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 = '5700' 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 = '5700' 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 HSYA2013012800012Structure · corrodedDURING MX, CORROSION INSPECTION, FOUND CORROSION ON LT WING OTBD SIDE OF NR 1 NACELLE INBD T/E BETWEEN WS 160 & 175. MX REMOVED LT WING UPPER SKIN DOUBLERS AT WS 160 AT APPROX 7.5" FROM L/E SPAR AND APPROX 7.5" FROM THE REAR EDGE SPAR. ON REMOVAL AND FURTHESDR REXA2012121201607Panel · chafedRS-2-20 (PANEL RACK) PANEL 584EB IS CHAFED. REMOVED & REPLACED PANEL 584EB IAW CRJ-900 SRM 51-42-11.SDR REXA2012121201606Panel · chafedRS-2-20 (PANEL RACK) PANEL 584GB IS CHAFED. REMOVED & REPLACED PANEL 584GB IAW CRJ-900 SRSM 51-42-11.SDR REXA2012121201605Panel · wornRS-2-22 PANEL 699AB HAS A WORN GROVE IN IT. LOCATED AND DRILLED THE REPLACEMENT PANEL 699AB P/N 601R-13-440-2 REF CRJ-900 SRM 51-40-11.SDR 2012FA0000530Track · corrodedLEFT "C" TRACK CORRODED.SDR 2012FA0000529Track · corrodedRIGHT "B" TRACK CORRODED.SDR AALA20120623017Tab · dentedTWO DENTS WITH DELAMINATE CLOSE TOGETHER, LOCATED 12 AND 10.25 INCHES FROM OUTBOARD END OF TAB. HOT BONDED REPAIR DOUBLER PER ESO 80087 AND SRM 51-70-02.SDR AALA20120623016Tab · dentedTWO DENTS WITH DELAMINATE CLOSE TOGETHER, LOCATED 28.5 AND 27 INCHES FROM OUTBOARD END OF TAB. INSTALLED DOUBLER PER ESO 80087 AND SRM 51-70-02.SDR AALA20120623015Tab · dentedDENT WITH DELAMINATE LOCATED 19 INCHES FROM INBOARD END OF TAB. INSTALLED DOUBLER PER ESO 80087 AND SRM 51-70-02.SDR AALA20120623014Tab · dentedTWO DENTS WITH DELAMINATE CLOSE TOGETHER LOCATED AT 5.5 AND 7.5 INCHES FROM INBOARD END OF TAB. ACCOMPLISHED DOUBLER REPAIR PER ESO 80087 AND SRM 51-70-02.SDR DALA1517979236Support Fitting · not reportedMLG ACTUATOR SUPPORT FITTING REPAIRED IAW AA 5740-01140.SDR UALA2011101005476Skin · damagedON ARRIVAL BIRD STRIKE ON LT WING OUTBD FLAP L/E HAS A HOLE ON END CAP. R & R LE FLAP CAP.SDR FDEA201107082618Unknown · smokeON TAKEOFF, TOWER REPORTED "EXCESSIVE SMOKE TRAILING FROM LT WING." DID AN ATB, NO INDICATION OF SMOKE ON ACFT AND NO ECAM WARNINGS. MX NOTED NO LEAKS FROM LT WING OR ENGINE. CREW STATED NO ABNORMAL HYD QTY OR OIL QTY DECREASE DURING TAKEOFF. NO ABNORMASDR CA110617009Bolt · crackedLOWER FOREWARD LT WING BOLT FOUND CRACKED DURING INSP SIRM 57-16-01, ITEM 10. THE AVIA DESIGN FRONT WING KIT IS INSTALLED ON THIS ACFT. TOTAL TIME ON THIS BOLT IS 12331.0 HOURS AND 12 YEARS, LIFE LIMIT ON THIS BOLT IS 15000 HOURS OR 15 YEARS.SDR ASOA201001940Unknown · corrodedLEFT WING HAS CORROSION. BLENDED CORROSION AND CHECKED WITH DEPTH GAUGE IS.010" DEEP AND UNDER THE HEAD OF THE FASTENERS IS BEYOND LIMITS IAW SRM 53-11-10-991-804. REMOVED LT WEB GOT NEW WEB, INSTALLED LT WEB IAW SRM 51-42-06-001-001-A01 AND 51-42-13-001-001SDR DALA1018800186Fitting · damagedWHILE ACCOMPLISHING SB767-54 A0080, FIG 48. FOUND LT WING AFT PITCH LOAD BACKUP FITTING PN 112T6006-5 TO HAVE SEM CONDITION AS SHOWN IN FIG 1. ADDED A RADIUS FILLER TO THE FITTING INSIDE THE SEM FTG HOLE IAW ERA 482262-14AD, REV O/ REF NRC 52674.SDR NSVA201089Structure · damagedRJ STRUCK 251CJ'S RIGHT WING CAUSING DAMAGE. THE INCIDENT OCCURRED DURING THE BOARDING PROCESS. THE PASSENGERS WERE DEPLANED. NO INJURIES OR ILLNESS REPORTED. FERRIED AIRCRAFT TO IAD AND REMOVED AND REPLACED THE LEADING EDGE.SDR FDEA201003100748Bolt · unknownUNABLE TO INSTALL IEA FASTENER IAW EO F-5450-7-5003C PT3 & PT4, FOR THE LT & RT WING ISLF. INSTALLED 2EA BACB30US10K BOLTS IAW EA F-5450-131166 IN THE LT & RT WING ISLF. FAA FORM 8100-9 ATTACHED. ( LOCATION PP-RBL 9, WS 285.65 ). MAJOR REPAIR.SDR 2009F00136Windshield · crackedIN CRUISE PILOTS WINDSHIELD CRACKED JUST RT OF CTR LINE FROM BOTTOM TO THE TOP OF THE PANE. DIVERTED FOR INSPECTION. MX INSPECTED AND APPLIED TAPE IAW CH56-10-01. MEL'D THE WINDSHIELD HEAT. CONTINUED ON.SDR 2009FA0000870Rod End · corrodedA MAJOR PORTION OF THE ROD END IS CORRODED. THE TOP OF THE SPHERICAL END OF THE BALL (ROD END) IS AGAINST THE BOTTOM OF THE WING SKIN. THE ROD END IS VERY DIFFICULT IF NOT IMPOSSIBLE TO INSPECT WITHOUT REMOVING THE WING STRUT AND PERFORMING A GOOD VISUAL INSPESDR EE4Y090277Skin · delaminatedRT WING INBOARD VANE FLAP OUTER AND INNER SKIN DELAMINATED.SDR CA090730002Fairing · improper partPART DOES NOT HAVE PROPER CERTIFICATION.SDR GUUA94057030709ASkin · corrodedDURING FUTHER INSPECTION OF SURFACE CORROSION DISCOVERED SEVERE CORROSION EXTENDS FROM WS 140.00 TO 190.00 APROXIMATELY. CUT OUT DAMAGED AREA AND INSTALLED AN EXTERNAL DOUBLER REPAIR.SDR CA080722007Bushing · missing(CAN) BUSHINGS MISSING FROM WING PICKUP LUGS ON ORIGINAL FRAMES INSTALLED IN ACFT.SDR HALA0800592Stiffener · crackedCRACK ON RIGHT WING FIXED T/E, JUST FORWARD OF O/B AILERON LENGTH WISE STIFFENER. REPAIRED RIGHT WING T/E, JUST FWD OF O/B AILERON STIFFENER PER SRM 51-20-11-OG-0, AND SRM 51-01-OG-0.SDR FDKA200805196Bonding Strap · corrodedBONDING STRAP IS CORRODED ON PANEL 5731. THE CORRODED STRAPS HAVE BEEN REMOVED AND REPLACED.SDR 08FDEA00944Fairing · dentedRT WING FAIRING 634 AT IS DENTED AND DELAMINATED. REPAIRED IAW SRM 57-20-35.SDR C2XA07SH103Access Panel · damagedRT PNL 191FR HAS COMPOSITE DAMAGE AT SCREW HOLES. MAINTENANCE REPAIRED RT PNL 191 FR IAW EC5750-01315. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.SDR C2XA07SH071Plate · corrodedSHV - DURING C-CHECK PANEL 191 BONDING PLATES HAVE CORROSION. MX REMOVED AND REPLACED CORRODED BONDING PLATES ON PANEL 191 IAW EC 5750-01315 REV D. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.SDR RAIA00706039Skin · crackedSTL - DURING INSPECTION, LT WING TRAILING EDGE SKIN WAS FOUND TO HAVE A 1.125 INCH CRACK PROPAGATING FROM RIVET TO TRAILING EDGE NEAR GROUND SPOILER ACTUATOR CUTOUT. MAINTENANCE INSPECTED IAW MANUFACTURER'S SERVICE INFORMATION AND PLACED ON TIME CARRYOVER FORSDR COMA0760258Unknown · unknownFLIGHT 5576 - LEFT WING OVERHEAT ON BEGINNING OF TAKEOFF THRUST. DEFERRED PER MEL 30-12-03-1.SDR QXEA200700545Unknown · damagedC4 PDX - AT LEFT UNDER WING STATION YW222.4 THERE IS AN AREA OF SMALL NICKS. REPAIRED IAW RD8-57-2996 AND SRM 51-20-11.SDR CA070108010Bolt · cracked(CAN) SCHEDULED WING BOLT INSPECTION, NOTED RT UPPER AFT WING BOLT CRACKED ON BOLT HEAD TO SHANK RADIUS. BOLT REPLACED WITH NEW. (TC NR 20070108010)SDR TRAX200601108Hose · twistedBWO 6042035-790 SNAG SHEET C-1026405 NR 2 BRADED STEEL HOSE ON LEFT COLLECTOR TANK FOUND FOULING ON RIB STIFFENER P/N 600-10221-1. RIB BLENDED IAW SRM 57-00-00 SERVICABLE.SDR 06FDEA04075Skin · unknownRT WING L/E SKIN LOWER SIDE SLAT DRIVE MECHANISM ACCESS DOOR CUT OUT AT STA XORS 402 EXISTING SKIN REPAIR. REMOVED EXISTING REPAIR IAW SRM 57-10-00 VOL 1. INSTALLED REPAIR IAW SRM 57-10-00 FIG 68 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER NR N01203 ANDSDR CA061020007Unknown · unknown(CAN) TYPE CERTIFICATE HOLDER (TCH) RECEIVED CALL INDICATING THIS AIRCRAFT WAS IN LEVEL FLIGHT WITH AN INDICATED AIRSPEED OF 120 KNOTS. THE PILOT FELT A VIBRATION IN THE AIRFRAME, LOOKED OUT THE LT WINDOW AND SAW THAT THE LT WING WAS FLUTTERING UP AND DOWN. THSDR 2006UALA01836Skin · crackedNR 3 SLAT LWR EXT SKIN CRACKED AT 3 FASTENERS BELOW ACTUATOR. MAJOR REPAIR: SLAT REPAIRED PER SRM 57-43-01 REPAIR 6.SDR UIEA200600220Fairing · damagedN493MC WAS AT PIK FOR A-2 CHECK. AS PER NON-MEL 06-068 AND N/ROUTINE 41. A HOLE WAS FOUND IN LEADING EDGE OF RIGHT WING BODY FAIRING AT STA 840. INTERIM REPAIR CARRIED OUT AS PER SRM 53-00-70 (NOTE B). TAP TEST ON EVERY CHECK AND PERMANENT REPAIR WILL BE CSDR 2006750001Wing · crackedWING CRACKED, REMOVED AND REPLACED LEFT WING.SDR 06FDEA0842Repair · noneREPAIR LOCATED ON RT WING NR 2 SLAT L/E REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUS INSTALLED REPAIR ON NR 2 SLAT L/E WAS DETERMINED TO BE COMPLIED WITH IAW EA 6-5743-94774 AND S00007 NOV SDR 06FDEA0799Repair · unknownFLUSH REPAIR LT WING NR1 SLAT STA. XORS 60, LE, MARKED NR 93. REPAIR REQUIRES EVALUATION FOR MAJOR/ MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. VISUALLY INSPECTED REPAIR L/W NR 1 SLAT STA. XORS 60 L/E, MARKED NR 93. FOUND TOSDR DHL2006760521Skin · crackedFOUND NR 5 SLAT IB FRAME AT ACTUATOR ROD END ATTACH IS CRACKED IN LOWER FWD RADIUS. REMOVED NR 5 SLAT I/B FRAME AT ACTUATOR ROD END IAW B727 SRM 51-30-2. REPLACED NR 5 SLAT I/B FRAME IAW B727 SRM 51-10-1 AND B727 SRM 51-30-2 P/N 65-17276-11. THIS REPAIR IS SDR 06FDEA0641Skin Panel · unknownFOUND REPAIR LOCATED LT AILERON WS 513-538. LOWER SURFACE. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA0594Repair · unknownDISCREPANCY RIGHT HAND WING L/E SLAT TRACK NR 10 CUT OUT ON LOWER SKIN HAS AN EXTERNAL DOUBLER REPAIR AT STA XOS 657 DIM. 7.5" X 5" CORRECTIVE ACTION R/R REPAIR IAW SRM 57-10-00 FIG 68 VOL 1 FABRICATED PART IAW DETAIL PART TRAVELER N01213 AND SRM 57-10-SDR 06FDEA0586Repair · unknownFOUND REPAIR LOCATED ON UPPER SURFACE OF LEFT WING AFT OF NR 4 L/E FLAP, STA 410. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA0585Repair · unknownFOUND 2 REPAIRS LOCATED ON UPPER SURFACE OF RT WING AFT OF NR 6 L/E, STA 546. REPAIRS REQUIRE EVALUATION FOR MAJOR MINOR DETERMINATION AND IF REPAIRS WERE ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA0584Repair · unknownFOUND REPAIR ON LEFT I/B FORE FLAP UPPER SURFACE. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA0583Repair · unknownFOUND REPAIR ON RIGHT OUTBOARD FORE FLAP L/E REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.SDR 06FDEA0567Repair · noneFOUND PREVIOUSLY REPAIR INSTALLED AT R/H WING LEADING EDGE 12 INCHES OUTBD OF LANDING LIGHT WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 57-30-4, FIG 2, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE AND SIZE, MATERIAL TYPE AND THICKNESSDR 06FDEA0563Repair · noneFOUND PREVIOUSLY REPAIR INSTALLED AT RIGHT WING LEADING EDGE, ON FRAME OF LANDING LIGHT WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 57-10-4 FIG. 4, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FAST
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