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 IPXA09157988Skin · puncturedINSPECTION TYPE:N/A .375 INCH PUNCTURE BOTTOM SKIN OF T/E WEDGE. REPAIRED PER EO A300-5750-35403-B.SDR 2010FA0000039Attach Bracket · crackedDURING ACFT INSP THE RT AILERON ATTACH BRACKET PN 6624034-12 WAS FOUND CRACKED. THE CRACK APPROX 5MM IN LENGTH WAS STARTING FROM FORWARD BOTTOM EDGE TOWARDS THE BOTTOM RIVET. MFG WAS ADVISED ABOUT THE FINDING.SDR NSVA2009061Aileron · damagedAIRCRAFT REQUIRES MAJOR REPAIR DUE TO PERMANENT REPAIR OF LT AILERON TRAILING EDGE ASSEMBLY BECAUSE OF LIGHTNING STRIKE. REPAIR WILL BE PERFORMED IAW RD 8/4-57-1212 AND TRACKED BY DMI ID 12181.SDR A6WA200940787Bushing · gougedRT AILERON OTBD PCU ATTACHMENT INBD LUG BUSHING GOUGED RT AILERON OTBD PCU ATTACHMENT INBD LUG BUSHING REPLACED IAW AMM CRJ 200 20-26-00-910-803 AND REO 601R-57-61-250, REV B. (K)SDR QXEA2009111300938Skin · chafedLT AILERON PANEL 589AB CHAFED. BLENDED IAW SRM 51-21-06-001-001-A01. REMOVED .005 MAX MATERIAL, WITHIN LIMITS IAW SRM 57-61-01-001-001-A01. TREATED, PRIMED, PAINTED IAW SRM 51-21-11-001-001-A01, 51-25-06-001-001-A01 AND 51-25-16-001-001-A01.SDR SIMA200920801AFitting · gougedDURING MAIN BASE VISIT INSPECTION FOUND THE RIGHT AILERON DAMPER FITTING TO BE DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE RIGHT AILERON BY REPLACING DAMPER FITTING WITH NEW FITTING IAW EO-EM-27MR-122. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR C2XA09TY264Bracket · corrodedTYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND BOTH LEFT AND RIGHT AILERON PCA BRACKETS CORRODED AND MIGRATED HAT BUSHIONS. MAINTENANCE REMOVED AND REPLACED BOTH AILERON PCA BRACKETS IAW EC5750-01177. ALL WORK WAS ACCOMPLISHED AND OPS CHECK GOOD AND WISDR FDEA200910263665Support · corrodedRIGHT WING AILERON, OUTBOARD HINGE NR 5 SUPPORT CORRODED AT WS 817. REPAIRED AS PER EA NR F-5710-133416. REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 CRITERIA.SDR C2XA09SH355Bushing · migratedSHV - DURING C-CHECK RT AILERON HAS MIGRATED HAT BUSHING ON O/B PCA ATTACHMENT BRACKET O/B SIDE. MAINTENANCE COMPLETED REPAIR OF RT AILERON O/B PCA ATTACHMENT BRACKET O/B SIDE IAW EC 5740-01152. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR CA091020005Spar · corroded(CAN) DURING INCORPORATION OF SB 27-3928 OF WEIGHT BALANCE CLIP INSP AND REPLACEMENT, THE TECH DISCOVERED SEVERE EXFOILATION CORROSION OF THE AILERON REAR SPAR IN A AREA OF THE AILERON TRIM TAB. REAR SPAR WAS REPLACED WITH NEW.SDR C2XA09SH348Bracket · gougedSHV- DURING C-CHECK RT AILERON DAMPENER BRACKET ON AILERON IS GOUGED. MAINTENANCE REMOVED AND REPLACED RT AILERON DAMPENER BRACKET ON AILERON IS GOUGED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR IPXA09M57551Skin · delaminatedINSPECTION TYPE:4C RT OUTBOARD AILERON P/N NRC6741-504, S/N 0043 T/E "T" SECTION IS DELAMINATED FROM WEDGE LOWER SURFACE. REMOVED AND REPLACED DELAMINATED SECTION OF COMPOSITE SKIN ON RT OUTBOARD T/E WEDGE, 82.5 INCHES FROM THE OUTBOARD END AND 36.5 INCHES AFSDR IPXA09M57697Wedge · misrepairedINSPECTION TYPE:1/C REPAIR SURVEY SEQ NR 283-W3-09 LT WING INBD AILERON OTBD T/E WEDGE PREVIOUS REPAIR NOT CORRELATED TO SRM. REPAIRED AS PER IPXA EO NR MD11-5750-35153-B AND SAA EA NR 011-5751-01-A205 1, ISSUE B REF RCD 358165.SDR A6WA200940607Bushing · corrodedLT WING INBD AND OTBD AILERON HINGE FITTING PLATES AND BUSHINGS ARE CORRODED. LT WING INBD AND OTBD AILERON HINGE FITTING PLATES AND BUSHINGS ARE REPLACED IAW AMM 20-11-00-910-801 AND AMM 20-26-00-910-803 AND SRM 51-42-06. (K)SDR AALA20090925TUL01Skin · corrodedCORROSION ON LOWER OUTBOARD SKIN OF NUMBER 1 SLAT. REMOVED DAMAGED SKIN AND INSTALLED DOUBLER PER SRM 57-43-01-2R.SDR C2XA09TY244Bracket · wornRT AILERON TO THE PCA ATTACHMENT HAS MIGRATED HAT BUSHINGS. REMOVED AND REPLACED RT AILERON PCA BRACKET IAW EC5750-01177.SDR IPXA09M57553Skin · delaminatedINSPECTION TYPE:4C LEFT I/B AILERON HAS DELAMINATION AND CRACK AT T/E. REMOVED DAMAGE AND APPLIED REPAIR PLIES IAW MD-11 SRM 57-50-02 REPAIR 2.SDR IPXA09M57684Skin · delaminatedINSPECTION TYPE:4C RT OTBD AILERON DELAMINATED AT INBD LOWER T/E REMOVED DAMAGE, FABRICATED AND APPLIED REPAIR CORE AND PLIES IAW SAA EA 011-5750-01-A2049 ISSUE A AND IPXA EA MD11-5750-35163-A.SDR IPXA09M57683Skin · delaminatedINSPECTION TYPE:4C RT OTBD AILERON DELAMINATION AT INBD UPPER T/E. REMOVED DAMAGE, FABRICATED AND APPLIED REPAIR CORE AND PLIES IAW SAA EA 011-5750-01-A2049 AND IPXA EO MD11-5750-35163-A.SDR SWIA200923060Splice · crackedRIGHT AILERON SPAR SPLICE CRACKED. (C CHECK)REPAIRED PER SRM AND REO.SDR USAA2009090892397Aileron · delaminatedCLT - C6 - MAJOR REPAIR - MINOR DELAMINATION ON LEFT AILERON TRAILING EDGE 7 INCHES FROM OUTBOARD END. REPAIRED LEFT AILERON TRAILING EDGE IAW B737 SRM 51-70-17.SDR AALA20090901TUL01Warning System · malfunctionedPAP - AIRCRAFT HAD TRAILING EDGE FLAP DISAGREE INDICATION DURING ARRIVAL TO PAP. EMERGENCY DECLARED, LANDED AT PAP WITHOUT INCIDENT. ACCOMPLISHED FAULT ISOLATION MANUAL 27-51-00 FIGURE 104 OF FLAP SLAT ELECTRICAL UNIT. CYCLED FLAPS CHECKS OK. SYSTEM GROUND SDR 2009FA0000901Rib · crackedDURING AN ANNUAL INSP, THE INSPECTOR FOUND WHAT APPEARED TO BE A CRACK EXTENDING FWD OF THE OTBD AILERON HING ATTACH BRACKET, LT AILERON, IN THE AILERON L/E RIB. THE AILERON WAS REMOVED AND THE AILERON OUTER HINGE BRACKET WAS REMOVED. PAINT WAS CHEMICALLY RSDR QXEA2009090100640Skin · chafedRFD - 8 YEAR TASK - CHAFING DAMAGE FOUND ON RT AILERON. REMOVED FASTENERS FROM LEADING EDGE SKIN. REMOVED LEADING EDGE SKIN FROM AILERON, CLEANED AND PREPPED FOR NEW SKIN. RECEIVED NEW SKIN, LOCATED, DRILLED AND COUNTERSUNK FOR FASTENERS, INSTALLED USING HISDR EE4Y090220Skin · delaminatedLEFT WING TRAILING EDGE SECTION, AILERON UPPER SURFACE SKIN DELAMINATED AT STA WBL 518.850 AND WBL 504.SDR COEA2009081910900Panel · corrodedFOUND IN COE HEAVY CHECK: LEVEL 2 CORROSION - RT AILERON FIXED TRAILING EDGE WEDGE CHANNEL HAS LEVEL 2 CORROSION. REMOVED AND REPLACED RT AILERON TRAILING EDGE CHANNEL PANEL IAW ATR SRM AND CMM.SDR C2XA09SH288Attach Bracket · wornSHV - DURING C-CHECK LT AILERON ATTACHMENT POINT FOR PCA O/B ROD END HAS MIGRATED HAT BUSHING. MAINTENANCE REMOVED AND REPLACED LT AILERON PCA FITTING IAW EC5750-01177 REV C. PREPPED, ALODINED, PRIMED, AND PAINTED IAW EMB-145 CPM 51-21-06. THE AIRCRAFT WAS SDR C2XA09SH287Fitting · out of limitsSHV - DURING C-CHECK LT AILERON PCA FITTING IS OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED LT AILERON PCA FITTING IAW EC5750-01177 REV C. ALODINED, PREPPED, PRIMED AND PAINTED IAW EMB-145 CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH286Bracket · damagedSHV - DURING C-CHECK RT AILERON DAMPER BRACKET ON AILERON DAMAGED. MAINTENANCE REMOVED AND REPLACED RT AILERON DAMPER INBOARD BRACKET IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH285Attach Bracket · gougedSHV - DURING C-CHECK RT AILERON PCA ATTACHMENT BRACKET ON AILERON IS GOUGED. MAINTENANCE REMOVED AND REPLACED RT AILERON PCA ATTACHMENT BRACKET IAW EC5750-01177 REV C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR IPXA09157179Aileron · misrepairedINSPECTION TYPE:1C REPAIR SURVEY SEQUENCE 128-W3-01 DOES NOT CORRELATE TO THE SRM. REMOVED, FABRICATED AND INSTALLED REPAIR DOUBLER ON LT WING ALL SPEED AILERON PER EO A300-5750-34748-A AND EA 300-5751-01-A1997.SDR IXXA09SMN093SSkin · dentedDURING ROUTINE C CHECK INSPECTION FOUND LEFT WING INBOARD AILERON UPPER SKIN DENTED AT STATION XA 515.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED,SDR IXXA09SMN092SSkin · crackedDURING ROUTINE C CHECK INSPECTION FOUND LT WING INBOARD AILERON UPPER SKIN CRACKED AT STATION XW 563.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, SDR COEA2009081207900Cap · corrodedFOUND IN COE HEAVY CHECK: LEVEL 2 CORROSION - RT AILERON TRAILING EDGE CAP BETWEEN RIB 18 AND 19 UNDER STATIC WICK HAS LEVEL 2 CORROSION. REMOVED AND REPLACED AILERON TRAILING EDGE CAP IAW ATR SRM.SDR SWAA095167Aileron · puncturedDURING SCHEDULED SPV CHECK, FOUND RT WING AILERON PUNCTURED. REPAIRED AILERON PER SRM.SDR IPXA09M57419Aileron · delaminatedINSPECTION TYPE:1C LT OUTBOARD AILERON TRAILING EDGE HAS SMALL DELAMINATED. REMOVED PAD AND FINISH, PREPARED AND APPLIED WET LAY-UP REPAIR IAW IPXA EO MD11-5750-34605-A AND SAA EA 011-5751-01-1791.SDR USAA2009081192086Aileron · crackedCLT - Q2 - MAJOR REPAIR - COMPOSITE DAMAGE ON RIGHT AILERON TRAILING EDGE AT EACH TAB HINGE CUTOUT. REPLACED RIGHT AILERON IAW TASK CARD 03C40627010.SDR IXXA09SMN078SSkin · damagedDURING ROUTINE C CHECK INSPECTION FOUND LEFT HAND INBOARD AILERON EXTERNAL LOWER SKIN PART BROKEN AT STATION XRS 624.000.REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. BONDED PARTS AS NSDR IPXA09657004Hinge Fitting · crackedINSPECTION TYPE:C RIGHT WING I/B AILERON I/B SUPPORT HINGE FITTING UPPER & O/B FLANGE CRACKED AT FASTENER AREA. CRACK LENGTH 0.312 INCH. RIGHT WING I/B AILERON I/B SUPPORT HINGE FITTING UPPER AND O/B FLANGE CRACKED AREA REPAIRED AS PER HX RS R57-55-36392 REVSDR C2XA09SH259Hinge · wornSHV - DURING C-CHECK LT AILERON OUTBOARD HINGE POINT HAS MIGRATED HAT BUSHINGS. MAINTENANCE REMOVED AND REPLACED LT AILERON O/B HINGE POINT IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH244Fitting · gougedSHV - DURING C-CHECK LT AILERON DAMPNER FITTING GOUGED. MAINTENANCE REMOVED AND REPLACED LT AILERON DAMPNER FITTING IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR FDEA200907222702Skin · misrepairedEXISTING REPAIR AT RT WING OTBD AILERON UPPER SKIN. EXISTING REPAIR AT RT WING OTBD AILERON UPPER SKIN EVALUATED AND FOUND NOT IAW SRM REPAIR. RT WING OTBD AILERON UPPER SKIN REPAIRED IAW EA NR 1-5750-132127, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISDR IPXA09656863Support Frame · crackedINSPECTION TYPE:C RT WING - I/B AILERON I/B HINGE SUPPORT FRAME AFT UPPER FLANGE FOUND CRACKED, CRACK LENGTH 1 INCH. RT WING I/B AILERON I/B HINGE SUPPORT FRAME AFT UPPER FLANGE REPAIRED AS PER HX RS R57-55-36384 REV A. THIS REPAIR IS CLASSIFIED AS MAJOR REPSDR 2009FA0000741Aileron · fodDURING THE ANNUAL INSP, THE AILERONS WERE RERIGGED. DURING THE RERIGGING PROCESS LOOSE HARDWARE WAS FOUND INSIDE THE AILERONS STUCK TO THE INSIDE SKIN OF THE AILERON WITH PAINT. THE LOOSE HARDWARE WAS REMOVED FROM THE AILERON. THE AIRPLANE WAS PAINTED IN 2SDR 2009FA0000709Block · crackedFOUND NUTPLATES ATTACHED TO BEARING BLOCK ASSY CRACKED THROUGH THREADED PORTION OF NUTPLATE. NUTPLATE HOLDS INBD AND OTBD HINGE BOLT. SUSPECT FURTHER FAILURE COULD RESULT IN SEPARATION OF AILERON FROM ACFT IN FLIGHT. (K)SDR CA090707008Hinge · cracked(CAN) CRACKS LOCATED AT DOUBLER ANGLE BENDS, TOP AND BOTTOM, ONLY LWR CRACKS ARE VISIBLE. CRACKS AT TOP ONLY VISIBLE WITH BORESCOPE OR REMOVING THE SKIN.SDR CA090707007Hinge · cracked(CAN) HINGE DOUBLERS CRACKED AT LWR ANGLE BEND, UPON REMOVAL OF HINGE, FOUND MORE CRACKS NEAR TOP OF HINGE, NOT VISIBLE UNLESS THE SKIN IS PEELED BACK OR THE USE OF A BORESCOPE.SDR C2XA09SH184Bushing · migratedSHV - DURING C-CHECK LT AILERON O/B HINGE FITTING (ON AILERON) HAT BUSHING IS MIGRATED. MAINTENANCE REMOVED AND REPLACED LT AILERON O/B HINGE FITTING IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH187Bushing · wornSHV - DURING C-CHECK RT AILERON PCA TO AILERON ATTACHMENT HINGE HAS WORN HAT BUSHINGS. MAINTENANCE REMOVED AND REPLACED PCA ATTACHMENT FITTING ON AILERON SIDE IAW EMB-145 SRM 51-40-02. MAINTENANCE COMPLETED REPAIR OF RT AILERON PCA TO AILERON ATTACHMENT HINGSDR C2XA09SH186Bushing · migratedSHV - DURING C-CHECK LT AILERON O/B ATTACHMENT BRACKET ON AILERON SPAR, O/B & I/B HAT BUSHINGS WERE MIGRATED. MAINTENANCE REMOVED AND REPLACED LT AILERON O/B HINGE FITTING IAW SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
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