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 GLBA1123GSpar · damagedDURING ROUTINE SCHEDULED MX SIX FASTNER HOLES WERE FOUND DAMAGED AT THE LT INBD FLAP TRACK AREA. WS 46.500. MX REPAIRED THE AFFECTED AREA IAW EO 09-1900-57-007. RII INSPECTIONS COMPLIED WITH IAW EO 09-1900-57-007. MATERIALS UTILIZED ARE INCLUDED IN THE EO INSDR FDEA200911184005Spar · crackedRT WING T/E EDGE FALSE SPAR CHORD ANGLE CRACKED WBL 118. REPAIRED RT WING T/E FALSE SPAR CHORD ANGLE WBL 118 IAW DWG SR27-57-038 REV C, REMOVED DOUBLER, CUT OUT WEB AND CRACKED ANGLE, FABRICATED REPAIR ANGLES, STRAP, NEW CHORD ANGLE, WEB SECTION AND DOUBLESDR 2010FA0000161Spar · corrodedCORROSION, VISUALLY APPEARED TO BE INTERGRANULAR TURNING TO EXFOLIATION, FOUND EXPLODING OUT OF THE LOWER PORTION OF THE VERTICAL SURFACE OF THE RT WING SPAR WEB, PN 86152-001, AT APPROX WING STA 56.0. THE AREA IS JUST OTBD OF THE LANDING GEAR TRUSS BRACKET, PSDR GLBA20091111FSpar · damagedDURING ROUTINE SCHEDULED MX, DISCOVERED 2 LOCK FASTENER HOLES MISDRILLED (HOLES ARE STEPPED) AT/ON THE LT WING, AFT WING SPAR ON THE FWD SIDE OF THE SPAR AT WS 127.288 AND 129.588. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED THE REQUIRED RII INSPECTSDR GLBA20091110GSpar · damagedDURING ROUTINE SCHEDULED MAINTENANCE AFTER REMOVAL OF A FASTENER, PART OF AN EXISTING RIVET WAS IN THE HOLE UPON REMOVING THE RIVET THE DIAMETER OF THE HOLE WAS FOUND TO BE APPROXIMATELY .230" ACROSS AT LEFT HAND WING SPAR W.S. 114.250. MAINTENANCE REPAIRED SDR GLBA20091110FSpar · damagedDURING ROUTINE SCHEDULED MX, A STEPPED LOCK FASTENER WAS FOUND IN THE LT WING SPAR AT WS 124.588. DEPTH OF THE STEP IS APPROX .150" DEEP. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED THE REQUIRED RII INSPECTIONS I.A.W. E.O. 09-1900-57-006. MATERIALS SDR HYIA781EA LFTWGSpar Cap · corrodedPRIOR TO REPAINTING OF ACFT, STRIPPING PROCESS REVEALED SIGNIFICANT INTERGRANNULAR CORROSION ON THE LT WING OTBD AFT SPAR, LWR CAP. MX CURRENTLY EVALUATING POSSIBLE REPAIR OR REPLACEMENT OF LT AFT OTBD SPAR, LWR CAP.SDR HNAA2010022400038Spar · crackedLT WING FRONT SPAR ANGLE FOUND CRACKED ON INBD SIDE OF NACELLE ( STA YW139). R & R ANGLE IAW SRM 51-40-00.SDR GUUA94757110209ASpar · corrodedREPORT: DURING SCHEDULED X-RAY INSPECTION DISCOVERED CORROSION INDICATIONS ON FORWARD LOWER SPAR ANGLE AT WS 125.5. BLENDED OUT CORROSION AND INSTALLED REINFORCEMENT STRAP.SDR WRLA20091101280Former · crackedCRACK - FORMER (P/N:ARB1164-5) CRACKED ABOUT .75 INCH LEFT WING FRONT SPAR LWR CHORD XOS 993 QTY = 1. REPAIRED THE CRACK FORMER IAW MD11 SRM 57-00-00 REV 41.SDR GUUA94157103109BSpar · corrodedDURING SCHEDULED X-RAY INSP OF LT WING COLLECTOR TANK FOUND SEVERAL SPOTS OF CORROSION ON LWR MAIN SPAR. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR STRAP.SDR SIMA200930601Sealant · damagedON FLIGHT 3695 THE CREW REPORTED THAT ON APPROACH, HAD A FUEL SMELL IN THE COCKPIT. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESEALED BOLT AT FRONT SPAR JUST INBOARD OF RIB 1 LEFT CENTER TANK. REFERENCE EMB 145 SRM 51-20-01. LEAK CHECK GOOD IAW AMM 28-11-00.SDR FDEA200910303727Spar Cap · damagedLT WING - REAR SPAR LWR CAP FASTENER HOLE AT XORS 1070 FOUND ELONGATED. REPAIR CARRIED OUT AS PER E.A. 1-5710-132260, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 108.SDR SWAA096794Spar · crackedDURING SCHEDULED 20Y CHECK, FOUND LT WING UPPER SPAR CHORD CRACKED. REPAIRED CHORD PER ER.SDR SWIA200923165Spar Cap · crackedLEFT WING FORWARD UPPER AUX SPAR CAP CRACKED. (C-CHECK) REPAIRED PER ETD.SDR FDEA200910243657Spar Cap · corrodedLEFT WING - REAR SPAR UPPER CAP SURFACE FOUND CORROSIONS AT XORS 1040.35. REPAIR CARRIED OUT AS PER E.A.1-5710-132251, THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 108.SDR CA091026001Spar · cracked(CAN) FOUND ON INSPECTION THAT THE FRONT SPAR OH THE RIGHT WING WAS CRACKED ON BOTH SIDES OF THE FIRST FLANGED LIGHTENING HOLE AT STATION 44.12, JUST OUTBOARD OF THE FUEL TANK ON THE RIGHT HAND WING. CRACK ON BOTH SIDES OF THE LIGHTENING HOLE IS 1/4" IN LENGTHSDR MZZA2009110400110Spar · corrodedLEFT WING FRONT SPAR HAS A SPOT OF IG CORROSION BETWEEN NR 1 AND NR 2 L/E FLAP WELL, APPROX LOCATION IFSS 150. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REPAIRED AREA PER EC/RA 5720-02079, DIP INITIATED TO PERFORM PERMANENT REPAIR WITHIN 12 MONTHS. PSDR GUUA94257102009ASpar · corrodedDURING SCHEDULED RT WING X-RAY INSP DISCOVERED INDICATION OF CORROSION ON FWD LWR SPAR ANGLE AT WS 126.5. BLENDED OUT CORROSION AND INSTALLED REINFORCEMENT STRAP.SDR HYIA818ANRTWSpar Cap · crackedDURING SCHEDULED MX VISIT, MX FOUND POSSIBLE CRACK ON RT WING FWD SPAR, UPPER CAP. CRACK CONFIRMED BY EDDY CURRENT INSP. SPAR CAP REPLACEMENT IN PROGRESS.SDR AALA20091013TUL06Spar · damagedRIGHT WHEEL LEADING-EDGE SPAR HAS DAMAGE AT 102 INCHES FROM INBOARD END. INSTALLED DOUBLER REPAIR PER AARD 51-70-00-3.SDR 2009FA0000938Spar · corrodedDURING THE ROUTINE INSP ON ACFT, CORROSION WAS FOUND ON THE SPAR AT THE MID WING SECTION OF THE ACFT BETWEEN THE SPAR DOUBLERS (PN AD-AC-0191-1 LT OTBD DOUBLER AND 1A RT OTBD DOUBLER, AT APPROXIMATE WING STA 53.0-63.0, THE 10 INCH OVERLAPPED SECTION ON BOTH LTSDR GUUA94057093009CSpar · corrodedDURING SCHEDULED LEFT WING X-RAY INSPECTION DISCOVERED SMALL CORROSION SPOTS AREA 1 WING SPAR. BLENDED OUT CORROSION AND INSTALLED REPAIR STRAP.SDR GUUA94057093009ASpar · corrodedDURING SCHEDULED RIGHT WING X-RAY INSPECTION DISCOVERED SMALL CORROSION SPOTS AREA 1 WING SPAR. BLENDED OUT CORROSION AND INSTALLED REPAIR STRAP.SDR SWAA096320Spar · crackedDURING SCHEDULED 10Y CHECK, FOUND CENTER WING SECTION REAR SPAR WEB CRACKED AT BS 663, RBL 34. REPAIRED WEB PER AAR EA.SDR SWAA096319Spar · crackedDURING SCHEDULED 10Y CHECK, FOUND CENTER WING SECTION REAR SPAR WEB CRACKED AT BS 663, LBL 41. REPAIRED WEB PER AAR EA.SDR IPXA09657534Angle · crackedINSPECTION TYPE:C LT WING - L/E LES 160 UPPER AREA FRONT SPAR ANGLE FOUND CRACKED. CRACK LENGTH 0.75 INCH. LT WING L/E LES 160 UPPER AREA FRONT SPAR ATTACH ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.SDR IPXA09657382Fitting · crackedINSPECTION TYPE:C LT WING L/E LES 548 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR CLIP FOUND CRACK. CRACK LENGTH 0.375 INCH. LT WING L/E LES 548 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-4SDR 2009FA0000764Spar · crackedDURING THE ANNUAL INSP, A CRACK WAS DISCOVERED IN THE REAR SPAR OF THE LT WING. THE CRACK WAS IN THE CTR OF THE SPAR RUNNING LENGTH WISE LT AND RT OF WHERE THE WING STRUT ATTACHES. (K)SDR IPXA09657390Angle · crackedINSPECTION TYPE:C RT WING LT LES 155 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR ANGLE FOUND CRACK. CRACK LENGTH 1 INCH. RT WING - LT LES 155 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR ANGLE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-SDR IPXA09657381Angle · crackedINSPECTION TYPE:C LT WING L/E LES 675 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR ANGLE FOUND CRACK. CRACK LENGTH 0.5 INCH. LT WING L/E LES 675 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR ANGLE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-4SDR KCSA091098Spar · corrodedLEFT WING FRONT SPAR WEB CORRODED WS 1379.SDR IXXA09SMN087SSpar Cap · corrodedDURING ROUTINE C-CHECK INSP, FOUND RUDDER RT SIDE FRONT SPAR CAP CORRODED AT STA ZR 323.000. REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED DAMAGED SPAR CAP. FABRICATED NEW SPAR CAP. CLEANED, TREATED, AND PRIMED AREA AND NEW SPAR CAP. INSTALLED NEW SPAR CAP SDR I5PA20090802Spar · corrodedDURING 5C CHECK AND INSPECTION, CORROSION WAS FOUND ON LT WING REAR SPAR LWR SKIN AT WS706 DIMENSION AREA 1.3 INCH X 1.7 INCH. AFTER CORROSION BLENDOUT FOUND MAX BLDOUT DEPT IS BEYOND LIMITATIONS. NO REINFORCEMENT REQUIRED, REMOVE ALL FASTENERS BLEND SMOOSDR I5PA20090801Spar · corrodedDURING 5C-CHECK AND INPS CORROSION WAS FOUND ON RT AND LT WING FRONT SPAR CHORD PLATE LWR SURFACE. AFTER BLEND OUT THE MAX LOSS OF MATERIAL THICKNESS WAS BEYOND THE ALLOWABLE LIMIT IAW SRM. FABRICATED AN INTERNAL REPAIR STRAP IAW EI-727-090701 HFEC ACCESSED SDR C8GA20090219Spar · corrodedWHILE IN HEAVY MX INSP, IT WAS NOTED THAT RT WING FRONT SPAR WEB IS CORRODED. REMOVED DAMAGED AREA, FABRICATED REPAIR DOUBLER FROM 2024 T3 DIM 10 INCHES X 12 INCHES .160 INCH. INSTALLED DOUBLER REPAIR, NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVISDR GLBA20090731GSpar Cap · crackedMAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE A CRACK ON THE RT WING AT RBL 114.250, LOWER SPAR CAP, AFT SIDE OF SPAR WHILE PERFORMING SB 57-3816. CRACK IS APPROXIMATELY .040" DEEP AND BASICALLY RADITES OUT FROM A FASTENER HOLE. MX REPAIRED AFFECTED ARSDR FDEA200907312851Spar Cap · corrodedRT WING - REAR SPAR UPPER CAP UPPER SURFACE FOUND CORROSIONS AT XORS 1043. REPAIRED AS PER EA 1-5710-132171. CLASSIFIED MINOR AS PER GMM 6-2-100 REV 107.SDR FDEA200907312850Spar Cap · corrodedRT WING - REAR SPAR UPPER CAP UPPER SURFACE FOUND CORROSION AT XORS 1040. REPAIRED AS PER EA 1-5710-132171. CLASSIFIED MINOR AS PER GMM 6-2-100 REV. 107.SDR EE4Y090198Spar · corrodedLT WING FRONT SPAR LOWER CHORD CORRODED.SDR USAA2009072791915Spar · crackedCLT - Q-4 - MAJOR REPAIR - CRACK ON LEFT WING REAR SPAR UPPER CHORD AT RSS224.14. REPAIRED LEFT WING REAR SPAR UPPER CHORD AT RSS224.14 IAW US AIRWAYS EA 101254.SDR C2XA09TY180Spar Cap · corrodedTYS - SURFACE CORROSION WAS FOUND ON THE LEFT WING SPAR ONE I/B CAP. MAINTENANCE REMOVED THE LITE CORROSION IAW EMB 135/145 SRM 57-20-01. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR SWIA200922685Spar Cap · crackedRT WING FWD AUX SPAR CAP JUST I/B OF ENGINE NACELLE HAS A CRACK THROUGH A HI-LOK. (C-CHECK) REPAIRED RT SPAR CAP JUST I/B OF NACELLE, IAW IC2009 -120/05978 AND IAW SRM 120 51-00-00.SDR SWIA200922313Spar Cap · crackedRIGHT WING FORWARD AUX SPAR CAP CRACKED. (C CHECK) REPAIRED PER SRM.SDR IPXA09656856Attach Fitting · crackedINSPECTION TYPE:C LT WING L/E LES 622 FRONT SPAR ATT CLIP FOUND CRACKED, CRACK LENGTH 1.125 INCH. LT WING L/E LES 622 FRONT SPAR ATT CLIP REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 44.SDR MZZA2009071700096Spar · corrodedLT WING L/ EDGE FRONT SPAR LOWER STRAP SING OF CORROSION AT OFSS 417,SS182 REPAIR CARRIED OUT IAW EC/RA 5730-02562.REFER TO ATTACHED FORM 44.0008 FOR SEQUENCE OF OPERATION. REFER TO L/P 0976283 FOR NDT INSPECTION. REFER TO L/P 7913648 DOR DIP INITIATED. DIPSDR FDEA200907072520Spar · crackedLT WING T/E FALSE SPAR, INBD END REPAIR DOUBLER IS CRACKED. WBL 118 REMOVED NR 7 SPOILER FITTING AND SUPPORT IAW SRM 51-30-2. REMOVED PREVIOUS DOUBLER, TRIMMED OUT WEB AND REMOVED PREVIOUS CHORD REPAIR IAW DWG SR 27-57-038 REV C. FABRICATED NEW WEB FROM 7SDR AALA20090703TUL13Fitting · crackedFORWARD SPAR LEFT SIDE FITTING CRACKED. INSTALLED NEW FITTING PER SRM 51-30-01.SDR FDEA200906292384Spar Cap · corrodedRT WING T/E REAR SPAR UPPER CAP AREA AROUND XORS 1042 FOUND WITH CORROSION. REPAIR CARRIED OUT AS PER E.A. 1-5710-132655, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 107.SDR USAA2009071691852Spar · crackedSAL - Q-3 - MAJOR REPAIR - NR 6211524 - CRACK IN LEFT HAND FUEL TANK REAR SPAR LOWER CHORD. REPAIRED LEFT HAND FUEL TANK REAR SPAR LOWER CHORD IAW US AIRWAYS EA 132523.
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