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 n_number = 'N466SW' 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 n_number = 'N466SW' 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 SWIA2026040976354Fitting · gougedLEFT WING REAR SPAR AT WS162.49 HAS A FITTING GOUGED & DAMAGED. REMOVED, REPLACED, AND INSTALLED FITTING ON LT WING REAR SPAR AT WS 162.49 IAW SRM 57-51-14,51-40-11,51-21-11,51-25-06,51-25-16,51-42-06, & 51-42-20,51-23-00.SDR SWI2025F00644Bracket · looseAFTER SELECTING GEAR LEVER UP, GEAR DISAGREE MESSAGE CAME ON AND RAN QRH BUT MESSAGE PERSISTS AND RETURNED TO IAH TO LAND. (FLIGHT 5297 - FILED CLOSED)PLEASE REFERENCE AML 1606345 FOR FDR DOWNLOAD. PER FDR ANALYSIS. RH MLG NEVER REGISTERED IN THE UPLOCK POSITISDR SWI2025F00066Electrical Sys · power lossCOMPLETE LOSS OF AC POWER IN FLIGHT. ADG DEPLOYED AUTOMATICALLY. POWER LOSS OCCURRED WHILE SELECTING FLAPS 8. RAN QRC/QRH AND RESTORED ALL AC POWER. NORMAL LANDING AND TAXI IN. (FLIGHT 5333) REFERENCE AML 1512638, AML 1512639, AML 1512641, AML 1512642, AMLSDR SWIA202501130Electrical Sys · power lossCOMPLETE LOSS OF AC POWER IN FLIGHT. ADG DEPLOYED AUTOMATICALLY. POWER LOSS OCCURRED WHILE SELECTING FLAPS 8. RAN QRC/QRH AND RESTORED ALL AC POWER. NORMAL LANDING AND TAXI IN. (FLIGHT 5333 - FILED CLOSED) PLEASE REFERENCE AML 1512638 PLEASE REFERENCESDR SWIA202501105Electrical Sys · power lossCOMPLETE LOSS OF AC POWER IN FLIGHT. ADG DEPLOYED AUTOMATICALLY. POWER LOSS OCCURRED WHILE SELECTING FLAPS 8. RAN QRC/QRH AND RESTORED ALL AC POWER. NORMAL LANDING AND TAXI IN. (FLIGHT 5333 - FILED OPEN)SDR SWIA2024091900006Frame · crackedFOUND 2 CRACKS AND SKIN OIL CANNING ON CENTER FRAME SECTOR P/N 600-34014-277 LOCATED OFF FS235.00 AND BETWEEN STGR-26L AND STGR-26R AFT OF NLG. THIS HAS BEEN CLASSIFED AS A MAJOT REPAIR. FORM M-337 INITIATED. (FILED CLOSED) PERFORMED SHORING OF THE AIRCRSDR SWIA2024090900800Skin · crackedFOUND 2 CRACKS AND SKIN OIL CANNING ON CENTER FRAME SECTOR P/N 600-34014-277 LOCATED OFF FS235.00 AND BETWEEN STGR-26L AND STGR-26R AFT OF NLG. THIS HAS BEEN CLASSIFED AS A MAJOT REPAIR. FORM M-337 INITIATED. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGSDR SWIA202405200017Skin · dentedCOMPLY WITH REPAIR FOR TEMPORARYREO 601R-52-11-3014 (DENTS TO PASSENGER DOOR OUTER SKIN BETEEN FS338.963-FS347.250 ABOVE DATUM LINE #1). (FILED CLOSED)COMPLIED WITH PERMANENT REPAIR ON PAX DOOR OUTER SKIN. PER REO 601R-52-11-3015 PRELIMINARY P1 REV -(P1) DATSDR SWIA2024052000014Door · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA90491-REO 601R-52-11-3014 MXCODEID74202-PR - MAIN CABIN DOOR HIT THE RAMP. COMPLIED WITH TEMPORARY REPAIR PER REO 601R-52-11-3014. FINAL REPAIR DUE WITHIN 100FH REF REO 601R-52-11-3014., PART NUMBER: - , SERIAL NUMBSDR SWIA20230410Unknown · crackedCRACK IN FORWARD PRESSURE BULKHEAD AT PARKING BRAKE ROD THROUGH HOLE. THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR, FORM M-337 WILL BE REQUIRED. (FILED CLOSED) APPLIED REPAIR DOUBLER TO FORWARD PRESSURE BULKHEAD AT PARKING BRAKE ROD THROUGH HOLE IN REF. TOSDR SWIA2023041100001Unknown · crackedCRACK IN FORWARD PRESSURE BULKHEAD AT PARKING BRAKE ROD THROUGH HOLE. THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR, FORM M-337 WILL BE REQUIRED. (FILED OPEN)SDR SWIA2023020007None · crackedDURING AUDIT OF TRU BAY SUSPECTED CRACK REPAIR FOUND REPAIR ANGLE -3 AND REPAIR DOUBLER -2 FABRICATED USING WRONG MATERIALS PER REO 601R-53-11-111 (C-CHECK RO 2/26/2023) UPON FURTHER INVESTIGATION FOUND -3 ANGLE WAS FABRICATED USING CORRECT MATERIAL ANSDR SWIA202301026None · corrodedLEFT FLOOR SILL FS349.00 - 364.00 HAS AN AREA OF CORROSION. (MARKED) (C-CHECK RO 2/26/2023) REPAIRED LH FLOOR SILL AT FS 349.00 -364.00 REF REO 601R-53-21-3601 REV -- DATE 2023-02-08. ALL STEPS OF REO COMPLIED WITH, SEE CONTINUE CARD FOR DETAILS. M337 SDR SWIA2023010026None · corrodedSEAT TRACK FS379.00 - 400.00 RBL9 HAS CORROSION. (C-CHECK RO 2/26/2023) REPLACED NEW SEAT TRACK AT RBL9 BETWEEN FS364.00 - FS409.00 REF CRJ200 AMM 53-01-11SDR SWIA20230100126None · corrodedRIGHT HAND PRESSURE FLOOR SEAT RAIL BETWEEN FS409.0+128 TO FS559.0, CORRODED AND GOUGED IN SEVERAL PLACES OF THE RAIL SECTION. (C-CHECK RO 2/26/2023) INSTALLED NEW SEAT RAIL BETWEEN FS 409.00 +128 AND FS 559.00 +5 PER FCRJ 200 AMM 53-01-11-400-802 AND SDR SWIA20230124None · corrodedL/H FLOOR SILL SHOWS EVIDENCE OF CORROSION IN MULTIPLE AREAS (MARKED) (C-CHECK RO 2/26/2023) CORROSION BLENDED OUT IN MARKED AREAS AND FOUND WITHIN LIMITS PER REO 601R-53-41-666 REV. -C, DATED 2012-11-06. 2EA FASTENERS WERE REPLACED WITH ALTERNATES AT SDR SWIA202301023None · damagedFRETTING ON WING PLANK AT ACCESS HOLE PANEL LANDING FOR FUEL PANEL 510AB (C-CHECK RO 2/26/2023) BLENDED WITHIN LIMITS, WING PLANK LANDING FOR 510AB PANEL REF REO 601R -57-21-030 REV L DATED 2014-02-05ORIGINAL MATERIAL 0.182" , REMAINING 0.179", REMOVEDSDR SWIA20230118None · crackedNLG WHEEL WELL CUTOUT - EXTERNAL SKIN - AFT L/H CORNER HAS SUSPECTED CRACK - FS 235 LBL 6 (C-CHECK RO 2/26/2023) COMPLIED WITH THE REPAIR FOR AFT L/H CORNER OF NLG WHEEL WELL CUTOUT. REF REO 601R-53-11-048 REV-D DATED 2015-06-10 AND REO 601R-53-11-3824 SDR SWIA2023010018None · crackedRH FWD DRAIN HOLE AFT ATTACH HOLE CRACKED AT 2 O'CLOCK POSITION AND RH AFT DRAIN HOLE BY BOOST PUMP AFT ATTACH HOLE CRACKED AT 9 O'CLOCK (C-CHECK RO 2/26/2023) : REPAIRED R/H FWD DRAIN HOLE AFT ATTACH HOLE BY OPENING UP THE DAMAGED HOLE AND REAMING PER SDR SWIA2023010017None · crackedAFT EQUIPMENT BAY - CLEAT SECURING INTERCOSTAL AT STGR 14L TO FRAME @ FS 625 CRACKED (C-CHECK RO 2/26/2023) REMOVED AND INSTALLED NEW AFT EQUIPMENT BAY - CLEAT/ INTERCOSTAL P/N 601-35012-52 AT STGR 14L TO FRAME @ FS 625 REF CRJ200 SRM 51-42-21 AND DWG 6SDR SWIA2023010016None · corrodedCABIN - L/H FLOOR SILL, JUST AFT OF FRAME @ FS 439, SHOWS EVIDENCE OF CORROSION AROUND NUTPLATE HOLE (C-CHECK RO 2/26/2023) REMOVED CORROSION FROM LH PRESSURE FLOOR SILL JUST AFT OF FRAME @ FS 439 REF REO 601R-53-41-666, REV -C, DATED: 2012-11-06, 1.2 DSDR SWIA20230113None · gougedLEFT AILERON - UPPER LEADING EDGE SKIN INNER SURFACE BETWEEN THE PCU ATTACHING LUGS IS GOUGED. (MARKED) (C-CHECK RO 2/26/2023) LH UPPER AILERON LEADING EDGE SKIN OUT OF LIMITS, REPLACED WITH NEW AILERON UPPER LEADING EDGE SKIN REF. CRJ200 SRM 51-42-06 ASDR SWIA2023010012None · corrodedINTERCOSTAL AT DD3 CENTER HAS CORROSION AROUND LIGHTNING HOLE. (C-CHECK RO 2/26/2023) REPLACED WITH NEW SERVICEABLE DD3 INTERCOSTAL (P/N 601R31056-1S) ONTO PAX DOOR USING ALL NEW FASTENERS. REF BOMBARDIER DWG# 601R31702 REV N AND CRJ200 SRM 51-42-06 RESDR SWIA2023011001None · chafed*RH LOWER WING PLANK AT FS513.00 WS45.0 HAS CHAFFE DAMAGED FROM THE BODY FAIRING (MARKED) (C-CHECK RO 2/26/2023) BLENDED WITHIN LIMITS ZONE A (**), ORIGINAL MATERIAL THICKNESS 0.300", REMAINING 0.296", MATERIAL REMOVED 0.004"REF REO 601R-57-21-3692, RSDR SWIA202301000011None · corroded*PAX DOOR AFT OUTER FORMER CORRODED UNDER PANEL 832GR (MARKED) (C-CHECK RO 2/26/2023) REPLACED PAX DOOR AFT FORMER REF CRJ 200 SRM 51-42-06 AND DRAWING 601R31702 REV N. M337 AND SKYWEST TASK CARD 51-900-1003-SKY COMPLIED WITH. SEE CONTINUE CARD FOR DETASDR SWIA20230100005None · damagedREAR PRESSURE BULKHEAD FORWARD FACE - SIX OF THE PICKET FENCE REPAIR PLATES HAVE DAMAGE FROM LINER SCREWS WL103.00. (MARKED) (C-CHECK RO 2/26/2023) COMPLIED WITH REO 601R-53-61-7951 REV-- DATED 2023-01-22 FOR REAR PRESSURE BULKHEAD FORWARD FACE REPAIR MSDR SWIA20230100003None · crackedSUSPECTED CRACK ON THE LH TRU BAY AT APPROX. FS.202 ON CORNER RADIUS (MARKED) (C-CHECK RO 2/26/2023) COMPLIED WITH REPAIR FOR CRACKED L/H TRU BAY REF CRJ 200 SRM 51-42-06 REV 39, DATED: MAR 10/21 AND REO 601R-53-11-111 REV NC DATE 98-MAR-18, COMPLIED WISDR SWIA202266604None · crackedFS280 BEAM, FWD FLOOR SUPPORT ANGLE BETWEEN LBL9 & RBL9, CRACKS IN RADIUS ON BOTH ENDS. (FILED CLOSED) REMOVED AND REPLACED FWD FLOOR SUPPORT ANGLE BETWEEN LBL9 AND RBL9 IN REFERENCE TO SRM 51-42-06.SDR SWIA202266603None · crackedFS280 BEAM, AFT FLOOR SUPPORT ANGLE REPAIR SPLICE, OB OF RBL9, CRACK IN RADIUS ON IB END. (FILED CLOSED) FABRICATED REPAIR SPLICE PER SRM 53-21-43. REMOVED AND REPLACED FS280 BEAM, AFT FLOOR SUPPORT ANGLE REPAIR SPLICE, OB OF RBL9 IAW SRM 51-42-21SDR SWIA202266602None · crackedFS280 BEAM/FLOOR SUPPORT BEAM CLIP, OB, RBL9, IS CRACKED IN RADIUS, UPPER END. (FILED CLOSED) FABRICATED BEAM CLIP PER SRM 53-21-43. REMOVED AND REPLACED FS280 BEAM/FLOOR SUPPORT BEAM CLIP, OB, RBL9, IAW SRM 51-42-21SDR SWIA202266601None · crackedFS280 BEAM/FLOOR SUPPORT BEAM CLIP, IB, RBL9, IS CRACKED IN RADIUS, UPPER END. (FILED CLOSED) FABRICATED BEAM CLIP PER SRM 53-21-43. REMOVED AND REPLACED FS280 BEAM/FLOOR SUPPORT BEAM CLIP, IB, RBL9, IAW SRM 51-42-21SDR SWIA202265646None · damagedRH OVERWING EMERGENCY EXIT WINDOW SCRATCHED BEYOND LIMITS. (FILED - CLOSED) REMOVED & REPLACED RH OVERWING EMERGENCY EXIT WINDOW IN REFERENCE TO APPLICABLE STEPS IN AMM 56-21-01. REMOVED WINDOW MFG DATE: 08-02SDR SWIA2020071451326Actuator · failedGEAR DISAGREE ON LANDING WHEN SELECTED. COMPLIED WITH QRH AND MESSAGE CLEARED. INDICATION WAS RIGHT MAIN LANDING GEAR. FLIGHT 5253 - FILED CLOSED. REFERENCE CP 21230240 FOR INSPECTION OF THE RT MLG UPLOCK ASSEMBLY. REFERENCE CP 2123043 FOR INSPECTION OF TSDR SWIA2020020648244Frame · cracked* FRAME AT FS 333.0 STR 2L IS CRACKED (C-CHECK) RO 2/04/2020 REPAIRED FRAME AT FS 333.0 STR 2L REF BOMBARDIER DWG, CRJ200 SRM AND CRJ200 SRM. LEAK CHECK GOODSDR SWIA2020020648243Frame · corrodedF.S. 333 FRAME HAS CORROSION ON FWD> AND AFT SIDE AS MARKED IN RED IN AVIONICS BELLY AREA (C-CHECK) RO 2/04/2020 REPAIRED F.S. 333 FRAME REF CRJ200 SRM, CRJ200 SRM, AND BOMBARDIER DWG. LEAK CHECK GOODSDR SWIA2020020648242Mount · corrodedGALLEY INBD. AFT FLOOR MOUNT AT APROX. RBL 9 EXFOLIATED (C-CHECK) RO 2/04/2020 REMOVED AND REPLACED GALLEY INBD. AFT FLOOR MOUNT AT APROX. RBL 9 REF BOMBARDIER DWG AND CRJ200 SRM. SEE CONTINUE CARD FOR DETAILS. SEE ATTACHED TASK.SDR SWIA2020020648241Floorbeam · cracked280 BEAM LBL 9 CRACKED CLIP AT UPPER ANGLE (C-CHECK) RO 2/04/2020 REMOVED AND REPLACED FS280, LBL9 CLIP REF CRJ200 SRM. AND USED BOMBARDIER REO FOR MATERIAL ID AND FASTENER CALL OUT ONLY. SEE CONTINUE CARD FOR DETAILS. SEE ATTACHED TASK.SDR SWIA2020020648240Floor Support · corroded* RIGHT PRESSURE FLOOR SILL PANEL FROM FS 409+128 O FS 559.0 HAS SEVERAL AREAS OF CORROSION (C-CHECK) RO 2/04/2020 REPAIRED RIGHT PRESSURE FLOOR SILL CORROSION L FROM FS 409+128 TO FS 559.0 REF REO. LEAK CHECK GOOD.SDR SWIA2020020648239Floor Support · corroded* LEFT PRESSURE FLOOR SILL PANEL FROM FS 409+128 O FS 559.0 HAS SEVERAL AREAS OF CORROSION (C-CHECK) RO 2/04/2020 REPAIRED LEFT PRESSURE FLOOR SILL PANEL FROM FS 409+128 O FS 559.0 REF REO. LEAK CHECK GOODSDR SWIA2020020648238Frame · corroded* FRAME AT FS 574.0 FWD SIDE HAS CORROSION IN THE AREA OF STR 26L TO 26R (C-CHECK) RO 2/04/2020 REPAIRED FRAME AT FS574 BETWEEN STR26L AND STR26R PER REO.SDR SWIA2020020648237Frame · corroded* FRAME AT FS 589.0 FWD SIDE HAS CORROSION IN THE AREA OF STR 26L TO 26R (C-CHECK) RO 2/04/2020 REPAIRED FRAME AT FS589 BETWEEN STR26L AND STR25R PER REO.SDR SWIA2020020648236Post · damagedF.S 409+128 BL 0.0 DEFECTS NOTED AT LH / RH AFT RADIUS OF VERTICAL POSTS. (C-CHECK) RO 2/04/2020 REPLACED LH/RH VERTICAL POSTS AND 2EA CLIPS @ FS409.00 + 128 BL0.0. REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-22, BOMBARDIER DWG 601R32208 REV-T, AND BOMBARDIESDR SWIA2020020648235Frame · corroded* FRAME AT FS 605.0 FWD SIDE HAS CORROSION IN THE AREA OF STR 26L TO 26R (C-CHECK) RO 2/04/2020 REPAIRED FRAME AT FS605 BETWEEN STR26L AND STR26R PER REO.SDR SWIA2020020648234Shim · migratedSIX LOOSE BOLTS ( 3 OTBD R/H & 3 OTBD L/H ) AND MIGRATED SHIMS FOUND ON THE HORIZONTAL STABILIZER STEADY FITTING. (C-CHECK) RO 2/04/2020 REPAIRED HORIZONTAL STEADY FITTING, REAMED HOLES AND INSTALLED NEW FASTENERS REF CRJ 200 REO. OPS AND GAP CHECKS GOOSDR SWIA2020020648250Doubler · corroded*DOUBLER ON PASSENGER DOOR FRAME, FS349.00 STGR18L, IS CORRODED. (MARKED) (C-CHECK) RO 2/04/2020 REMOVED AND BLENDED OUT CORROSION IS WITHIN LIMITS AT PAX DOOR FRAME DOUBLER, FS349.00 STGR18L. REF. CRJ 200 SRM, SRM(SEE DETAILS FOR CORRECTIVE ACTION)SDR SWIA2020020648233Door Sill · gouged*PASSENGER DOOR UPPER SILL GOUGED, 4 PLACES, UNDER THE CEILING PANEL ATTACH POINTS FS310.00 Ï¿½ FS349.00. (C-CHECK) RO 2/04/2020 BLENDED OUT GOUGE DAMAGE TO PAX DOOR UPPER SILL DOUBLER AT STR3L BETWEEN FS310.00 - FS349.00 IS STRUCTURALLY ACCEPTABLE. COMPLISDR SWIA2020020648232Door Sill · corroded*PASSENGER DOOR SILL ANGLE HAS CORROSION AT MULTIPLE AREAS AND EXFOLIATION THRU THE ANGLE AT THE DOOR CLOSED SENSOR. (MARKED) (C-CHECK) RO 2/04/2020 PAX DOOR SILL ANGLE IS OUT OF LIMITS PER REF CRJ 200 SRM, REMOVED AND REPLACED PAX DOOR SILL ANGLE WITH NEWSDR SWIA2020020648249Anchor Fitting · corroded* AFT PASS DOOR ANCHOR FITTING HARDWARE RUSTED AND CORRODED MARKED (C-CHECK) RO 2/04/2020 REPLACED PASSENGER DOOR AFT COUNTERBALANCE ANCHOR FITTING. REF CRJ200 AMM TASK.SDR SWIA2020020648248Plate · corroded* AFT SERRATED PLATE CORRODED MARKED (C-CHECK) RO 2/04/2020 REPLACED WITH NEW PAX DOOR AFT COUNTERBALANCE ANCHOR FITTING SERRATED PLATE REF CRJ 200 AMM.SDR SWIA2020020648231Skin · gouged* APU EXHAUST CUTOUT EXTERIOR SKIN Ï¿½ GOUGES AND EDGE DAMAGE ON AFT SIDE OF CUTOUT (MARKED). (C-CHECK) RO 2/04/2020 REMOVED DAMAGE ON APU EXHUAST CUTOUT EXTERIOR SKIN, REF CRJ 200 SRM. SKIN IS WITHIN LIMITS PER BOMBARDIER REO. SEE CONTINUATION CARD FOR DE
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