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 AU970447Spar Cap · cracked(AUS) WING LOWER SPAR CAP CRACKED THROUGH SPLICE HOLE - CRACK LENGTH APPROXIMATELY 31.75MM (1.25IN) - FOUND DURING MAGNETIC PARTICLE INSPECTION IAW SB-AG-39SDR 97ZZZX2653Spar · corrodedDURING ANNUAL INSPECTION, FOUND LT WING MAIN SPAR UPPER CAP SEVERELY CORRODED ON FWD FLANGE. ONLY WAY TO DETECT IS WITH A MIRROR THROUGH FWD WHEELWELL INSPECTION PANEL. WING REMOVED AND SPAR REPLACED. SUBMITTER STATED INTERGRANULAR CORROSION IS THE CAUSE.SDR UPS97223119Spar Skin · corrodedINSPECTION TYPE:D, NR 2 FUEL TANK FRONT SPAR SKIN IS CORRODED RT WING. CORROSION BLENDED OUT IAW SRM 51-10-6.SDR 97ZZZX2664Spar · corrodedDURING HIDDEN DAMAGE INSPECTION OF WINGS AFTER HAIL AND WIND DAMAGE, FORWARD LEFT WING SPAR, EXTRUDED STIFFENER WAS FOUND TO HAVE SEVERAL SPOTS OF INTERGRANULAR CORROSION. SUBMITTER STATED THIS IS A COMMON PROBLEM ON CESSNAS THAT DID NOT HAVE ANY WING PARTS PSDR 97ZZZX3322Spar · corrodedWING SPAR CORROSION DUE TO BONDING MATERIAL AND OUTDOOR ELEMENTS. TIED DOWN OUTSIDE FOR SEVERAL YEARS WITHOUT USE.SDR MWEA97324Aux Spar · improper repairDURING INSPECT, RT WING AUX SPAR INSPECT DOES NOT C/W SB57148. MAINT C/W SB57-148.SDR MWEA97323Spar Cap · corrodedDURING INSPECT, STA XRS 102 AND 112 RT WING AFT SPAR UP CAP EXFOLIATION CORROSION. MAINT REPAIRED IAW DAC DRWG RO9570041.SDR MWEA97312Spar Cap · corrodedDURING INSPECT, LT WING FWD FACE FRONT SPAR LWR CAP FWD FLANGE STA 132 TO 140 MOD CORROSION. MAINT REPAIRED IAW DAC TELEX SVC-MSP-0297/JLW 10 MAR 97.SDR AU970883Spar · cracked(AUS) WING FORWARD SPAR FORWARD AND REAR RH WEBS CRACKED - FOUND DURING INSPECTION IAW AD/BEECH55/62 AMDT4 AND BEECH SB2269SDR ABXA9700927Spar Cap · corrodedDURING C-CHECK, FOUND THE CENTER WING SPAR AFT VERTICAL FACE OF THE SPAR CAP AT STA XCW -40 SEVERLY CORRODED. REPAIRED IAW ABX REA D957-19174-MR.SDR GAIA2197Spar Rail · corrodedTAT - DURING C-CHECK INSPECTION, FOUND CORROSION AT UPPER LT TOP AFT WING SPAR RAIL AT FUSELAGE WING FITTINGS. CORROSION DAMAGE SUBMITTED TO TRACOR COM JET/ CONVAIR FOR EVAULATION. THE ABOVE AREAS WERE FOUND TO BE IN LIMITS IAW TRACOR MSG NR 505-97-WLD-058 DSDR AALA970774Spar · corrodedTUL - FRONT WING SPAR CHORD ANGLE AND WEB CORRODED LOWER AREA AT THIS SEAL RETAINER. CUT OUT CORRODED WEB, BLENDED OUT CHORD ANGLE CORROSION PER SRM 57-10-1. INSTALLED WEB AND CHORD ANGLE. REPAIR PER ESO 11697 DATED 4-4-97. 77,504 HOURS. CYCLES, 52,602. SDR TSAA9757088Spar Chord · corrodedDURING HEAVY MAINTENANCE VISIT, EXFOLIATION CORROSION FOUND ON RIGHT WING LEADING EDGE OUTBOARD OF NR 5 SLAT ACTUATOR. REPAIRED PER ECO NR 1803 R3-WING FRONT SPAR LOWER CHORD FORWARD HORIZONTAL FLANGE LOWER SURFACE CORROSION REPAIR. AIRCRAFT RETURNED TO SERVISDR DHL9780128CSpar · crackedAT C-CHECK, FOUND .1875 HOLE AT RT X69.5 SHOWED CRACK INDICATION AT BOLT HOLE NR 1. CONFIRMED CRACK BY NDT, CUT OUT DAMAGED AREA OF SKIN TO REWORK DAMAGED SECTION, FABRICATED FILLER, TREATED AND CLEANED SPAR CAP. INSTALLED FILLER PER SRM 51-3-1 AND DOUGLAS DSDR AU970840Spar Cap · cracked(AUS) LH AND RH WING LOWER SPAR CAPS PNO 202077901 AND PNO 202077902CRACKED IN SPLICE BLOCK HOLESSDR UPS97222643Spar Chord · corrodedINSPECTION TYPE:SI, CENTER SECTION UPPER REAR CHORD HAS EVIDENCE OF CORROSION SEPARATED FROM WEB LBL 6-36 WL 190. CORROSION REMOVAL WAS OUT OF LIMITS. REMOVED AND REPLACED REAR SPAR UPPER CHORD, SPLICE AND WEB ALL WORK DONE PER EWO NR 97-2109, UPS FILE NR 72SDR AU970466Spar Cap · cracked(AUS) LH AND RH WING LOWER SPAR CAPS PNO 20207-T901 AND PNO 20207-T902 CRACKED - LH LOWER SPAR CAP HAS ONE CRACK IN TWO HOLES - RH LOWER SPAR CAP HAS TWO CRACKS IN OUTBOARD HOLE - FOUND DURING FLUORESCENT MAGNETIC PARTICLE INSPECTION IAW AG-39SDR RAAA97B2019Spar Chord · corrodedDURING SCHEDULED C1 CHECK, FOUND RIGHT WING FRONT SPAR UPPER CHORD CORRODED AT WS 513. REPAIRED PER BOEING MSG RVV-SEA-97-0004RR.SDR RAAA97B2018Spar Chord · corrodedDURING SCHEDULED C1 CHECK, FOUND RIGHT WING FRONT SPAR UPPER CHORD CORRODED AT WS 524. REPAIRED PER BOEING MSG RVV-SEA-97-0004RR.SDR RAAA97B2017Spar Chord · corrodedDURING SCHEDULED C1 CHECK, FOUND RIGHT WING FRONT SPAR UPPER CHORD CORRODED AT WS 499. REPAIRED PER BOEING MSG RVV-SEA-97-0003RR.SDR AU970375Spar · incorrect repair(AUS) LH WING SPAR INCORRECTLY REPAIRED IN AREA BETWEEN STA 136.188 ANDSTA 148.875 - CORROSION HAD BEEN REMOVED FROM THE SPAR CAP TO A DEPTH OF 2.6162MM BY 50.8MM WIDE BY 26.9MM LONG (0.103IN DEEP BY2.0IN WIDE BY 1.060IN LONG) - REPAIR HAD BEEN CARRIED OUT THRSDR 9708101143Spar Chord · crackedDURING M-CHECK, FOUND CRACK IN RADIUS AT AFT UPPER SPAR CHORD WING STA XW 948-946 LEFT WING. REPAIRED PER EA 11-123995.SDR RAAA97B2009Spar Chord · corrodedDURING SCHEDULED S4 STRUCTURAL/CPCP INSPECTION PER CARD S4 14108, FOUND CENTER WING UPPER REAR SPAR CHORD CORRODED, LBL 50 TO LBL 70 AND RBL 40 AT BS 870. REPLACED CENTER WING UPPER REAR SPAR CHORD PER BOEING MSG 9710012RR AND 970010TR.SDR UPS97222626Spar Chord · corrodedINSPECTION TYPE-SI, WHILE WORKING CUSTOMER CARD 510847, FOUND THE LOWER CENTER SPAR CHORD TO BE CORRODED. REMOVED CORRODED SPAR CHORD PROCURED NEW SPAR CHORD AND INSTALLED IAW EWO 97-2136 UNDER FILE NR 727-57-1812.SDR DLL15970733Spar Cap · crackedSEVERAL HOLES IN THE RT WING REAR SPAR WERE FOUND CRACKED IN THE UPPER SPAR CAP BETWEEN IWS 293.58 AND IWS 346.109. THE HOLES ARE COMMON TO THE SPAR WEB AND SPAR CAP.SDR AU970399Spar · corroded(AUS) RH WING REAR SPAR CORRODED IN ROOT AREA BENEATH STEEL ATTACHMENT BRACKETSDR CALA9700625Spar · crackedDURING 1/2 D-CHECK INSPECTION, FOUND RT WING REAR SPAR CRACKED 1.75 INCH BELOW I/B LOWER MOUNT FOR NR 2 FLAP HINGE. REPAIRED PER ECRA 5761-01001.SDR 97ZZZX1859Spar · corrodedDURING MAINTENANCE TO CHANGE THE WING FUEL TANK FLEXIBLE HOSES, FOUND INTERGRANULAR CORROSION IN THE AREA WHERE THE HOSES PASS THROUGH THE SPARS, AND THE TOP AND BOTTOM OF THE RIGHT SPAR STRUCTURE.SDR 97ZZZX1858Spar · corrodedDURING MAINTENANCE TO CHANGE THE WING FUEL TANK FLEXIBLE HOSES, FOUND INTERGRANULAR CORROSION IN THE AREA WHERE THE HOSES PASS THROUGH THE SPARS, AND THE TOP AND BOTTOM OF THE RIGHT SPAR STRUCTURE.SDR 97FDEA00218Spar · crackedNR 0025 003, CRACK AT LT WING REAR SPAR UPPER CHORD AT RSS 300.SDR UPS97822828Spar Cap · crackedINSPECTION TYPE-C, LT MLG WHEEL WELL, WING REAR SPAR LOWER CAP AT FASTENER 6 INCHES OUTBOARD FROM KEEL BEAM STA 857 HAS A CRACK. REMOVED FASTENERS (10) ALONG REAR SPAR AFT SIDE, REAMED DAMAGED HOLE TO .375, CUTOUT CRACKED AREA, FABRICATED REPAIR STRAP, FILLERSDR 97ZZZX2349Spar · corrodedHEAVY CORROSION FOUND DURING ROUTINE INSPECTION OF MAIN SPAR. ALSO, 2 CRACKS .1250 INCH LONG IN THE WELD AT RIGHT WS 64.SDR UPS97822705Spar Cap · crackedINSPECTION TYPE-D HFEC INSP DETECTED A CRACK APPROXIMATELY .375 INCH LONG LOCATED AT SECOND FASTENER HOLE INBD OF NR 1 PYLON ON THE LT WING FRONT SPAR LOWER CAP. REEMED NR 10 HOLE TO .750 DIAMETER HOLE, COLD WORKED HOLE AND INSTALLED FREEZE PLUG, INSTALLED RESDR CALA9700512Spar Web · crackedINSPECTION FOUND A .75 CRACK IN WEB AT FRONT SPAR JUST OUTBOARD OF LT FORWARD TERMINAL PIN FITTING. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-40-2.SDR CKSA97114Spar Cap · crackedDURING C-1 CHECK INSPECTION, FOUND LEADING EDGE STA WX454 LOWER SPAR CAP CRACKED. INSTALLED REPAIR IAW SRM 57-2-0 FIGURE 2 AND REPAIRED RIB IAW AIA/E/2478 EA 97-023D. C-1 CHECK INSPECTION WORK CARD NUMBER 1004. NON-ROUTINE TASK CARD NUMBER 93409.SDR CKSA97065Spar · corrodedDURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION, TOP OF RIGHT REAR SPAR STA ZR329.250 CORRODED. REPAIRED IAW SKETCH AIA/E/2295. CORROSION TASK CARD NUMBER 6800-0552. NON-ROUTINE TASK CARD NUMBER 82911.SDR CKSA97060Spar · misdrilledDURING CPCP CHECK INSPECTION, FOUND MISDRILLED HOLES IN FRONT SPAR XFS366. REPAIRED IAW SKETCH AIA/E/2376. CORROSION TASK CARD NUMBER 116L/R-0552. NON-ROUTINE TASK CARD NUMBER 84740.SDR CKSA97029Auxilliary Spar · crackedDURING CPCP CHECK INSPECTION, FOUND RIGHT AUXILLIARY SPAR LOWER OUTBOARD END CRACKED. REPLACED AUXILLIARY SPAR IAW DC8 DRAWING 5616128. CORROSION TASK CARD NUMBER 119L/R-0551. NON-ROUTINE TASK CARD NUMBER 82905.SDR 9709046718Spar Web · corrodedDURING ARMAR, FOUND CORROSION ON LEFT WING FRONT SPAR WEB FSS 607. REPAIRED PER \NEA 67-121744.SDR MWEA97141Spar Cap · corrodedDURING INSPECTION, LT WING AFT SPAR LWR CAP AT STA XRS 531 TO 537 XRS 543 TO 546 HEAVY CORRODED. MAINTENANCE INSTALLED REPAIR IAW DAC TELEX SVC-MSP-1072/KJL DATED 12-DEC-1996.SDR 97ZZZX1640Spar · corrodedINTERGRANULAR CORROSION FOUND ON LEFT WING REAR SPAR WHILE INSPECTING AS REQUIRED BY AD 96-24-17. REPLACED WITH NEW SPAR.SDR AU970265Spar · corroded(AUS) CENTRE SECTION REAR CARRY THROUGH SPAR CORRODED - SEE MDR 97/0252 FOR ADDITIONAL INFORMATIONSDR AU970252Spar · corroded(AUS) LH WING FRONT MAIN SPAR CORRODED - SEE MDR 97/0255 TO MDR 97/0265 FOR ADDITIONAL DEFECTS REPORTED UNDER THE SAME MDR NUMBERSDR AU970249Spar · cracked(AUS) WING REAR SPAR CRACKED IN RADIUS OF WING ATTACHMENT WEBSDR CA970319008Spar · cracked(CAN) FOUND REAR WING SPAR CRACKED AT TOP OUTER STRUT ATTACH PLATE. THE CRACK WAS ONLY VISIBLE WHEN A LOAD WAS APPLIED TO SPAR TIP.SDR DLL15970449Rear Spar · crackedDURING ACCOMPLISHMENT OF E.O. 7-59089-3, SEVERAL HOLES IN THE LT WING REAR SPAR WERE FOUND CRACKED IN THE UPPER SPAR CAP BETWEEN IWS 293.58 AND IWS 346.109. THE HOLES ARE COMMON TO THE UPPER WING SKIN AND SPAR CAP AND TO THE SPAR WEB AND SPAR CAP. THE SUBJECSDR DLL15970414Spar Cap · crackedDURING ACCOMPLISHEMENT OF EO 7-59089-3, SEVERAL HOLES IN THE RT WING REAR SPAR WERE FOUND CRACKED IN THE UPPER SPAR CAP BETWEEN IWS 293.58 AND IWS 346.109. THE HOLES ARE COMMON TO THE UPPER WING SKIN AND SPAR CAP AND TO THE SPAR WEB AND SPAR CAP. THE DAMAGE SDR 97ZZZX1737Spar Cap · corrodedDURING C-CHECK INSPECTION, LEVEL 2 CORROSION WAS NOTED ON LOWER FWD SPAR CAP AT RT WING STA 560 AT ATTACH POINT FOR LOWER LEADING EDGE ACCESS PANEL. APPARENTLY CAUSED BY INADEQUATE PREVENTIVE TREATMENT.SDR 97ZZZX1584Spar · corrodedAIRCRAFT WAS BEING DISASSEMBLED FOR PAINTING. UPON REMOVAL OF LEFT WING ROOT, AN AREA OF INTERGRANULAR CORROSION WAS FOUND ON THE TOP SURFACE OF THE INBOARD SPAR. EXFOLIATION HAD PENETRATED TO A DEPTH OF .0625 INCH OVER AN AREA APPROXIMATELY 3 INCHES BY 1.50SDR VJ970136Rear Spar · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE FOLLOWING WAS FOUND .125 INCH CRACK ON LOWER FLANGE OF REAR SPAR AT STATION 58 STRINGER 11, RIGHT WING. FABRICATED REPAIR 'L' ANGLE PER EO 97-461 PAGE 6 OF 7075 T6 .125 6 INCHES BY 12 INCHES. D
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