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 AWXA200601129Spar · corrodedCORROSION AROUND HOLE NR 77 OF REAR SPAR LEFT WING. CORROSION AROUND HOLE NR 77 OF REAR SPAR LEFT WING WAS REMOVED IAW PART A OF AWA ER NR 26 - 5721 - 06181 - ES2 MONITORING IAW ER 26-5721-06181-ES2 ITEM 1 SHEET 4 AT 11.SDR AWXA200601123Spar · corrodedFOUND CORROSION AROUND HOLE NR 54 OF REAR SPAR LEFT WING. CORROSION AROUND HOLE NR 54 OF REAR SPAR LEFT WING WAS REMOVED ACCORDING TO PART AOF ER NR 26-5221-06181-ES2.SDR AWXA200601122Spar · corrodedFOUND CORROSION AROUND HOLE NR 52 OF REAR SPAR LEFT WING. CORROSION AROUND HOLE NR 52 OF REAR SPAR LEFT WING WAS REMOVED IAW ER 26-5921-ES2 PART A MONITORING IAW ER 26 - 5921 - 06181 - ES2 ITEM 1 SHEET 4 AT 11.SDR AWXA200601121Spar · corrodedFOUND CORROSION AROUND HOLE NR 75 OF REAR SPAR LEFT WING. CORROSION AROUND HOLE NR 75 OF REAR SPAR LEFT WING WAS REMOVED IAW PART A OF AWA ER NR 26 - 5421 - 06181 - ES2.SDR AWXA200601118Spar · corrodedCORROSION WAS FOUND AROUND HOLE NR 57 REAR SPAR RIGHT WING. CORROSION AROUND HOLE NR 57 REAR SPAR RIGHT WING WAS REMOVED IAW PART A OF AWA ER NR 26 - 5721 - 06181 - E82.SDR AWXA200601117Spar · corrodedFOUND CORROSION AROUND THE HOLE NR 62 OF REAR SPAR LEFT WING. CORROSION AROUND THE HOLE NR 62 OF REAR SPAR LEFT WING WAS REMOVED IAW PART A AWA ER 26 - 5721 - 06181 - E82 MON, TORING IAW ER 26 - 5721 - 06181 - E82 ITEM 1 SHEET 4.SDR 2006FA0000793Spar · corrodedTHE DEFECT IS SEVERE CORROSION IN SPAR TUBE LT SIDE UPPER AT WING STA 90. PROBABLE CAUSE IS EXPOSURE TO MOISTURE OVER AN EXTENDED PERIORD OF TIMEM. RECOMMENDATION TO PREVENT RECURRENCE WOULD BE TO SEAL AND FILL WITH LIN SEED OIL. FURTHER RECOMMENDATION WOULSDR 06FDEA2420Spar Cap · corrodedSNRM N00579: LEFT HAND WING REAR SPAR UPPER CAP AT STA XORS 1042 FOUND WITH CORROSION. COMPLIED WITH FEDEX E.A. 1-5710-100689.SDR 06FDEA2419Spar Cap · corrodedSNRM N00394: RIGHT HAND WING REAR SPAR UPPER CAP BENEATH THE UPPER CLOSE OUT PANEL BETWEEN STA XORS 1042 TO XORS 981 FOUND WITH CORROSION. COMPLIED WITH FEDEX E.A. 1-5710-100690.SDR 06FDEA2418Spar Cap · corrodedSNRM N00385: LEFT HAND WING REAR SPAR UPPER SURFACE OF THE SPAR CAP AT STA 970 TO 980 FOUND WITH CORROSION. COMPLIED WITH FEDEX E.A. 1-5710-100688.SDR 1060530036RSpar Cap · corrodedRT MAIN SPAR CAP BIO-CORROSION CLEANED AND TREATED AND REPAIRED IAW RAYTHEON FR-CO-01358 REV 1.SDR 1060530036LSpar Cap · corrodedLT MAIN SPAR CAP BIO-CORROSION. CLEANED AND TREATED AND REPAIRED IAW WITH RAYTHEON FR-CO-01359 REV 1.SDR EIA2006201Spar · corrodedLEFT WING LOWER FRONT SPAR WEB FOUND CORRODED BETWEEN ILES 901-1080. REMOVED CORROSION PER SRM 51-10-01 & 57-10-01 FIG 1; FABRICATED AND INSTALLED REPAIRS PER ECRA 470-57-289-2.SDR LR7A06060Stiffener · crackedDURING SCHEDULED C7 CHECK PER JOB CARD HC5711 FOUND LT INBOARD WING FRONT SPAR WEB STIFFENER WITH A 3.5 INCH CRACK INSIDE OF NR 2 DRY BAY AT FS 517, CWS 178, WL 275. REPLACED STIFFENER IAW SMP 583 51-60 & 51-70.SDR EIA2006202Spar · corrodedLEFT WING LEADING EDGE CAVITY SPAR WEB AT LOWER CHORD HAS CORROSION FROM OFSS 1258-1274. REMOVED CORROSION PER B747 SRM 51-10-01, FABRICATED AND INSTALLED REPAIR PER ECRA 470-57-283-2.SDR ABXA060241Spar · corrodedRIGHT WING REAR SPAR AREA HAD PANEL STRUCTURE WITH CORROSION UNDER NUT PLATES. AREA WAS PREVIOUSLY BLENDED AT WBL 280 NEAR INBOARD AILERON. REPAIRED CORRODED AREA OF SPAR IAW B767 SRM 57-51-02.SDR AWXA200601096Spar · scratchedSCRATCH IN THE PROXIMITY OF HOLE NR 52 OF REAR SPAR RIGHT WING. THE SCRATCH WAS REPAIRED IAW PART B OF AWA ERN 26 - 5721 - 06181 - ES2.SDR AWXA200601089Spar · corrodedDISCOVERED CORROSION AROUND HOLE NR 73 OF REAR SPAR LEFT WIND. REMOVED IAW PART A OF ER NR 26 - 5721 - 06158 - E82.SDR AWXA200601082Spar · corrodedDURING C7 CHECK DISCOVERED CORROSION AROUND HOLE NR 55 OF THE LEFT WING REAR SPAR. CORROSION WAS REMOVED AROUND HOLE NR 55 LEFT WING REAR SPAR IAW PART A OF AMERICA WEST AIRLINES ENGINEERING REPAIR NR 26-5721-06181-ES2.SDR 06FDEA2274Spar Cap · corrodedDURING PASSENGER TO FREIGHT CONVERSION: FOUND CORROSION ON LT WING UPPER REAR SPAR CAP AT STA XORS 653.100, XORS 737,550, XORS 826.500. REMOVED CORROSION FOR SRM 57-20-00 FIG 16. MEASURED THK AND IN LIMITS FOR SRM 57-20-00 FIG 16. PERFORMED DYE PENETRANT ISDR QXEA200601634Spar · damagedPDX: GOUGE FWD LT WING SPAR AT UPPER BONDING FLANGE APPROX YW 217.00 JUST INBOARD OF LEADING EDGE. MAINTENANCE REPAIRED IAW Q400 SRM 51-21-10, SRM 51-25-10, NDTM PART 1, 51-00-02, HORIZON EA 6-57-493 AND RD 8/4-57-676.SDR QXEA200601491Spar Cap · brokenPDX: RT WING LOWER SPAR CAP BROKEN OFF AT APPROX STA YW150.0 - 154.0. MAINTENANCE REPAIRED IAW Q400 NDTM PART 6, 51-00-01, HORIZON EA 6-57-448, RD 8/4-57-671 AND NDTM PART 6, 51-00-01-250-801.SDR 06FDEA2198Spar Cap · corrodedLEFT HAND WING REAR SPAR UPPER CAP AT STA XORS 780 TO XORS 801 FOUND WITH CORROSION. REPAIRED AS PER FEDEX E.A. 1-5710-99688. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA2197Spar Cap · corrodedLEFT HAND WING REAR SPAR UPPER CAP STA XORS 670 TO XORS 708 FOUND WITH CORROSION. REPAIRED AS PER FEDEX E.A. 1-5710-99688. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR QXEA200601426Spar · corrodedPDX - C4 SUSPECTED CORROSION ON AFT SIDE ON FORWARD SPAR BOTTOM AT YW255.000, LEFT HAND WING AFT SIDE OF SPAR. REPAIRED IAW DHC-8-200 SRM 51-20-11, 51-20-16 AND 51-20-36.SDR QXEA200601425Spar · corrodedPDX - C4 SUSPECTED CORROSION ON AFT SIDE OF FORWARD SPAR AT YW2.55000, LEFT HAND WING. REPAIRED IAW DHC-8-200 SRM 51-20-16 AND 51-20-36.SDR GUUA94957060206ASpar Cap · damagedRT WING REAR SPAR LOWER CAP AFT FLANGE DEFLECTED .046 INCHES UPWARD. LOCATED AT WS 104.50. HAND FORMED SPAR FLANGE BACK TO ORIGINAL PROFILE, PERFORMED NDT EDDY CURRENT INSP BY A QUALIFIED LEVEL III INSPECTOR NO CRACK INDICATIONS NOTED. FABRICATED AND INSTALLSDR 2006FA0000595Spar · crackedREQUIRED INSPECTION OF WOODEN WING SPARS IN ACCORDANCE WITH AD. REVEALED A COMPRESSION CRACK IN THE LT WING FWD SPAR AT THE TOP OB OF WING STRUT ATTACH DOUBLER PLATE. (K)SDR AUCR200600006Spar Cap · crackedDURING SCHEDULED INSPECTION FOUND CORROSION INDUCED CRACK IN UPPER AFT SPAR CAP EXTENDING OUTBOARD FROM PREVIOUS REPAIR IN THE AREA OF FLAP TRACK 5, WS 346. DURING DISASSEMBLY TO EFFECT REPAIR FOUND ADDITIONAL STRESS CORROSION FRACTURE ON UPPER AFT SPAR CAP ASDR QXEA200602362Spar · damagedYYC: LT WING REAR SPAR HAS 30 HST COLLARS RUBBING CONTROL CABLES AT INBOARD FLAP, INBOARD SCREW JACK, YW55. MAINTENANCE REPAIRED IAW Q400 SRM 51-40-15-330-801 AND SRM 51-23-20-390-801.SDR UPS06847084Spar Cap · crackedINSPECTION TYPE:SP 3 MAIN-CRACK ONE HALF INCH CENTER SPAR AFT SURFACE AT XRS26. REPAIRED CENTER SPAR CAP IAW SAA EA 008-5710-01-A0218, UPS RAA DC8-57-20169.SDR LR7A06042Spar · crackedDURING SCHEDULED C6 CHECK PER JOB CARD HSP57119/L FOUND CENTER WING FWD SPAR WEB CRACKED AT CWS 20.5, FS 517, WL 287. REPAIRED WEB IAW LAC MEA 382-57-06-017.SDR 1060504022ASpar Cap · corrodedBIO-CORROSION RT MAIN SPAR CAP AT WS 124.588. REPAIRED IAW MFG FR-CO-01350 REV.1SDR 1060504022Spar Cap · corrodedBIO-CORROSION LT MAIN SPAR CAP AT WS124.588. REPAIRED IAW MFG FR-CO-01350 REV.1SDR GUUA05210602Spar Cap · damagedFLIGHT: 9137 SAQ/FLL RT LANDING GEAR COLLAPSE BACKWARDS ON LANDING FOUND RT WING REAR SPAR LOWER CAP AFT FLANGE DEFLECTED .046 INCHES UP. HAND FORMED SPAR FLANGE BACK TO ORIGINAL PROFILE PERFORMED NDT EDDY CURRENT INSPECTION BY A QUALIFIED LEVEL III INSPECTORSDR UPS06447024Spar · crackedINSPECTION TYPE:C LT WING FRONT SPAR WEB AT WS 642 AREA 1EA HOLE (9TH HOLE COUNT FROM TOP) COMMON TO RIB POST FOUND CRACK AT WEB. CRACK LENGTH .0625 INCH. LT WING FRONT SPAR WEB AT WS 642 (9TH HOLE COUNT FROM TOP) COMMON TO RIB POST IN ZONE A AS PER SB 747-5SDR USAA060716Fitting · damagedWING FRONT SPAR PITCH LOAD FITTING. ACCOMPLISHED AS REQUIRED, REMOVED & REPLACED FITTINGS, FASTENERS PER EO 5700T254A .SDR AWXA200600955Spar · crackedNR 5921152 - DURING C-19 CHECK, DISCOVERED CRACK INDICATIONS 3 HOLES UPPER AFT SPAR CHORD UNDER LT MAIN LANDING GEAR SUPPORT FITTING. MAINTENANCE REPAIRED UPPER AFT SPAR CHORD UNDER LT MAIN LANDING GEAR SUPPORT FITTING IAW ER 03-5700-06152-RC1.SDR AWXA200600947Spar Cap · corrodedNR 5921066 - DURING C11 CHECK DISCOVERED CORROSION ON THE RT WING REAR SPAR UPPER CAP, APPROXIMATELY 36 INCHES FROM WING TO BODY FAIRINGS AT WS 170R. CORROSION WAS FOUND TO BE OUT OF SRM LIMITS. MAINTENANCE REPAIRED THE RT WING REAR SPAR UPPER CAP AT WS 170RSDR 06FDEA1913Spar Cap · corrodedFOUND LEFT WING, REAR SPAR UPPER CHORD AT APPROX STA XORS 1040. FOUND CORRODED. CORROSION AT LEFT WING REAR SPAR UPPER CHORD AT APPROX STA XORS 1040. REPAIRED AS PER FEDEX EA NR 1-5710-97758, TITLE: WINGS, LEFT REAR SPAR UPPER CAP AFT TANG CORROSION CENSDR UPS06847043Spar Cap · crackedINSPECTION TYPE:C1 WING CTR LOWER SPAR CAP CRACKED, LEFT W/W LBL 9-19 AND LBL 37-44. STOP DRILLED CRACKS AT WING LWR CTR SPAR CAP LBL 9-19 AND LBL 37-44. FABRICATED AND INSTALLED REPAIR PARTS AT WING CTR SPAR CAP LBL 9-19 AND LBL 37-44 IAW SRO8570009 REV A CSDR UPS06447025Spar · crackedINSPECTION TYPE:C LT WING FRONT SPAR UPPER CHORD WS 642 AREA FOUND 1EA HOLE CRACK AT WEB RUNNING O/B APPROX .0625 INCH LONG. LT WING FRONT SPAR UPPER CHORD WS 642 WEB REPAIRED AS PER RS R57-21-35488. INSPECT THE FRONT SPAR IN ZONE-A AS PER SB 747-57A2311 R2 SDR UPS06847044Fitting · gougedINSPECTION TYPE:C3 LT WING FLAP STA 219 CANOE SIDE BRACES HAVE PLAY AT ACTUATOR UPON REMOVAL OF LT WING FLAP STA 219 CANOE, FOUND REAR SPAR FITTING GOUGED OUT OF LIMITS IAW SRM 57-51-12. MACHINED LT WING SPAR FITTING. FABRICATED AND INSTALLED FOUR SPACERS ALSDR CA061025006Spar · cracked(CAN) DUING INSPECTION IAW FAA AD 90-08-14 AND SB53-2269 REV 2 SHORT CRACKS WERE VISUALLY FOUND EMINATING FROM 2 HUCK BOLT LOCATIONS ON THE LT FORWARD WING SPAR CARRY THROUGH WEB FACE. CRACKS WERE CONFIRMED BY LPI. REPAIRED IAW MFG FAA APPROVED DRAWING 58-4000SDR ACE04302006Spar Cap · corrodedMAINTENANCE FOUND CORROSION ON FORWARD SPAR LOWER CAP FORWARD FLANGE, IN THE CENTER FUSELAGE BAY, UNDER ORIGINAL SEALANT. REPAIR REQUIRED REMOVAL OF CORROSION AND STRAP DOUBLER PER FR-CO FACTORY REPAIR DESIGN.SDR ABXA060222Spar · corrodedLEFT WING REAR SPAR AFT FACE HAD CORROSION AT WING ROOT XRS 5. ACCOMPLISHED REPAIR IAW REA D857-53586-MR, REV. IR AT LEFT WING REAR SPAR.SDR 2006FA0000500Spar · crackedDURING WING RECOVER, FOUND LT WING FRONT SPAR WITH A CRACK ORIGINATING AT THE BUTT END, FOLLOWING THE WOOD GRAIN OB THROUGH UPPER ATTACH BRACKET HOLES AND EXTENDING APPROXIMATELY 1 INCH PAST IB MOST FUEL TANK SUPPORT BRACKET, UPPER HOLE. NO EVIDENCE OF CRACKSSDR 1060406014ASpar · corrodedBIO CORROSION LT MAIN SPAR CAP FLANGE AT WS 124.588 REPAIRED IAW FIELD REPAIR FR-CO-01337 REV.1SDR 1060406014Spar · corrodedBIOCORROSION RT MAIN SPAR CAP FLANGE AT WS124.588 REPAIRED IAW FIELD REPAIR FR-CO-01337 REV.1SDR 06FDEA1615Spar · corrodedCORROSION RT WING REAR SPAR UPPER SURFACE BETWEEN BS 799-827. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOL2 AND FOUND WITHIN LIMIT AS PER SRM 57-20-00 FIG16 VOL1.
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