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 FDEA200902190593Spar Cap · crackedFUEL LEAK LT WING LOWER REAR SPAR CAP AT WS XORS 346, INDICATION OF CRACK AT THE POINT OF LEAK. REAR SPAR REPAIRED AS PER E.A. 8-5710-126158. SEQ.#924.SDR IPXA09855973Frame · crackedINSPECTION TYPE:SV CRACKED FORMER AT RT WING LE STA XFS 303 BOTTOM AFT. FABRICATED NEW FORMER AND INSTALLED PER DAC DWG 5769530 REV F, AND DC8 SRM 51-1-20D REV 78.SDR MTNA0903001Spar · corrodedCORROSION ON LEFT WING REAR SPAR BETWEEN RIBS 28 AND RIBS 29. BLENDED OUT IAW ATR STRUCTURAL REPAIR INSTRUCTION DO/TS/-721/09-11337.SDR FDEA200902160552Spar Cap · corrodedRIGHT WING UPPER SURFACE TRAILING EDGE REAR SPAR AREA APPROXIMATELY XORS 981 FOUND CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II AND FOUND OUT OF LIMIT AS PER SRM 57-10-00 FIGURE 17 VOLUME I. REPAIR CARRIED OUT ON REWORK AREA AS PER EA 1-5710-12SDR FDEA200902160551Spar Cap · corrodedRIGHT WING UPPER SURFACE REAR SPAR CAP AT APPROXIMATELY XORS 1042 FOUND CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II AND FOUND OUT OF LIMIT AS PER SRM 57-10-00 FIGURE 17 VOLUME I. REPAIR CARRIED OUT ON REWORK AREA AS PER EA NR 1-5710-128576. SDR GUUA93657021309BSpar · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED POSSIBLE AREAS OF CORROSION IN LT WING FUEL COLLECTOR TANK ON MAIN SPAR. REMOVED CORROSION ON LEFT MAIN SPAR LOWER CAP AND INSTALLED INTERNAL AND EXTERNAL DOUBLERS.SDR UPS09654804Stiffener · crackedINSPECTION TYPE:C RT WING - LES 662 FRONT SPAR STIFFENER FOUND CRACK. CRACK 0.375 INCH LENGTH. RT WING - LES 662 FRONT SPAR STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.SDR UPS09654558Support Bracket · crackedINSPECTION TYPE:C RT WING- L/E LES 548 L/E SUPPORT UPPER FWD FRONT SPAR SUPPORT BRACKET FOUND CRACKED (1 INCH LENGTH). RT WING - L/E LES 548 L/E SUPPORT UPPER FWD FRONT SPAR SUPPORT BRACKET REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02.SDR GUUA94557012309ASpar · corrodedDURING SCHEDULED INSPECTION DISCOVERED BIO-CORROSION ON LEFT WING MAIN SPAR LOWER AFT SPAR FLANGE AT WS 117. BLENDED OUT ALL CORROSION FILLED AREA OF REPAIR AND INSTALLED REINFORCEMENT DOUBLER STRAP.SDR UPS09M54495Spar · misrepairedINSPECTION TYPE:C RT WING - REF EFN 25120081005, LOWER SURFACE F/SPAR AT XORS 810-817, FASTENER TYPE & DOUBLER LOCATION DOES NOT TALLY WITH SRM 57-10-00 FIG 45. EXISTING DOUBLER REMOVED AT AFFECTED AREA. HFEC C/O IAW DAC NDT SPM REV 13 PART 06-10-01.001 ON ESDR FDEA200901180230Spar · crackedCRACK ANGLE FALSE SPAR AT NR 7 SPOILER ACTUATOR CUT-OUT. CRACKED ANGLE OUT OF LIMITS IAW SRM 57-10-1 FIG 1. REMOVED SUPPORT FITTING & VERTICAL STRUCTURE IAW DWG SR27-57-038 & SRM 51-30-2. TRIMMED AFT WEB AT CUT LINE IAW DWG SR27-57-038 REV C. REMOVED CRACKSDR MTNA0901002Spar · corrodedREPAIRED CORROSION ON THE LEFT WING REAR SPAR UPPER EXTRUSION VERTICAL FLANGE BETWEEN RIBS 24-27 AS FOLLOWS. BLENDED OUT CORROSION IN ACCORDANCE WITH ATR STRUCTURAL REPAIR INSTRUCTIONS DO/TS-107/09-11167 ISSUE A. THE DEVIATIONS WERE THAT HOLES WERE OVERSIZEDSDR DL76G090039Spar · cutWHILE CUTTING THE LOWER WING SKIN FOR THE WINGLET MODIFICATION, THE FRONT SPAR LOWER CHORD AFT FLANGE WAS ALSO CUT AT 0 FSS 1035. THE DAMAGE WAS TRIMMED OUT AND INSTALLED A TITANIUM STRAP.SDR SWIA200921278Spar Cap · crackedLEFT WING INBOARD AUX SPAR CAP CRACKED (C CHECK). REPAIRED PER EMB DIRECTIVE.SDR FDEA200901050041Spar · crackedRT WING T/E, FALSE SPAR INBD ATTACHMENT HAS LOOSE HARDWARE AND SEPARATION BETWEEN PARTS, WBL 118 FOUND CRACKED. REPAIR ACCOMPLISHED PER DRAWING SR27-57-038 REV "C". STD. REWORK DRAWING INBD BEAM CRACK REPAIR.SDR UPS09654317Bracket · crackedINSPECTION TYPE:C RT WING LES 675 L/E SUPPORT AFT UPPER FRONT SPAR BRACKET FOUND CRACKED. RT WING LES 675 L/E SUPPORT AFT UPPER FRONT SPAR BRACKET REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.SDR SWIA200821276Spar Cap · crackedLEFT WING INBOARD UPPER AUXILIARY SPAR CAP IS CRACKED (C CHECK). REPAIRED PER EMB DIRECTIVE.SDR DL757081780Spar · damagedFWD SPAR UPPER CHORD OVER SIZED HOLES FROM FACTORY. CLEANED HOLE NDT, INSTALLED OVERSIZED FASTENERS.SDR DLM88081752Spar · crackedFOUND CRACK IN REAR SPAR LOWER CHORD AT O/B FLAP, I/B HINGE. CUT OUT DAMAGED SECTION OF CHORD AND SPLICED IN NEW SECTION. REPAIRED IAW ER/A 471595-14.SDR DU4R2008284Spar · corrodedDURING SCHEDULED INSPECTION, FOUND CORROSION ON WEB, LT WING REAR SPAR, ABOVE LT AFT BOOST PUMP WS 188SDR DU4R2008279Spar · corrodedDURING SCHEDULED INSPECTION, FOUND CORROSION ON LT WING REAR SPAR BELOW LEFT AFT BOOST PUMP RSS 185.SDR FDEA200812125128Spar · crackedCRACKED CHORD FALSE SPAR UNDER NR 7 SPOILER FITTING. REMOVED LOWER SECTION OF CHORD IAW DRWG SR27-57-038 REV C AND FABRICATED NEW LOWER SECTION, 2 REPAIR ANGLES, 1 REPAIR STRAP, AND WEB IAW DWG SR27-57-038 REV C. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-1SDR FDEA200812125127Spar · crackedFALSE SPAR CHORD CRACKED UNDER NR 8 SPOILER . TRIMMED INBRD WEB SECTION IAW DRAWING SR 27-57-038 REV C. TRIMMED LOWER STRUCTURE IAW DRAWING SR 27-57-038. LOCATED, DRILLED, DEBURRED LOWER ANGLE IAW 51-30-5 & DWG SR 27-57-038 REV C. FABRICATED 2 EA ANGLES ASDR 2008FA0000922Spar · crackedDURING ROUTINE INSP, CRACKS WERE OBSERVED IN THE LT AUXILARY SPAR. THE MAIN GEAR IS ATTACHED AT THE OTBD END. THE CRACKS WERE AT THE 11,2,5 AND 7 O`CLOCK POSITIONS OF THE HOLE WHICH THE WIRE BUNDLE PASSES THROUGH, AND WERE OF VARYING LENGTH. CRACKS WERE ALSSDR 2008FA0000921Spar · crackedDURING ROUTINE INSP, CRACKS WERE OBSERVED IN THE LT AUXILARY SPAR. THE MAIN GEAR IS ATTACHED AT THE OTBD END. THE CRACKS WERE AT THE 11, 2, 5 AND 7 O`CLOCK POSITIONS OF THE HOLE WHICH THE WIRE BUNDLE PASSES THROUGH, AND WERE OF VARYING LENGTH. CRACKS WERE ASDR 2008FA0000919Spar · crackedDURING ROUTINE INSP, CRACKS WERE OBSERVED IN THE LT AUXILARY SPAR. THE MAIN GEAR IS ATTACHED AT THE OTBD END. THE CRACKS WERE AT THE 11, 2, 5 AND 7 O`CLOCK POSITIONS OF THE HOLE WHICH THE WIRE BUNDLE PASSES THROUGH, AND WERE OF VARYING LENGTH WITH THE 2 LOWESDR CA081209005Spar Cap · cracked(CAN) WHILE PERFORMING AD 92-26R1 NO DEFECTS WERE FOUND DURING ULTRASONIC INSPECTION OF REQUIRED INSPECTION AREA. DUE TO PREVIOUS CONCERNS (3) WITH FINDING CRACKS OUTSIDE OF INSPECTION AREA FURTHER INVESTIGATION WAS PERFORMED. CRACKS WERE FOUND IN LOWER SPARSDR SWAA086830Fitting · crackedDURING SCHEDULED 14Y CHECK, FOUND RT WING VERTICAL WEB CRACKED AT FWD SPAR FITTING. REMOVED AND REPLACED FITTING PER SRM.SDR KCSA081610Spar · corrodedCORROSION ON L/E SPAR WEB UNDER SUPPORT RIB AFT [VERTICLE] CORD AT APPROX WS 1574.SDR KCSA081609Spar · corrodedCORROSION ON L/E SPAR WEB UNDER SPAR STIFFENER AT APPROX WS STA 1589.SDR FDEA200812025045Angle · gougedLT WING AFT OF REAR FALSE SPAR APPROX RIB 6A AREA HAS VERTICAL WEB GOUGED AND DOUBLE DRILLED HOLES. REMOVED LOWER SKIN PANEL AND DAMAGED ANGLE REF SRM 51-40-21 PARA 6 AND 13. FABRICATED NEW ANGLE REF SRM 57-51-11 AND DWG A57244531. ALODINED REF SRM 51-21-1SDR FDEA200811264982Fitting · crackedLEFT WING HOLE " D " OF EO 6-5710-7-5005 P1 SHOWS A CRACK INDICATION APPROX 1/16 LONG. COMPLIED WITH FEDEX EA 6-5710-123673, WINGS - AD 99-16-01 - EO 6-5710-7-5005 - LT WING REAR SPAR, MLG FWD PICK-UP FITTING BOLT HOLE "D".SDR DU4R2008264Repair · crackedDURING SCHEDULED INSPECTION, FOUND A TEMPORARY REPAIR AT LBL 33 AND LBL 41 CRACKED AND REQUIRING REPAIR.SDR SWAA086340Spar · crackedDURING SCHEDULED 20Y CHECK, FOUND RT WING REAR SPAR WEB CRACKED AT FWD MLG BEAM FITTING. REPAIRED WEB PER PAE ER.SDR FDEA200811124865Spar Cap · crackedAPPROX 2.75 INCH CRACK EXISTS IN RT WING LOWER SPAR CAP (PSE 57.10.008) AT XORS = 411. CRACK RUNS FROM AFT EDGE OF SPAR CAP AFT TANG, FWD APPROX 1.625 INCH TO RADIUS, THEN UPWARDS AND INBOARD APPROX 1.125 INCH AND TERMINATES AT VERTICAL LEG FASTENER AT APPROXSDR CALA0801072Spar · crackedLEFT WING LEADING EDGE FRONT SPAR WEB FOUND CRACKED AT OFSS 1027 APPROXIMATELY 1 X 1 INCH L SHAPE. LEFT WING FRONT SPAR WEB AT OFSS 1027 REPAIRED PER ECRA 5710-02152.SDR 08FDEA04865Spar Cap · crackedAPPROX 2.75 INCH CRACK EXISTS IN RT WING LOWER SPAR CAP (PSE 57.10.008 ) AT XORS = 411. CRACK RUNS FROM AFT EDGE OF SPAR CAP AFT TANG, FWD APPROX 1.625 INCH TO RADIUS, THEN UPWARDS AND INBOARD APPROX 1.125 INCH AND TERMINATES AT VERTICAL LEG FASTENER AT APPROSDR SWAA086102Spar · crackedDURING SCHEDULED 20Y CHECK, FOUND LT WING UPPER T/E SPAR CHORD CRACKED AT MLG BEAM TO SPAR FITTING. REPAIRED CHORD PER PAE ER.SDR 08FDEA04660Spar Cap · damagedCOMPLY WITH LT WING REAR SPAR LOWER CAP SPLICE-LIFE LIMITED REPAIR, STA XORS 395 TO 446 PER EA 8-5710-118517 REV NR POS, SEQ NR 000007. COMPLIED WITH E.A. 8-5710-118917 WING-REAR SPAR LOWER CAP SPLICE-LIFE LIMITED REPAIR.SDR 2008FA0000724Spar Cap · crackedDURING FURTHER EVALUATION FOLLOWING PREVIOUSLY REPORTED DAMAGE A TERTIARY FRACTURE WAS FOUND ON THE FORWARD SPAR CAP, HORIZONTAL FLANGE, WING STA 143.5. THE FRACTURE WAS VISUALLY IDENTIFIED AND CONFIRMED WITH EDDY CURRENT. AN INTERNAL VISUAL EXAMINATION IDENSDR 2008FA0000723Spar Cap · crackedDURING FURTHER EVALUATION FOLLOWING PREVIOUSLY REPORTED DAMAGE A SECOND CRACK WAS FOUND ON THE FORWARD LOWER CAP AT BUTTLINE 56R. THE CRACK WAS VISUALLY IDENTIFIED AND CONFIRMED WITH EDDY-CURRENT SURFACE SCAN.SDR IXXA08SMN200SSpar Cap · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING UPPER REAR SPAR CAP VERTICAL FLANGE CRACKED AT STATION XRS 554.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED STOP HOLE. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND AFTER DRILSDR 2008FA0000704Spar Cap · fracturedDURING INSPECTION TO DETERMINE THE SOURCE OF A FUEL LEAK A FRACTURE WAS FOUND IN THE LOWER FORWARD RIGHT SPAR CAP AT WING STA 75 EMANATING FROM NUT PLATE FASTENER HOLE ON FORWARD FLANGE TO THE EDGE OF FLANGE MEMBER WITH SLIGHT ENCROACHMENT AFT FROM SAME HOLE, SDR HNAA2009012500020Spar · crackedSUPECTED CRACK ON LT WING FRONT SPAR AT INBD NACELLE ATTACHMENT TOP CORNER. R&R ANGLE IAW STRUCTURAL REPAIR MANUAL 51-40-00.SDR KCSA081535Spar · chafedNR 1 PYLON MID SPAR WEB STIFFENER HAS CHAFF DAMAGE AT NAC. STA-210 R/H TOP.SDR UPS08653687Spar · crackedINSPECTION TYPE:N/A RT WING ILES677 FRONT SPAR D-NOSE I/B FOUND CRACK AS MARKED CRACK LENGTH .75 INCH. RT WING ILES677 FRONT SPAR D-NOSE BEAM WEB REPAIRED AS PER SRM 57-41-13-2R FIG 201.SDR 08FDEA04304Spar · crackedCRACK ON WING CENTER SECTION REAR SPAR WEB STA 870 LBL 13 TO 16.SDR 08FDEA04286Frame · crackedCENTER FUSELAGE ZONE 12 REINFORCE THE UPPER FRAME BASE TO ARCH STRUCTURE AT FRAME 45 FASTENER HOLE CRACKED ON FR4AME FOOT, RIGHT SIDE. COMPLIED WITH E.A 6-5310-123911.SDR 08FDEA04283Frame · crackedFUSELAGE MAIN FRAME FRAME FOOT 45 RIGHT SIDE ,INSTALL 1ONE CADMIUM PLATED SHOULDERED BUSH MADE OF STAINLESS STEEL 17-4PH REQUESTED BY E.A 6-5310-123911. FABED BUSHING ON MAE TRAVELER T8/761893, INSTALLED PER E.A 6-5310-123911SDR 08FDEA04282Frame · crackedCENTER FUSELAGE ZONE 20 REINFORCE THE UPPER FRAME BASE TO ARCH JUNCTION AT FRAME 44 FASTENER HOLE CRACKED ON FRAME FOOT FITTING. COMPLIED WITH E.A 6-5310-123911.
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