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 = '5751' 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 = '5751' 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 QXEA200500289Panel · wornRT AILERON LEADING EDGE PANEL 699CB HAS A WEAR MARK FROM THE SEAL. REPAIRED IAW CRJ700 SRM 51-12-0-001-001-A01, 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND SRM 51-25-01-001-001-A01.SDR QXEA200500270Skin · chafedYYC - RIGHT AILERON UPPER SKIN JUST AFT OF LEADING EDGE IS CHAFED AT STATION 290, 340 AND 323. REPAIRED IAW CRJ700 SRM 51-41-02-001-001-A01, 57-61-01-101-001-A01, 51-12-00-001-001-A01, 51-25-00-001-001-A01, 51-25-01-001-001-A01 AND 51-41-02-001-001-A01.SDR 05FDEA00137Balance Weight · corrodedRIGHT WING OUTBOARD AILERON 1 EACH BALANCE WEIGHT HAS CORROSION OUTBOARD SIDE OF ACTUATOR. REMOVED AND REPLACED RIGHT WING OUTBOARD AILERON BALANCE WEIGHT, BALANCE WITHIN LIMITS IAW FEDEX EA 8-5751-83957, WINGS REPLACEMENT OF CORRODED RIGHT HAND OUTBOARD AILESDR 05FDEA00110Balance Weight · corrodedLEFT WING OUTBOARD AILERON CENTER BALANCE WEIGHT CORRODED.SDR 05FDEA00108Balance Weight · corrodedLEFT WING OUTBOARD AILERON INBOARD BALANCE WEIGHT CORRODED. REMOVED AND REPLACED LEFT WING OUTBOARD AILERON INBOARD BALANCE WEIGHT IAW FEDEX EA 8-5751- 83958, WINGS-REPLACEMENT OF CORRODED LEFT HAND, OUTBOARD AILERON BALANCE WEIGHT.SDR C2XA05TY005Fitting · damagedTYS, DURING A SCHEDULED INSPECTION THE RIGHT AILERON TO PCA ATTACH FITTING HOUSING WAS GOUGED AND ELONGATED. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW EMB-145XR-AMM 27-11-00 AND EC5750-01177.SDR UPS05243685Hinge · crackedINSPECTION TYPE:C, LEFT O/B AILERON O/B BALANCE PANEL FWD IDLER HINGE CRACKED. HINGE REPLACED IAW 51-30-2.SDR USAA050169Skin · delaminatedPIT - FOUND COMPOSITE SKIN DELAMINATED 1 INCH AREA, RT AILERON TAB OUTBOARD T/E. INSTALLED REPAIR PLYS PER SRM 51-60-01 AND 51-70-16. (M)SDR 2005FA0000131Skin · crackedDURING AN ANNUAL INSPECTION OF THE AIRCRAFT THE LT AILERON ASSEMBLY WAS FOUND TO HAVE A CRACK IN THE OB SKIN. PROBABLE CAUSE OF CRACKING OF THE LT AILERON ASSEMBLY IS UNKNOWN. AILERON REMOVED FOR MAINTENANCE AND REPAIRED BY REPLACING DAMAGED PART. (K)SDR 2005FA0000130Skin · crackedDURING AN ANNUAL INSPECTION OF THE AIRCRAFT THE LT AILERON ASSEMBLY WAS FOUND TO HAVE A CRACK IN THE OB SKIN. PROBABLE CAUSE OF CRACKING OF THE LT AILERON ASSEMBLY IS UNKNOWN. AILERON REMOVED FOR MAINTENANCE AND REPAIRED BY REPLACING DAMAGED PART. (K)SDR 2005FA0000129Skin · crackedDURING AN ANNUAL INSPECTION OF THE AIRCRAFT THE LT AILERON ASSEMBLY WAS FOUND TO HAVE A CRACK IN THE OB SKIN. PROBABLE CAUSE OF CRACKING OF THE LT AILERON ASSEMBLY IS UNKNOWN. AILERON REMOVED FOR MAINTENANCE AND REPAIRED BY REPLACING DAMAGED PART. (K)SDR QXEA200500081Hinge · chafedPDX - RIGHT AILERON INBOARD HINGE CHAFFED AGAINST TRIM ACTUATOR HARNESS. PRIMED AND BLENDED AREAS IAW EA 2-57-298.SDR QXEA200500080Hinge · chafedPDX - RIGHT AILERON INBOARD HINGE CHAFED. PRIMED AND BLENDED AREA IAW EA 2-57-298.SDR C2XA04TY178Skin · dentedDURING 4C INSPECTION, FOUND THE LEFT AILERON LEADING EDGE DENTED BEYOND LIMITS. REPAIRED IAW EC5750-01233. AIRCRAFT RETURNED TO SERVICE.SDR 04FDEA03211Skin · damagedDURING AIRPLANE'S CONVERSION FROM P-F/ACF, FOUND LT OUTBD AILERON UPPER SKIN STA XOA 907 TO XOA 912. REPLACE SKIN PER SRM 51-35-01 PAG 1-12. REBALANCE AILERON WILL BE PERFORMED PER NRC NF10454.SDR USAA041033Spar · damagedPIT - Q2 - SPAR, .50 INCH X .25 INCH AREA COMPOSITE DAMAGE/ DELAMINATION. LT AILERON L/E SPAR 26 INCHES FROM OB END UPPER FLANGE. REMOVED DAMAGED AREA AND TAPER SANDED FLANGE, INSTALLED REPAIR PLYS IAW EA, SRM.SDR USAA041032Skin Panel · damagedPIT - Q2 - TOP SKIN PANEL, 2 INCH SQ SINGLE LAYER, COMPOSITE DAMAGE, LT AILERON TOP SKIN PANEL AT TAB CONTROL ROD FAIRING MOUNT SURFACE. REMOVED DAMAGED MATERIAL, INSTALLED REPAIR PLYS, RESTORES FINISH IAW SRM.SDR USAA041031Spar · damagedPIT - Q2 - SPAR, 2 INCHES X 1 INCH AREA, COMPOSITE DAMAGE/ DELAMINATION, LT AILERON, LEADING EDGE SPAR 34 INCH FROM OB END, UPPER FLANGE. INSTALLED REPAIR PLYS AND EXTRA IAW EA AND SRM.SDR 04FDEA03124Skin · delaminatedLEFT WING INBOARD AILERON LOWER SKIN BILGED, (CORRODED). REMOVED LOWER INBOARD AILERON SKIN IAW DC10 SRM 57-35-01 VOL II, FABRICATED INTERNAL DOUBLERS AND SKIN IAW DAC DWG ARC1210-1 AND EA 8-5710-81531, LEFT HAND LOWER AILERON SKIN DELAMINATION. REPAIR, BONDSDR CA041110019Support Bracket · cracked(CAN) AILERON BELLCRANK SUPPORT BRACKET WAS DISCOVERED TO BE CRACKED. PART WAS REPLACED WITH A NEW BRACKET AND THE AIRCRAFT RETURNED TO SERVICE.SDR CA050120002Balance Weight · misinstalled(CAN) DURING HEAVY MAINTENANCE THE RT AILERON WAS DISCOVERED IN AN IMPROPER CONFIGURATION. THE BALANCE WEIGHT ASSOCIATED WITH A COMPOSITE UNIT WAS FOUND TO BE INSTALLED WHEN THE AILERON WHICH WAS REMOVED FOR REPAINT COULD NOT BE BALANCED AT REINSTALLATION. THESDR SWAA043074Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND LT WING AILERON DELAMINATED. REMOVED AND REPLACED LT AILERON PER MM.SDR CA041007007Guard · missing(CAN) THE AIRCRAFT DEPARTED AIRPORT AND REPORTED AILERON CONTROLS STIFF. THE AIRCRAFT RETURNED TO WITHOUT FURTHER INCIDENT. UPON INVESTIGATION IT WAS FOUND THAT AN AILERON CABLE IN THE LT WING WAS DISLODGED FROM THE PULLEY. FURTHER INVESTIGATION SHOWED THE CABSDR UPS04243392Skin · corrodedINSPECTION TYPE-C RT OB AILERON HAS PITTING CORROSION ON CONTROL ROD ATTACH CASTING. AILERON REPLACED IAW MM 27-10-14.SDR UPS04243397Hinge · corrodedINSPECTION TYPE-C RT IB AILERON TAB HINGE CASTINGS ARE CORRODED AND SUSPECT CRACK ON AILERON REAR SPAR. REPLACED REAR SPAR IAW SRM 51-30-02. NEW TAB HINGES INSTALLED IAW SRM 51-30-02SDR QXEA200400692Skin · chafedRT AILERON UPPER HALF OF LEADING EDGE HAS VARIOUS AREAS OF CHAFING FROM APPROXIMATELY WS 282.00 TO WS 353.00. REPAIRED IAW CRJ SRM 51-21-11 AND SRM 51-12-20.SDR HNAA0400097Skin · dentedTHIS EO8-57-04-0678 PERFORMS REPAIR FOR DENTED RT AILERON LOWER SKIN (P/N 85740055). NOTED DENT REPORTED AS OIL CANNING. REPAIR CONSISTS OF DRILLING OUT CENTER OF DENT TO RELIEVE OIL CANNING THEN INSTALLING EXTERNAL DOUBLER. THIS EO IS A MAJOR REPAIR.SDR IXXA060420SDoubler · misinstalledDURING ROUTINE C CHECK, FOUND LEFT WING OUTBOARD AILERON REPAIR SHORT ONE RIVET FROM STATION XA661 TO XA671. REPLACED PER ALL APPLICABLE DATA.SDR 2004UALA00812Hinge Fitting · crackedLT WING OUTBOARD AILERON NR 2 HINGE FITTING CRACKED AT AFT LOWER AREA THROUGH LWR AFT FASTENER. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED FITTING.SDR USAA040539Skin · debondedCLT - FOUND AILERON COMPOSITE AND SEPARATED 2 INCH BY 5 INCH AREA, LEFT AILERON, INBOARD LOWER CORNER. REPAIR PLYS INSTALLED, DISBOND CHECKED, SANDED, PRIMED AND PAINTED PER EA 95798 AND SRM 51-70-17. (M)SDR IXXA060135SHinge Fitting · crackedDURING ROUTINE C CHECK FOUND LEFT WING INBOARD AILERON UPPER INBOARD HINGE FITTING CRACKED. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED HINGE FITTING. RECEIVED NEW PART, LOCATED, DRILLED, DEBURRED, PRIMED, INSTALLED NEW FITTING AND NEW FASTENERS. RIGGED ASDR SWAA042325Limiter · bindingWITH FLAPS EXTENDED INFLIGHT, CONTROLS BIND IN ROLL IN BOTH DIRECTIONS. WITH FLAPS UP ROLL IS NORMAL (AUTOPILOT WILL STAY ENGAGED WITH FLAPS DOWN) FELT BINDING AGAIN IN BANK WHEN FLAPS EXTENDED FOR LANDING. REMOVED AND REPLACED AILERON FORCE LIMITER PER MM.SDR USAA040553Skin · delaminatedCLT - FOUND SKIN DELAMINATED 3 INCH AREA, 48 INCHES FROM OUTBOARD END, TOP SURFACE, LEFT AILERON. COMPOSITE REPAIR AND BALANCED PER SRM 51-70-17, 51-60-01. (M)SDR UPS04242972Casting · corrodedINSPECTION TYPE: C, CORROSION ON LEFT O/B AILERON I/B CASTING. CASTING REPLACED IAW SRM 51-30-2.SDR UPS04242999Hinge · crackedINSPECTION TYPE: C, LT OB AILERON OB HINGE FITTING ON AIRCRAFT HAS A SUSPECT CRACK. NDT CARRIED OUT AND CRACK CONFIRMED. LT OB AILERON REMOVED IAW 27-10 -14. OB HINGE REMOVED IAW SRM 51-30-2. NEW HINGE INSTALLED IAW SRM 51-30-2.OB AILERON INSTALLED MM 27-10SDR 2004UALA00714Attach Fitting · crackedFOUND APPROX 7.5 INCH VERTICAL CRACK ON THE 2ND FROM OUTBOARD FWD WING TO AILERON HINGE ATTACH FITTING SUPPORT STRUCTURE FOR RIGHT. THE NR 2 RIGHT OUTBOARD AILERON HINGE FITTING HAD BEEN REPLACED DUE TO PRIOR CRACKING. DURING REPLACEMENT A SLIGHT MIS-ALIGNMENSDR 04FDEA02326Counterweight · corrodedRT WING TRAILING EDGE OB AILERON BALANCE WEIGHTS CORRODED AND 50 PERCENT OF PROTECTIVE PAINT IS MISSING. REMOVED AND REPLACED WEIGHT ASEMBLY IAW SB 57-119 AND CMM 57-51-02. REMOVED AND INSTALLED BUSHINGS IAW CMM 57-51-02, SB 57-119 AND EA 8-5750-77610. FLASDR 04FDEA02325Counterweight · corrodedLT OB AILERON BALANCE WEIGHTS, 5 EACH HAVE CORROSION AND CAD PLATING MISSING. REMOVED AND REPLACED WEIGHT ASSEMBLY IAW CMM 57051-07, SB 57919. REMOVED CORROSION FROM HOLE AND INSTALLED BUSHING IAW SB 57-117 AND CMM 57-51-02 AND EA 8-5750-77610. FLAP PEENED ASDR AWXA200400863Skin · delaminatedMCN - MAJOR REPAIR - DURING C-19 CHECK A PREVIOUS REPAIR ON LOWER SURFACE OF RT AILERON WAS FOUND DELAMINATED AT WBL 480.5. MAINTENANCE REMOVED EXISTING REPAIR ON LOWER SURFACE OF RT AILERON AT WBL 480.5; CLEANED AND PREPARED AREA; FABRICATED NEW REPAIR PLIESSDR DHL2004804528Doubler · brokenRT WING OB AILERON LWR. SKIN DOUBLER BROKEN 0.250, XA 615.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED EDW 27.2, DWG W27-R02, REV 1R. REMOVED DAMAGED DOUBLER IAW DWG W27-R02, ED EDW 27.2. TRIMMED OUT PLATING SEGMENT(DAMAGED) IAW DWG W27-R02, ED EDW 27.2.SDR DHL2004804529Skin · crackedITEM REF. NR. 0848: REPAIR OF DENT AND BROKEN CRACK TO RT WING IB AILERON UPPER PLATING AT XW 563.000 PERFORMED MAJOR REPAIR IAW ED-EDW 27-1, DWG W27-R01 REV IR. REMOVED EXISTING FASTENERS ON AREA IAW SRM 51-1-21 PG. 1, SRM 51-1-20D PG. 21. TRIMMED OUT DAMAGEDSDR CALA0400582Skin · damagedINSPECTION FOUND THE LT AILERON DAMAGED ON THE LOWER BONDED SKIN PANEL. THE DAMAGE WAS REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5751-01058.SDR 04FDEA02099Fitting · corrodedWINGS-OUTBD AILERON, ACTUATOR ATTACH FITTING REWORK. CLOSING ACTION ON 07/16/04. ON N/R S00014, COMPLIED WITH EA8-5750-79553.SDR 2004UALA00673Rib · crackedSIGNIFICANT SHUDDER ON CLIMBOUT WITH RIGHT O/B AIL. *S/D* THE NR 2 RIGHT OUTBOARD AILERON HINGE FITTING WAS FOUND CRACKED DUE TO FATIGUE. THE CRACKED FITTING WAS REPLACED.SDR IXXA060414SSkin · dentedDURING ROUTINE C CHECK, FOUND LEFT WING OUTBOARD AILERON SKIN DENTED FROM STATION XA646 TO XA674. REPLACED PER ALL APPLICABLE DATA.SDR DHL2004804512Bracket · crackedRIGHT OUTBOARD AILERON LWR SECTION HINGE BRACKET 1.000 CRACKED, STA XA 752.000. REMOVED CRACKED BRACKET IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW BRACKET IAW DC8 SRM 51-1-21 PG 1, DC8 SDR 04FDEA02016Skin · corrodedRIGHT HAND WING INBOARD AILERON LOWER SKIN BULGED/CORRODED AND I EACH FASTENER POPPED. REMOVED AND REPLACED INBOARD AILERON LOWER SKIN PER FEDEX EA 8-5750-77595. REMOVE AND REPLACE LEADING EDGE SKIN PER FEDEX DC10-10 SRM 51-35-01 VOL 2.SDR 04FDEA01924Skin · dentedRIGHT HAND WING INBOARD AILERON - INBOARD EDGE OF LOWER SKIN SURFACE DENTED. REMOVED DAMAGE AND FABRICATED REPAIR DOUBLER IAW DC10 SRM 57-00-01 VOLUME 1. INSTALLED REPAIR DOUBLER IAW DC10 SRM 51-35-01 VOLUME 2.SDR 04FDEA01925Skin · dentedRIGHT HAND WING INBOARD AILERON UPPER SKIN SURFACE HAS NUMEROUSE DENTS. CHECKED LIMITS ON 58 DENTS, 54 DENTS WITHIN LIMITS, 4 DENTS EXCEEDED SRM LIMITS IAW DC10 SRM 51-30-01 VOLUME II. TWO DENTS ON FORWARD UPPER SURFACE AND TWO DENTS ON AFT UPPER SURFACE DAMSDR UPS04242859Rod · crackedINSPECTION TYPE: C, RIGHT INBOARD AILERON TAB SUSPECT CRACK ON TAB ACTUATING ROD AT AFT END. HFEC CARRIED OUT IAW NDT MANUAL 51-00-00 PT 6 FIG 4, CRACKS CONFIRMED. ACTUATING ROD REMOVED IAW 27-10-01. REPLACED AFT END OF ROD IAW SRM 51-30-02. REINSTALLED AC
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