INSTALLED IAW DC-8 SRM 51-1-21.SDR 03FDEA00150Spar Cap · corrodedLT WING FWD OF NR 4 SPOILER AREA REAR UPPER SPAR CAP FOUND RIVET PULLED. SNRM NR 112 : WINGS - OUTER WING / REAR SPAR TRAILING EDGE - LT REAR SPAR UPPER CAP REPAIR CARRIED OUT AS PER EA 1-5720-67571, PART 1.SDR UPS03840213Spar · crackedINSPECTION TYPE: C3, PERFORM LT WING AND RT WING FWD SPAR INSPECTION OF LWR SPAR CAP PER EO DC8-5 710-14184-C AS REQUIRED. REAMED 1 DISCREPANT HOLE ON L/W TO .3230, PERFORMED HFEC AND NO CRACKS NOTED PER DAC SPM 06-10-01.003. CHECKED SPAR THICKNESS AT .689 SDR AMWA13Spar Cap · chafedUPON A MAINTENANCE CHECK IT WAS DISCOVERED THAT BOTH THE RIGHT AND LEFT SPAR CAP WAS CHAFING THE WHEEL WELL. BLENDED THE CHAFED AREA IN ACCORDANCE TO RAYTHEON FIELD REPAIR. NO TEARDOWN REPORT WILL BE REQUIRED.SDR AMWA9Spar Cap · chafedUPON A SERVICE INSPECTION MAINTENANCE FOUND THE LEFT AND RIGHT LOWER SPAR CAP BEHIND THE NACELLE INNER FEN WAS CHAFED. BLENDED, ALODINED AND PRIMED BOTH OF THE LOWER WING SPAR CAP IN ACCORDANCE WITH RAYTHEON FIELD REPAIR. REFERENCE NUMBER JV/0215-03. NO TEARDSDR AMWA8Spar Cap · chafedUPON A DETAILED INSPECTION MAINTENANCE FOUND THE ELECTRIC LINE CHAFING ON RIGHT FORWARD WING SPAR IN THE WHEEL WELL. BLENDED LOWER WING SPAR CAP IN ACCORDANCE WITH RAYTHEON FIELD REPAIR. NO TEARDOWN REPORT IS REQUIRED.SDR UPS03840202Spar · crackedINSPECTION TYPE:C3 LT WING FRONT SPAR LOWER CAP XFS 7 HAS A CRACK INDICATION FOUND BY HFEC. STOP DRILLED CRACK, FABBED REPAIR ALODINED AND PRIMED INSTALLED REPAIR.SDR UPS03440229Fitting · corrodedINSPECTION TYPE: C, LT WING REAR SPAR KICK FITTING AREA, CORROSION FOUND ON HOLE-D AT TERMINAL FITTING. D-HOLE REWORK AS PER EO B747-5710-18343A AND RS 57-12-34973.SDR UPS03440228Fitting · crackedINSPECTION TYPE: C, RIGHT BS 1241 WING REAR SPAR KICK FITTING, HOLE D-CORROSION CRACK FOUND APPROX 0.040 INCH RUNNING I/B FWD SURFACE. D-HOLE REWORKED AS PER EO B747-5710-12138 AND EO B747-5710-18343A RS 57-12-34973.SDR UPS03840207Spar · crackedINSPECTION TYPE: C3, LT WING UPPER FRONT SPAR SHOWS EVIDENCE OF STRESS CORROSION AT APPROX ST A XRS 540. REMOVED CORROSION IAW DC8 SRM 51-1-8, FAB REPAIR STRAP AND FILLER IAW R EO G09022. ALODINED AND PRIMED REPAIR IAW DC8 SRM 51-1-8. INSTALLED REPAIR STRASDR CA030218001Spar Cap · corroded(CAN) CORROSION ON UPPER RIGHT AND LEFT FORWARD WING SPAR CAPS BETWEEN WS 223 & 236 AND WS 122 & 132. CORROSION IS BEYOND LIMITS, WINGS TO BE REMOVED AND SPARS TO BE REPLACED AS DIRECTED BY BEECHCRAFT ENGINEERING.SDR SWAA030209Spar · crackedDURING SCHEDULED D CHECK, FOUND RT MLG BEAM REAR SPAR CHORD CRACKED. REMOVED AND REPLACED RT MLG BEAM REAR SPAR CHORD PER BFG ER.SDR DHL2003804900Frame · crackedLT WING CTR L/E FORMER UPPER PART AT STA XFS 347.750 WITH 1.000 INCH CRACK. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, STOP DRILLED CRACK IAW SRM 57-2-0 PG 9 - 10. FABRICATED DOUBLER ANGLE (2024-T3 AL0.040) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED DSDR QXEA0300149Spar Cap · chafedPDX- LEFT HAND WING FRONT SPAR, LOWER CAP IS CHAFED. REPAIRED IAW DHC-8 SRM 51-20-16 AND 51-20-26.
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