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 SWIA202155870Spar · crackedCOMPLY WITH BOMBARDIER SERVICE BULLETIN 670BA-57-016 REV D DATED 09/12/2014 FOR THE LH AND RH REAR SPAR LINK ASSY REPLACEMENTS (BOTH ARE CRACKED AT CLEVIS BEARINGS) (C-CHECK) RO 2/1/2021 COMPLIED WITH BOMBARDIER SERVICE BULLETIN 670BA-57-016 REV D DATED 09SDR JGVR20210122001Spar Cap · corrodedBLENDED CORRODED AREA OF THE AFT LOWER SPAR CAP INBOARD OF WS 37 LOCATED IN THE RT MAIN LANDING GEAR WHEEL WELL, PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. BLENDED CORRODED AREA OF THE LOWER AFT SPAR CAP INBOARD OF WS 37 LOCATED ON THE LT MAIN LANDINSDR R61A2021020700145Spar · crackedDURING HEAVY MAINTENANCE FOUND RH WING OB SPAR 1 CRACKED AT WINGTIP ATTACHMENT. RH WING OB SPAR 1 REPLACED WITH NEW IAW EMB SRM 51-43-04 AND 51-43-03. A/C REMAINS IN CHECK.SDR R61A2021011800068Spar · crackedDURING HEAVY MAINT CHECK FOUND LT WING SPAR 1 CRACKED. REMOVED AND REPLACED LT WING SPAR 1 AT WINGTIP ATTACHMENT, IAW EMB SRM 51-40-08, 51-23-06.SDR R61A2021011800067Spar · crackedDURING HEAVY MAINT CHECK FOUND RT WING SPAR 1 CRACKED. REMOVED AND REPLACED RT WING SPAR 1 AT WINGTIP ATTACHMENT, IAW EMB SRM 51-40-08, 51-23-06.SDR COEA2021020301803Spar · damagedDURING TAXI, THE AIRCRAFT STRUCK THE HANGAR. DAMAGE DESCRIPTION RT WING FRONT SPAR SUSTAINED COMPOSITE DELAMINATION, TORN MISSING PLIES AND BROKEN FIBERS AT RIB 31. CORRECTIVE ACTION REPAIRED PER SRAS ES_0131069_02...17181 ISSUE B, DATED 2/3/2021.SDR FDEA202101150129Former · crackedRT WING FIXED LEADING EDGE FORMER CRACKED AT APPROXIMATELY OSS663. REMOVED OLD AND INSTALLED NEW NOSE FORMER, IAW BAC DWG 114T2512 AND FED EX EA H- 5720-T0359036.SDR SWIA202156418Spar · chafedRIGHT WING AFT SPAR - AFT LOWER WING PLANK, DIRECTLY BELOW REAR LOWER SPLICE JOINT @ BL 45, SHOWS EVIDENCE OF CHAFFING AND IMPACT DAMAGE AS MARKED / 57-610-600 (C-CHECK) RO 2/25/2021 REMOVED CHAFING DAMAGE TO WING PLANK TO A SMOOTH FINISH.C/W NDT INSPECTIOSDR IPXA2021020665378Spar Cap · corrodedINSPECTION TYPE:4CLT WING UPPER T/E PANEL IS BULGED FWD OF #4 SPOILER.REPAIRED CORRODED LT WING UPPER REAR SPAR CAP AFT FLANGE BETWEEN XORS 645 AND XORS 673 IAW VT-SAA EA 011-5710-01-A8847 REV. IR AND UPS EO MD11-5710-79244-A. (MINOR)SDR IPXA2021020665385Spar Cap · corrodedINSPECTION TYPE:4CLT WING REAR SPAR LOWER CAP HAS CORROSION AT O/B FLAP O/B HINGE I/B SIDE BRACE.REPAIRED CORRODED LT WING REAR SPAR LOWER CAP BETWEEN XORS 714 & XORS 735 IAW VT-SAA EA 011-5710-01-A8817 REV. IR AND UPS EO MD11-5710-79239-A. (MAJOR)SDR IPXA2021020165189Spar Cap · corrodedINSPECTION TYPE:C4LT WING TE UPPER SPAR CAP CORRODED STA XORS 558. REPAIRED CORRODED LT WING TE UPPER SPAR CAP IAW VT-SAA EA 011-5710-01-A8827 REV I/R AND UPS EO MD11-5710-79101-A. MINORSDR JGVR2021011101Spar · corrodedTWO SPOTS OF VERIFIED CORROSION ON LT WING MID SPAR, AFT SIDE AROUND BRAKE LINE FITTINGS. MECHANICALLY REMOVED CORROSION FROM AROUND BOTH LT BRAKE CARRY THRU FITTING IN LT WING MID SPAR. REPAIRED CORROSION BLENDS, IAW TEXTRON AVIATION MEMO DQ28431 RRL DATED SDR 6PMR202012270001Spar · corrodedLT WING UPPER SKIN, FRONT SPAR, APPROXIMATELY WING STA 285 HAS CORROSION AROUND FASTENERS. CORRECTIVE ACTION: COMPLIED WITH EO 20495-6.SDR 6PMR2020122480315Spar · corrodedLT WING UPPER SKIN, FRONT SPAR, APPROXIMATELY WING STA 170 HAS CORROSION AROUND FASTENER. CORRECTIVE ACTION: REMOVED CORROSION AND BLENDED AREA. ACCOMPLISHED NDT, SHOT PEEN. REAPPLIED CORROSION PROTECTION, IAW EO 20495-6. PEMCO NON-ROUTINE 10248-0315.SDR SIMA20201220007Spar · crackedLT WING SPAR I CRACKED AT RIB 9. CRACK LENGHT 0.3 NUMBER OF CRACKS 1. C/A: ACCOMPLISHED PERMANENT REPAIR ON LT WING SPAR I AT RIB 9, IAW EMB 145 SRM 57-20-05 ITEM 3.SDR SWIA202055871Spar · crackedL/H SIDE REAR WING SPAR LINK AT FS 797.0 HAS CRACK AT CLEVIS BEARING. (C-CHECK) RO 2/1/2021 CORRECTIVE ACTION COMPLIED WITH ON MX 22193034 JOB 91516157 OP 4, COMPLY WITH SB 670BA-57-016 REV D 9/12/2014 FOR LH AND RH REAR SPAR LINK ASSEMBLY REPLACEMENTS.SDR SWIA202056362Tape · chafedRIGHT WING FRONT SPAR IS MISSING WHITE ANTI-CHAFE TAPE AT NUMEROUS LOCATIONS. REPLACE AS REQUIRED. (UPPER AND LOWER) (C-CHECK) RO 2/17/2021. REPLACED UPPER AND LOWER RT WING FRONT SPAR MISSING ANTI CHAFE TAPE IAW CRJ200 AMM 57-41-01-400-803, AMM 57-41-01-40SDR JGVR20201214001Spar Cap · corrodedREMOVED EXISTING HI-LOC FASTENERS AND BLENDED CORRODED AREA OF THE LT AFT WING SPAR LOWER CLIP LOCATED IN THE LT MAIN LANDING GEAR WHEEL WELL. PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, PRIMED REPAIR AREA, INSTALLED EXISTING FASTENESDR JGVR2020124001Spar · corrodedREMOVED EXISTING HI-LOC FASTENERS AND BLENDED CORRODED AREA OF THE LT AFT WING SPAR LOWER CLIP LOCATED IN THE LT MAIN LANDING GEAR WHEEL WELL. PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, PRIMED REPAIR AREA, INSTALLED EXISTING FASTENESDR SWIA202054885Spar · crackedRT WING FRONT SPAR CRACKED AT TIP. C-CHECK RO 12/27/2020. REMOVED AND REPLACED RT WING SPAR I WITH NEW PART FROM FACTORY. NO CHANGE TO WEIGHT AND BALANCE, REF EMB175 SRM.SDR SWAA2021011338320Spar · corrodedCORROSION FRONT SPAR WEB LOCATED FUEL BOOST PUMP IFSS 120 APPROXIMATELY AT LT WING AND WBL 94.24. REPAIRED LT WING FRONT SPAR WEB AT IFSS 120.00 AT FUEL BOOTS PUMP FAYING SURFACE, IAW EA NR 20-157-02599 REV IR AND EA 57-0854-20 REV 0 MEASURES OF THE REWORK ARSDR SWAA2021011338321Spar · corrodedCORROSION FRONT SPAR WEB LOCATED FUEL BOOST PUMP IFSS 120 APPROXIMATELY AT RT WING AND WBL 94.24. REPAIRED RT WING, FRONT SPAR WEB LOCATED AT 120.0 IFSS AT FUEL BOOST PUMP FAYING SURFACE, IAW EA NO 20-157-02589 REV IR AND EA NR 57-0819-20 REV 0 EWIS PROTECTIOSDR R61A2020121600905Spar · crackedWHILE IN HEAVY CHECK, RT WING OUTBOARD SPAR 1 CRACKED AT WINGTIP ATTACHMENT, REPLACED ON AAR NRC 4500809-6000-0005, PER SRM 51-43-03. THIS AIRCRAFT IS IN HEAVY CHECK IN YQG AT THE TIME OF REPORTING.SDR R61A2020121600890Spar · crackedMAJOR REPAIR, LT WING OUTBOARD SPAR 1 CRACKED AT WINGTIP ATTACHMENT. REPLACED SPAR 1 ON AAR NRC 4500809-5000-0030, PER SRM 51-43-01.SDR UIEA2020120302522Spar · corrodedCORROSION ON LT WING FRONT SPAR LOWER CHORD BETWEEN FSSO 1509.45 AND 1525.45. ACCOMPLISH EI NO T2020A57M-3164 REV 2 AND REV 1. INSTALLED PART IAW DWG NO 65B07853 SHEET 03 REV A. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR UIEA2020120302525Spar · crackedCRACK ON WEB OF LT WING FRONT SPAR NEAR FSSI 686. ACCOMPLISHED IAW EI NO T2020A57M-3151 REV 1 AND REV 2. JOB COMPLETED AND CONDITION CHECK SATISFIED.SDR FDEA202011202913Spar · crackedRT WING, BASIC WING STRUCTURE FRONT AND REAR SPAR BOTTOM BOOM INBOARD AND OUTBOARD OF RIB 9 INSPECTION, FOUND W HOLE WITH CRACK SIGNAL. COMPLIED WITH EA: 6-5710-T0358209 P1. TITLE: WINGS-BASIC WING STRUCTURE-RT WING REAR SPAR BOTTOM BOOM HOLE W/558 AT RIB 9 CSDR EE4Y2020111811942Spar · crackedLT WING REAR SPAR UPPER CHORD AT RSS 224 OPEN HOLE WITH CRACK INDICATION. NOTE: IT WAS REPAIRED, AS PER B737-400 SRM INSTRUCTIONS (REF: JOB: A1J185 NRI: 5-43).SDR 2020FA0000507Spar Cap · corrodedDURING AN ANNUAL INSPECTION, THE LEFT WING WAS REMOVED AS PART OF THE AD INSPECTION OF THE WING CENTER SECTION AD 2002-26-02. I HAD ALREADY INSPECTED THE WING PANEL FOR AD 2003-21-01 WHILE IT WAS STILL ON THE AIRFRAME AND HAD NOT FOUND ANYTHING. HOWEVER, SINSDR DALA2021012000370Spar · corrodedCORROSION FOUND ON MATING SURFACES OF LT WING REAR SPAR (AFT SURFACE) COMMON TO RETRACTION JACK FITTING AROUND HOLE NR 80. CORRECTIVE ACTION: PERFORMED INSP WITH REPETETIVE INSP MON PUT IN PLACE. ER/A 588446-14AD REV ORIGINAL. OK FOR CONTINUED SERVICE.SDR DALA2021011900307Spar · corrodedCORROSION FOUND ON MATING SURFACES OF RT WING REAR SPAR (AFT SURFACE) COMMON TO RETRACTION JACK FITTING AROUND HOLES NR 58 AND NR 81. CORRECTIVE ACTION: COMPLIED WITH ER/A 588447-14AD REV ORIGINAL. OK TO CONTINUE TO MONITOR, JOB COMPLETE.SDR DALA2020111703761Spar · corrodedCORROSION FOUND ON MATING SURFACES OF LT WING REAR SPAR (AFT SURFACE). CORRECTIVE ACTION: COMPLIED WITH ERA 588446-14AD (1656889).SDR 2020FA0000564Spar · corrodedTHE AIRCRAFT CABIN HEADLINER WAS REMOVED FOR MAINTENANCE. AFTER REMOVAL, SEVERE INTERGRANULAR CORROSION WAS FOUND ON THE CARRY THROUGH SPAR. THIS RENDERED THE SPAR UNAIRWORTHY AND HAS TO BE REPLACED. AFTER FURTHER INVESTIGATION, IT WAS DISCOVERED THERE WAS SDR FDEA202011122831Angle · crackedRT WING, RIB 8 INSPECTION OF CENTER SPAR SEALING ANGLE VERTICAL WEB ADJACENT TO PYLON REAR ATTACH FITTING, FASTENER HOLE 58 FOUND CRACK. COMPLIED WITH EA: 6-5710-106289 C P4. TITLE: WINGS-BASIC WING STRUCTURE-SB A300-57-6033 ELONGATED HOLES & CRACK AT RIB 8 SDR R61A202011120045Spar · crackedMAJOR REPAIR LT WING TIP SPAR 1 CRACKED. REPLACED LT SPAR 1.SDR R61A202011120044Spar · crackedMAJOR REPAIR RT WING TIP SPAR 1 CRACKED. REPLACED RT SPAR 1.SDR JGVR202011110202Spar · corrodedSPOT OF VERIFIED CORROSION IN LT WHEEL WELL ON AFT SPAR, LOWER SPAR CLIP. MECHANICALLY REMOVED 1 SPOT OF VERIFIED CORROSION IN LT WHEEL WELL ON AFT SPAR LOWER SPAR CLIP. FOUND CORROSION BLENDS EXCEEDING C680 SRM 51-70-02 AND SUBMITTED FINDINGS TO TEXTRON ENGSDR JGVR20201111001Spar · corrodedSPOTS OF VERIFIED CORROSION IN RT WHEEL WELL ON AFT SPAR, LOWER SPAR CLIP. MECHANICALLY REMOVED 1 SPOT OF VERIFIED CORROSION IN RT WHEEL WELL ON AFT SPAR LOWER SPAR CLIP. FOUND CORROSION BLENDS EXCEEDING C680 SRM 51-70-02 AND SUBMITTED FINDINGS TO TEXTRON ENSDR SWIA202053968Spar · bentREAR SPAR (P/N 601R10851-3 SRM 57-21-07, FIG 4 ITEM 11) LOWER FLANGE BETWEEN WS 371.00-WS 377.00 IS BENT 0.200" UPWARD ALONG 2.20" SPANWISE. CLASSIFIED AS MAJOR REPAIR M-337 INITIATED. FILED CLOSED. REPAIR OF REAR SPAR LOWER FLANGE PERFORMED BY MHIRJ MRT PESDR IPXA2020112162612Spar Cap · corrodedINSPECTION TYPE: 4C LT WING REAR SPAR UPPER CAP AFT FLANGE HAS CORROSION BETWEEN XORS 672.5 AND XORS 762. REPAIRED CORRODED LT WING REAR SPAR UPPER CAP AFT FLANGE BETWEEN XORS 672.5 AND XORS 762, IAW VT-SAA EA 011-5710-01-A8724 REV IR AND UPS EO MD11-5710-785SDR IPXA2020111762512Spar Cap · corrodedINSPECTION TYPE: 4C LT WING REAR SPAR LOWER CAP HAS CORROSION JUST BELOW NR 3 SPOILER. REPAIRED LT WING REAR SPAR LOWER CAP/VERTICAL FLANGE AFT SURFACE/BETWEEN XORS 582 & XORS 587, IAW VT-SAA EA 011-5710-01-A8708 REV. IR AND UPS EO MD11-5710-78522-A. (MINOR)SDR IPXA2020111762511Spar Cap · corrodedINSPECTION TYPE: 4C RT WING AFT LOWER SPAR CAP HAS EXFOLIATION CORROSION INBOARD OF OUTBOARD FLAP OUTBOARD HINGE.REPAIRED CORRODED RT WING REAR SPAR LOWER CAP VERTICAL FLANGE AFT SURFACE, HORIZONTAL AFT FLANGE UPPER AND LOWER SURFACES/BETWEEN XORS 720 & XORS 7SDR IPXA2020110862141Spar Cap · corrodedINSPECTION TYPE: 2C RT WING AFT LOWER SPAR CAP HAS CORROSION AT XORS STA 705. REPAIRED RT WING AFT LOWER SPAR CAP BETWEEN XORS STA 703-XORS STA 708, IAW SRM 57-00-10 FIG 101 ALLOWABLE DAMAGE 1. (MINOR).SDR DALA2020110503586Spar · damagedDURING INITIAL INSPECTION MAINTENANCE FOUND A TOOL MARK ON UPPER FILLET INTERIOR AREA STA WBL 740 FRONT SPAR RT WING. REPAIRED PER ERA 588364-14.SDR HNAA2020121100341Spar · crackedLT WING SPAR 1 CRACKED AT SECOND SCREW HOLE OUTBOARD OF RIB 9, CRACK IS APPROXIMATELY 3/8" LONG, FROM FWD FLANGE EDGE TO SCREW HOLE. EASI NR 6581 USED, FREQ=400KHZ, V-GAIN=77.0, H-GAIN=64.0, LPF=100. ACCOMPLISHED REPAIR OF LT WING SPAR I AT RIB 9, IAW EMB 14SDR HNAA2020121100339Spar · crackedRT WING SPAR 1 CRACKED ON LOWER FLANGE AT SCREW HOLE JUST OUTBOARD OF RIB 9. CRACK IS APPROXIMATELY 1/4 INCH, END IS MARKED. ACCOMPLISHED REPAIR OF RT WING SPAR I AT RIB 9, IAW EMB 145 SRM 57-20-05 ITEM 2 AND EO-1-57-20-0412.SDR COEA2021031707913Spar · corrodedWO 223107 NR 903015 HEAVY CHECK COE/MAJOR REPAIR: WHILE PERFORMING PERMANENT REPAIR, ADDITIONAL LEVEL 2 CORROSION FOUND ON REAR SPAR UPPER CHORD BETWEEN RIBS 3L-4L OUTBOARD OF RIB 4L. CORRECTIVE ACTION: REPAIRED PER SRAS ES-0092053_01/19...14067 ISSUE B, DATEDSDR SWAA2021072826556Spar Web · corroded***CORROSION*** RT WING FRONT SPAR WEB HAS CORROSION COMMON TO UPPER BOOST PUMP BONDING STRAP MOUNT LOCATION APPROXIMATELY IFSS 119; 10 INCHES FROM BOTTOM OF WEB / REPAIRED CORROSION DAMAGE ON R/W FRONT SPAR WEB COMMON TO UPPER BOOST PUMP BONDING STRAP LOCATIOSDR JGVR20201027002Spar · corrodedMECHANICALLY REMOVED CORROSION FROM AFT SPAR, LOWER FORWARD SPAR CAP ANGLE LOCATED IN RT WHEEL WELL AT WS35. PERFORMED NDT AND REPORTED RESULTS FOR REPAIR DISPOSITION. CLEANED, TREATED AND TOP COATED REPAIRED AREA, IAW TEXTRON STRUCTURES FIELD REPAIR.SDR SWAA2020120329114Spar · corrodedCORROSION FRONT SPAR ON LEADING EDGE INTERNAL AREA OF KRUEGER FLAP AT RT WING LOCATED AT WBL 94.24 AND IFSS 120.00. PERFORMED REPAIR FRONT SPAR ON LEADING EDGE INTERNAL AREA OF KRUEGER FLAP AT RT WING LOCATED AT WBL 94.24 AND IFSS 120 FUEL BOOST PUMP FAYING S
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