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 = '5700' 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 = '5700' 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 IPXA2025052395256Bracket · gougedLH WING, UPPER SURFACE, ATTACHMENT WTB FAIRIG AREA, BRACKET SUPPORT HAS GOUGE (2EA). DOT 103-34 (ATTACHED PHOTO). NSTALLED NEW BRACKET IAW A300-600 SRM 51-40-21. RIVET P/N: CR3213-6-03 BATCH: 0004194656, HI-LOCK P/N: DAN5-6-6 BATCH: 0004178101, COLLAR P/N: NSSDR DALA2025041502917Not Reported · cracked-AD- DUE TO CRACK INDICATION FOUND DURING INSP, COMPLIED WITH AMDS CARD 5720-01103-01B. REQUIRES COMPLETION OF PRI 624259-14. COMPLIED WITH PRI 624259-14AD REV 0, 1, & 2. COMPARED PRI 324259-14AD REV 0, 1, & 2 WITH ERA 624259-14AD REV ORIG AND ALL ITEMS MATCH.SDR DALA2025042303168Unknown · damagedDAMAGE OUT OF SRM LIMITS. FOLLOWING LOG #6984744, C/W REPAIR INSTRUCTIONS PER ER/A 625734-14 REV ORIGINAL SECTION 1.A. PERMANENT REPAIR IS REQUIRED IN ACCORDANCE WITH THIS ER/A PRIOR CLOSING THE LOG. REPETITIVE INSPECTION EVERY DAY. TERMINATING WITHIN 10 FC.SDR JJBA2025123060Fitting · looseAT RH AILERON, MANY LOOSE RIVETS AT DAMPER FITTING. BUSHINGS REPAIR ON RH AILERON LOWER SKIN, AT DAMPER FITTING.SDR 2025FA0000227Clamp · incorrectDURING A SCHEDULED INSPECTION, IT WAS DISCOVERED THAT A LARGE PERCENTAGE OF CONNECTION CLAMPS IN THE ENVIRONMENTAL SYSTEM WERE THE INCORRECT PART NUMBER AND DID NOT FIT THE TUBING. THEY HAD BEEN TIGHTENED COMPLETELY AND WERE STILL TOO LARGE AND LOOSE.SDR DALA2025040102422Structure · cracked-AD- COMPLIED WITH AMDS CARD 5720-01103-01B. REQUIRES COMPLETION OF PRI 623843-14AD DUE TO CRACK INDICATION FOUND DURING INSP. COMPLIED WITH PRI 623843-14AD REV 0,1,2, & 3. COMPARED PRI 623843-14AD REV 0,1,2, & 3 WITH ERA 623843-14AD REV ORIG AND ALL ITEMS MATSDR NACA2025041430005Skin · corrodedCORROSION-SKIN, L/H WING INSPAR LOWER SKIN LOWER SURFACE, WS 846, REAR SPAR.SDR DALA2025031001851Drag Fitting · damagedSHIP 688 A.D.//A.A. DAMAGES WERE FOUND ON OPEN HOLE AT LH ENG DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOW; HOLE #17 CORROSION ON SKIN AND FITTING BTW 1 TO 3 O CLOCK POSITION AND 7 TO 11 O CLOCK POSITION IN REF. CARD 5720-01100-05A JOB # 138-0001 STEP 14. CORRECTISDR DALA2025031001850Drag Fitting · damagedSHIP 688 A.D.//A.A. DAMAGES WERE FOUND ON OPEN HOLE AT LH ENG DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOW; HOLE #9 CORROSION ON SKIN BTW 1 TO 3 O CLOCK POSITION AND GOUGE ON FITTING BTW 11 TO 1 O CLOCK POSITION IN REF. CARD 5720-01100-02A JOB # 141-0001 STEP 25. SDR SWI202503190387Panel · damagedTRANSFER FROM EAML 1549262 : CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 1548503, TRANSITION LEADING EDGE PANEL (620ML) ON RH SIDE REQUIRES REPLACEMENT (FLIGHT 5449 - FILED CLOSED) DRESSED DENT BACK ON PANEL 620ML AT WS139 IN REFERENCE WITH RESDR SWIA202503170004Skin · damagedTRANSFER FROM EAML 1549262 : CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 1548503, TRANSITION LEADING EDGE PANEL (620ML) ON RH SIDE REQUIRES REPLACEMENT (FLIGHT 5449 - FILED OPEN) DRESSED DENT BACK ON PANEL 620ML AT WS139 IN REFERENCE WITH REO SDR JGVR20250303004Structure · corrodedBLENDED ONE AREA OF CORROSION FROM LH LOWER WING FORWARD OF THE AILERON, PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREA PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT BY CLEANING, TREATING, AND PRIMING AREAS.SDR JGVR20250303003Structure · corrodedMECHANICALLY REMOVED CORROSION LOCATED AROUND LH OVERWING FUEL FILLER, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER TEXTRON REPAIR MEMO BY CLEANING, TREATING, AND PRIMING AREAS.SDR JGVR20250303002Rib · corrodedREMOVED EMERGENCY BRAKE LINES AND CARRY THROUGH FITTINGS FROM RH AND LH RIBS AT WS 37, BLENDED CORRODED AREAS, PERFORMED, NDT, AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT BY CLEANING, TREATING, AND PRIMSDR JGVR20250303001Structure · corrodedMECHANICALLY REMOVED CORROSION LOCATED AROUND RH OVERWING FUEL FILLER, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAID AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT BY CLEANING, TREATING, AND PRIMING AREAS.SDR IPXA2025020524347Structure · corrodedOPEN, CORROSION BETWEEN JOINT PLATES 2&3 AT RIB 9. DOT 12-1 APPROVEDSDR DALA2025011600403Wing · pilot errorSHIP 3503 -MISC- DURING TAXI OUT THE RIGHT WING TIP CONTACTED AN RJ AIRCRAFT. CORRECTIVE ACTION: NTSB IS CONDUCTING AN INVESTIGATION AND REPAIRS WILL FOLLOW. REPAIR C/O PER ERA 620966-14 REV. ORIG. PRI REV. 0,1,2,3,4,5,6,7. (LP# 4008640)SDR SCNA20250131039Structure · wornRH WING, SLAT #4 ACTUATOR AREA, FIXED LEADING EDGE WITH WEAR. PERFORMED PERMANENT REPAIR AT R/H WING SLAT #8 ACTUATOR AREA FIXED L/E IAW B737-800 SRM 57-41-01-2R-1 REPAIR 1 PARAG 4 TABLE 202 AND SRM 51-70-04-2R-10 REPAIR 10 PARAGRAPH 4 FIG 201 REV 83.SDR DALA2025010600087Drag Fitting · damagedDAMAGES WERE FOUND ON OPEN HOLES AT RH ENG DRAG FTG CLAMP-UP, HOLE #12 GOUGES ON FITTING BTW 5 TO 7 O CLOCK POSITION , HOLE #13 CORROSION ON SKIN BTW 1 O' CLOCK POSITION, HOLE #18 GOUGE ON SKIN BTW 6 O' CLOCK, IN REF. CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00SDR IPXA2024120658412Seal · brokenSLAT JACK SHUTTER SEAL ON LEFT WING BROKEN RIBS 14/15 REMOVED DAMAGED SHUTTER SEAL. DRILLED AND INSTALLED NEW SHUTTER SEAL IAW SRM 51-40-21.SDR EE4Y2024120521408Skin · damagedPERFORMED REPLACEMENT OF PERMANENT REPAIR INSTALLED AT RH WING SKIN TRAILING EDGE AT RIB 10 AREA, AS PER COOPESA´S EO COO-EO-2024-21191-R00 REV 00, SINCE EXISTING REPAIR WAS FOUND WITHOUT MATERIAL TRACEABILITY RECORDS, THE REPAIR WAS FOLLOWED BY THE EMBRAER DISDR DALA2024120511459Angle · cracked(LOG 0692267) RH PACKS BAY VAPOR BARRIER UPPER ANGLE IS CRACKED AT STA-663, RBL-11. REMOVED, FABRICATED AND INSTALLED R/H UPPER ANGLE REPAIR AT STA 663 BETWEEN RBL 8 TO RBL 18 I.A.W. B737 SRM 57-10-10-2R-5.SDR DALA2024111210875Strut · corrodedSHIP 3160 CORROSION ON INTERCONNECTING STRUT AT RH WING. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT RH AS PER A320 FAM AMM 27-51-44-000-001-A AND FAM AMM 27-51-44-400-001-A. (0655297)SDR IPXA2024110111230Access Panel · damaged**SDR FILED OPEN**LIFT WING LOWER SURFACE, TRAILING EDGE PANEL 541KB APPEARS TO HAVE CIRCULAR REPAIR TOP COVERING MISSING. REINSTALLED PANEL 541KB REFER T3F18E00GZ3QSDR CALA2024110102769Door · missingPDA 2 SLAT # 8, TELESCOPING DUCT TAI SEAL DOOR MISSING PICTURES ATTACHED SDR ACCOMPLISHED NO SDR OR PDA REQUIRED DUPLICATE WRITE UP, REF LP 9419899SDR CALA2024103002752Fairing · brokenUPON WALKAROUND FOUND PANEL 193DL MISSING ABOVE LH WING PART NIS IAD. PARTS UPDATED IN MATERIALS. MORE ITEMS ADDED TO MATERIALS AS PRECAUTIONARY. ALSO REQUIRES 12 EA BACB30LH3-5 (BOLTS), CANNOT ADD MORE ITEMS INTO MATERIALS. GVI OF THE PANEL ATTACH BRACKETS, FSDR IXXA2024092809Fairing · damagedRIGHT WINGLET TIP, FAIRING SKIN HAS LIGHTNING STRIKE DAMAGESDR IXXA2024092808Fairing · damagedRH WINGLIT TIP, FAIRING SKIN HAS LIGHTNING STRIKE DAMAGESDR DALA2024092609450Unknown · unknown(LOG 0572417) WHILE PERFORMING THE SPLIT SCIMITAR INSTALLATION ON A/C 3702, DELTA WORK CARD 5732-01015-01A-07, STEP 23 (APB TASK CARD 737-8340-11 REV E, OPERATION 240), THERE WAS AN INTERFERENCE ISSUE WITH THE L-8 STRAPS AT RIB 22 ON THE LEFT WING.SDR CALA2024090302365Hinge · missingPDA 2 LEFT WING #3 CANOE FAIRING TRAILING EDGE IS MISSING HINGE AND SEAL. REMOVED AND REPLACED SEAL AND HINGE ASSY REF SRM 51-40-02. CYCLED FLAPS. OPS CHECK GOOD PARTS USED: 25-5726-3-0119,QTY :1SDR CALA2024090602392Fitting · crackedSHEAR FITTING AT STATION 540 AND RBL 15.04 IS CRACKED. SUPPORT T ASK NSA EMX N/R 00098.SDR DALA2024081908267Wing · unknownAD/EM-EO TASK - LH WING W/C 5720-01102-06A STEP 36. TO GENERATE A STANDALONE "SDR" LOG PAGE AND ENSURE "SDR REPORTABLE" CHECKBOX IS MARKED ASSOCIATED WITH THE REPAIR. LH WING SEALANT APPLIED AS PER W/C 5720-01102-06A STEP 15. FOUND SATISFACTORY AND W/C STEP 36SDR DALA2024081908266Wing · unknownAD/EM-EO TASK - RH WING W/C 5720-01102-06B STEP 30. TO GENERATE A STANDALONE "SDR" LOG PAGE AND ENSURE "SDR REPORTABLE" CHECKBOX IS MARKED ASSOCIATED WITH THE REPAIR. RH WING SEALANT APPLIED AS PER W/C 5720-01102-06B STEP 13. FOUND SATISFACTORY AND W/C STEP 30SDR DALA2024081408127Not Reported · corrodedSHIP 6710 ER/A 619940-14 REPAIR CORROSION. CORRECTIVE ACITON: REF ERA 619940-14. (0492280)SDR IXXA2024073004Cap · cracked# 1 END CAP CRACKEDSDR IPXA2024082670943Doubler · corrodedR/WING OUT BOARD FLAP, STATIC WICK BASE IS CORRODED. 72-013. ACCOMPLISHED WORK PER EO: EO-91267-REQ 1 AND VTMAE EA 300-5750-27-A3672 REV.- .SDR UIEA2024072200715Chain · missingLH WING, INNER ACCESS PANEL 521QB, ON BOTH REFUEL COUPLINGS, CHAINS MISSING(<P>THE CAPS ASSY OF REFUEL COUPLINGS WERE REPLACED IAW AMM 28-21-01-404-010 REV:142 22/APR/2024. NO FURTHER DEFECTS NOTED</P>)SDR DALA2024073007633Unknown · unknownAD/EM-EO TASK - LH WING W/C 5720-01102-05A STEP 24. TO GENERATE A STANDALONE "SDR" LOG PAGE AND ENSURE "SDR REPORTABLE" CHECKBOX IS MARKED ASSOCIATED WITH THE REPAIR. LH WING SEALANT APPLIED AS PER W/C 5720-01102-05A STEP 11. FOUND SATISFACTORY AND W/C STEP 24SDR DALA2024073007632Unknown · unknownAD/EM-EO TASK - RH WING W/C 5720-01102-05B STEP 24. TO GENERATE A STANDALONE "SDR" LOG PAGE AND ENSURE "SDR REPORTABLE" CHECKBOX IS MARKED ASSOCIATED WITH THE REPAIR. RH WING SEALANT APPLIED AS PER W/C 5720-01102-05B STEP 11. FOUND SATISFACTORY AND W/C STEP 24SDR CALA2024071700224Screw · missingSCREW MISSING LEFT WING GEARBAY TOP. PICTURE IN ATTACHED PICTURE FROM UPPER WING LH SIDE A/C RELEASED IAW EC/RA#5751-01513 INITIATE A DIP TO PERFORM PART 2 AFT EVERY CYCLE AND PART 3 PERMANENT REPAIR WITHIN 2 FLT CYCLES APPROVED FOR 2 CYCLE DIP WITH TAPE INSPESDR DALA2024071507132Nut Plate · damagedSHIP 3118 FOUND DAMAGED NUTPLATE AND MISSING FASTENER ON PANEL 622AB. CORRECTIVE ACTION: REPAIRED PER ERA 619466-14. (5154520)SDR SWAA2024071609879Fairing · cracked#3 FLAP FAIRING TIP APPEARS TO HAVE A STRESS ALONG THE OUTBOARD SIDE<[01] R&R'D #3 FLAP FAIRING TIP IAW AMM 27-51-18;[02] VERIFIED THE FOLLOWING:<BR>R&R'D #3 FLAP FAIRING TIP IAW AMM 27-51-18SDR FDEA202407040935Fairing · damagedRH FAIRING PANEL 196GR PN 113T1740-276 (ALONG WITH ATTACHING PANELS AND DOOR ON FAIRING) DAMAGED FROM FLAP RE-TRACK. TO INCLUDED PN 113T1740-178 FAIRING PANEL, WITH PN 113T2022-32 (WITH SUPPORT ASSY PN 113T2016-2 ATTACHED) & PN 113T2022-36 (WITH SUPPORT ASDR SWIA2024091607002Landing · corrodedLH TIRE BURST COVER 542AZ FWD PANEL LANDING HAS MULTIPLE SPOTS OF CORROSION (FLAGGED). (C-CHECK RO 9/15/2024) TIRE BURST PANEL 542AZ ANGLE LANDING FOUND OUT OF LIMITS. REMOVED AND REPLACED WITH NEW SERVICEABLE UNIT REF CRJ900 SRM 51-42-21-001-001-A01, ASDR UIEA2024060500493Torque Tube · corrodedRIGHT WING TORQUE TUBE WITH EVIDENCE OF CORROSION.(<P>TORQUE TUBE WAS REPLACED PER AMM 27-51-41-400-801. NO FURTHER DEFECTS NOTED.</P>)SDR DALA2024051605275Wing · none(LOG 5926508) ON TAXI IN AT CLE LEFT WINGLET CAME INTO CONTACT WITH RIGHT HORIZ STAB OF SPIRIT A321. PERFORMED VIS INSPS AND NDT REF B737 AMM 05-51-36 AND B737 NDTM PT6 51-00-00 PROCEDURES 16 AND 23 WITH NO FINDINGS RESET CBS AND OP GOOD CVR, INSTALLED NEW WINSDR SWAA2024050782984Shutoff Valve · malfunctionedACFT DEPARTED BLEEDS OFF. GOT CABIN ALTITUDE WARNING AT 12;500. PERFORMED QRH STEPS IMMEDIATE ACTION. BLEEDS TURNED ON. CABIN PRESSURIZATION IN MANUAL. OUTFLOW VALVE AND VSI RESPONDED CORRECTLY. CABIN ALTITUDE SHOWED 25000 FT AT 11000FT. CABIN DIFFERENTIAL AT SDR DALA2024042804739Drag Fitting · damagedAIRCRAFT 6809, DAMAGES WERE FOUND ON OPEN HOLES AT LH ENG DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOW; HOLE #1 CORROSION ON SKIN BTW 1 TO 2 O CLOCK POSITION, HOLE #2 CORROSION ON SKIN AND FITTING BTW 9 TO 6 O CLOCK POSITION, HOLE #4 CORROSION ON SKIN AND FITTING SDR DALA2024043004820Sealant · unknownAD/EM-EO TASK - RH WING W/C 5720-01102-06B STEP 30. RT WING SEALANT APPLIED AS PER W/C 5720-01102-06B STEP 13 FOUND SATISFACTORY.SDR DALA2024043004819Sealant · unknownAD/EM-EO TASK - LH WING W/C 5720-01102-06A STEP 36. LH WING SEALANT APPLIED AS PER W/C 5720-01102-06A STEP 15. FOUND SATISFACTORY AND W/C 5720-01102-06A STEP 36 "SDR REPORTABLE" CHECKBOX IS MARKED. (LP# 0309268)
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