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 = 'N783SW' 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 = 'N783SW' 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 SWAA2023091901688Floor Panel · crackedFWD CARGO COMPARTMENT FLOOR PANEL IS CRACKED<[01] OKAY TO CONTINUE PER MEL 25-16-01 SP1B FWD BIN TO REMAIN EMPTY;[02] REMOVED AND REPLACED CRACKED FLOOR PANEL FROM FWD CARGO COMPATMENT PER 25-52-10. MEL CLEARED SP1B.SDR SWAA2023061959937Girt Bar · out of positionGIRT BART LOCATED AT THE R2 AFT GALLEY DOOR IS HANGING OUT OF POSITION<[01] REPOSITIONED GIRT BAR AS REQD. AMM 25-66-01<BR>R2 DOORSDR SWAA2023061658972Handle · looseFWD ENTRY DOOR UPPER ASSIST HANDLE LOOSE<[01] ADJUSTED FWD ENTRY DOOR ASSIST HANDLE PER AMM 52-11-31-000-802SDR SWAA2023060956455Battery Pack · inoperativeFWD LH EMERGENCY LIGHT BATTERY INOP.<[01] REMOVED AND REPLACED FWD LH EMERGENCY LIGHT BATTERY PACK REF: AMM 33-51-06.SDR SWAA2023042730410Floor Panel · crackedFWD CARGO AFT FLOOR PANEL HAS A CRACK 9.5 INCHES IN LENGTH<[01] REMOVED AND REPLACED FWD CARGO AFT FLOOR PANEL IAW AMM 25-52-10.SDR SWAA2023021502479Tailpipe · fireENGINE TAILPIPE FIRE @ 75KTS DURING T/O ON NO 1 ENG REJECTED T/O ; PERFORMED QRH PROCEDURES .FLAMES WERE REPORTED FROM ANOTHER A/C AND TOWER RAN BRAKE COOLING ON PWB TAXI TO GATE NORMALLY FIRE TRUCKS CLEARED US TO GATE RAN COOLING FOR APPROX 3 MINUTES PRIOR TOSDR SWAA2022120979977Slide · out of positionSTBD AFT A/C SERVICE DOOR SLIDE PULL HANDLE VISIBLE AND EXPOSED WHEN DOOR IS ARMED. REPOSITIONED MANUAL HANDLE COVER FOR AFT SERVICE DOOR ESCAPE SLIDE IAW AMM 25?66-01. OPS CHECKS NORMAL.SDR SWAA2022102765082Flashlight · inoperativeFA FOUND FWD GALLEY UPPPER EMER FLASHLIGHT NOT BLINKING / [01] R&R EMER FLASHLIGHT PER AMM 25-64-00SDR SWAA2022090649795Slide · lowFORWARD RIGHT SERVICE DOOR SLIDE INDICATOR GAUGE SHOWING LOW. SLIDE PART REQUEST IS BUILT INTO THE SUBTASK / [01] R&R?D FWD SERVICE (R1)DOOR EMERGENCY ESCAPE SLIDE PER MT 725-61-06-FSSDR SWAA2022060111139Web · crackedRIGHT WING TRAILING EDGE DEFLECTION CONTROL RIB PANEL SUPPORT WEB CRACKED AT OUTBOARD ATTACH FASTENER HOLE. REMOVED DAMAGE WEB ANGLE AT R/H WING TRAILING EDGE DEFLECTION CONTROL PANEL PER REF B737-700 SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW PART WED ANGLE SDR SWAA2022060111136Support Angle · crackedRIGHT WING TRAILING EDGE DEFLECTION CONTROL RIB PANEL SEAL SUPPORT ANGLE CRACKED AT WEB ATTACH POINT. REMOVED DAMAGE SEAL SUPPORT ANGLE AT R/H WING TRAILING EDGE DEFLECTION CONTROL PANEL PER REF B737-700 SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW PART WEB ANGLSDR SWAA2022060111137Support Angle · crackedLEFT WING DEFLECTION CONTROL RIB PANEL VERTICAL SEAL SUPPORT ANGLE CRACKED AT THE FORWARD SIDE OF WEB. / [01] REMOVED AND REPLACED SEAL SUPPORT ANGLE AT FWD SIDE OF WEB ON L/W DEFLECTION CONTROL PANEL PER REF B737-700 SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1.SDR SWAA2022030279163Light · missingEMERGENCY EXIT LIGHT LENS NOT INSTALLED AT R2 DOOR / [01] REMOVED & REPLACED EMERGENCY EXIT LIGHT ASSY; AT R2 DOOR; PER AMM 33-51-01.SDR SWAA2022021472148Sensor · faultyCREW REPORTED FLAP LOCK OUT ON LANDING ; / [01] REPLACED SLAT #1 INBOARD PROXIMITY SENSOR PER AMM 27-88-11; OPS CHECK GOOD.SDR SWAA2021110832157Girt Bar · out of positionL-1 DOOR GIRT BAR HITTING AFT DOOR CUTOUT (WHEN OPENING DOOR) ; / [01] REMOVED R1 DOOR SLIDE REF MT 725-61-06; [02] REPOSITIONED GIRT BAR FOR L1 DOOR REF B737 MM 25-66-01-400-803; [03] REMOVED L1 DOOR SLIDE REF MT 725-61-06; [04] EDIT WORK CAPTURE STEP 1 (& 3)SDR SWAA2021110832154Girt Bar · out of positionR-1 DOOR GIRT BAR HITTING DOOR CUTOUT WHEN CLOSING ON AFT CORNER ; / [01] REMOVED R1 DOOR SLIDE REF MT 725-61-06; [02] REPOSITIONED GIRT BAR FOR R1 DOOR REF B737 MM 25-66-01-400-803; [03] OK TO INSTALL R1 DOOR SLIDE.; [04] REINSTALLED R1 DOOR SLIDE REF MT 725-SDR SWAA2021102832155Bulb · inoperativeL-1 DOOR UPPER EMERGENCY LIGHT WITH 2EA BULBS INOP ; / [01] RECITED BULBS (2EA) AT L-1 DOOR UPPER EMERGENCY LIGHT AS PER REF B737 AMM 33-51-01-960-801 PERFORMED OPERATIONAL TEST FOUND NORMAL; [02] VERIFIED STEP 1SDR SWAA2021110831031None · poppedPASSENGER CABIN LIGHTING EMERGENCY CHARGER FWD C/B POPPING AT P18. ; PASSENGER CAIN LIGHTING EMERGENCY CHARGER FWD CB POPPING AT P18. / [01] PERFORMED TROUBLESHOOTING PASSENGER CABIN LIGHTING CHARGER FWD C/B AS PER WDM 33-51-11; FOUND BATTERY CHARGER M1875 AT SDR SWAA2021110831030Light · inoperativeOVERHEAD BIN EMERGENCY LIGHT INOP BY ROW 4 LH ; OVERHEAD IN EMERGENCY LIGHT INOP Y ROW 4 LH / [01] RE-SECURED CONNECTOR D11090 IN AISLE LIGHT L1065; AS PER REFERENCE B737 WDM 33-51-12; PERFORMED OPERATIONAL TEST AS PER REFERENCE B737 AMM 33-51-00-710-801; NORMSDR SWAA2021110929830Scuff Plate · crackedFWD CARGO FWD SCUFF PLATE CRACKED ; / [01] RECEIVED WELDED SCUFF PLATE ON TAG #397070; ISSUE TAG #HZ896; P.O.#1734696. WILL BE INSTALLED ON CARD 3 # TTG8Q004G7HY; [02] VERIFIED STEP 1SDR SWAA2021110826978Floor Panel · delaminatedFOUND PANEL 212DC DELAMONATE AT CORNER ; / [01] PREPARED FOR REPAIR AT PANEL 212 DC AS PER B737-700-SRM 51-70-06-2R-6; [02] VERIFIED STEP 1. OK TO INSTALL REPAIR.; [03] ACCOMPLISHED REPAIR OF DELAMINATION OF THE EDGEBAND OF HONEYCOMB OF FLIGHT DECK CEILING PANSDR SWAA2021110826221Seat Track · corrodedFOUND FIRST OFFICER FWD I/B AND O/B SEAT TRACKS WITH CORROSION ; / [01] 1ST OFFICER FWD I/B AND O/B SEAT TRACKS WERE REMOVED ON TASKCARD TTG8Q0036K60.; [02] VERIFIED STEP 1. OK TO INSTALL NEW FWD SEAT TRACKS.; [03] INSTALLED NEW 1ST OFFICER FWD I/B AND O/B SEASDR SWAA2021110826222Seat Track · corrodedFOUND CAPTAIN FWD I/B AND O/B SEAT TRACKS WITH CORROSION ; / [01] RECEIVED CAPTAIN FWD I/B AND O/B SET TRACKS TO BE INSTALLED ON CARD TTG8Q0036K4C; [02] RECEIVED CAPTAIN FWD I/B AND O/B SET TRACKS TO BE INSTALLED ON CARD TTG8Q0036K4CSDR SWAA2021110924748None · corrodedCORROSION.>>>>>VERTICAL FIN FWD R/H ATTACHMENT FITTING LUGS STA 1016 INNER BORE EVIDENCE OF PITTI CORROSION. ; / [01] REMOVED CORROSION ON VERTICAL FIN FWD R/H ATTACHMENT FITTING LUGS STA. 1016 PER REF. 737 SRM 51-10-02-0G-0; BY REAMING HOLE TO FINAL SIZE; 1.0SDR SWAA2021110924747None · corrodedCORROSION >>>>>>>VERTICAL FIN FRONT SPAR R/H FITTING LUG HAVE SIGN OF PITTI CORROSION AT INNER BORE. ; / [01] REMOVED CORROSION ON VERTICAL FIN FRONT SPAR R/H FITTING LUG; PER REF. 737 SRM 51-10-02-0G-0; BY REAMING HOLE TO FINAL SIZE ; 1.040 (0N VERTICAL); [02SDR SWAA2021110924746None · corrodedCORROSION >>>>>>>VERTICAL FIN FRONT SPAR L/H FITTING LUG HAVE SIGN OF PITTI CORROSION AT INNER BORE. ; / [01] REMOVED CORROSION ON VERTICAL FIN FRONT SPAR L/H FITTING LUG ; PER REF. 737 SRM 51-10-02-0G-0; BY REAMING HOLE TO FINAL SIZE ; 1.040;( ON VERTICAL); [SDR SWAA2021110919709Skin · corrodedAFT UPPER FUSELAGE AT STA 1016 - STA 1088 STR 3L - STR 3R WL 308.5 HAS SURFACE CORROSION. REMOVED CORROSION ON UPPER FUSELAGE FROM BS 1016 TO 1088, BETWEEN STRINGER 3L AND 3R, WL 308.5 IAW SRM 51-10-02-0G-0. NO MATERIAL LOST AREAS WITHIN LIMITS IAW SRM 53-00SDR SWAA2021110820614Angle · crackedCABIN PASSENGER STATION 616 LBL 60 CRACK AT FASTENER HOLE ; / [01] INSTALLED EWIS PROTECTION AT LT SIDE BETWEDN STA 540 TO 639 REF B737-7 AMM 20-60-07-913-801; [02] REMOVED CABIN PASSENGER INNER CHORD CREASE BEAM AT LT SIDE LBL 60 FROM STA 530 TO STA671 REF B7SDR SWAA2021110819715Angle · crackedCABIN PASSENGER STATION 616 LBL 60 CRACK AT FASTENER HOLE ; / [01] INSTALLED EWIS PROTECTION AT LT SIDE BETWEDN STA 540 TO 639 REF B737-7 AMM 20-60-07-913-801; [02] REMOVED CABIN PASSENGER INNER CHORD CREASE BEAM AT LT SIDE LBL 60 FROM STA 530 TO STA671 REF B7SDR SWAA2021110920599None · corroded>>> CORROSION >> VERTICAL STABILIZER; RIGHT FRON SPAR FITTING PITTING CORROSION ; / [01] REMOVED BUSHING AT VERTICAL STABILIZER RIGHT FRONT SPAT FITTING AS PER B737-700 SOPM 20-50-03; [02] REMOVED CORROSION AT VERTICAL STABILIZER RIGHT FROM SPAR FITTING REF B7SDR SWAA2021110920598None · corroded>>> CORROSION >> VERTICAL STABILIZER ; LEFT FRON SPAR FITTING CORROSION ; / [01] REMOVED BUSHING AT VERTICAL STABILIZER LEFT FRONT SPAR FITTING AS PER B737-700 SOPM 20-50-03; [02] REMOVED CORROSION AT VERTICAL STABILIZER LEFT FROM SPAR FITTING REF B737-7 SRM 5SDR SWAA2021110920597None · corroded>>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; LEFT FRON SPAR FITTINGS CORROSION ; / [01] REMOVED BUSHINGS AT VERTICAL STABILIZER CENTER SECTION LEFT FRONT SPAR AS PER B737-700 SOPM 20-50-03; [02] REMOVED CORROSION AT VERTICAL FIN LT FITTING REF B737-7 SSDR SWAA2021110919708Fitting · corroded>>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; RIGHT O/B REAR SPAR FITTINGS PITTING CORROSION ; /SDR SWAA2021110919702Fitting · corroded>>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; LEFT O/B REAR SPAR FITTINGS CORROSION ; /SDR SWAA2021110919701Fitting · corroded>>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; LEFT I/B REAR SPAR FITTINGS CORROSION ; /SDR SWAA2021110919700Fitting · corroded>>> CORROSION >> VERTICAL STABILIZER; RIGHT FRON SPAR FITTING PITTING CORROSION ; /SDR SWAA2021110919699Fitting · corroded>>> CORROSION >> VERTICAL STABILIZER ; LEFT FRON SPAR FITTING CORROSION ; /SDR SWAA2021110919698Fitting · corroded>>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; LEFT FRON SPAR FITTINGS CORROSION ; /SDR SWAA2021110920602Fitting · corroded>>> CORROSION >> VERTICAL STABILIZER ; RIGHT I/B REAR SPAR FITTINGS PITTING CORROSION ; / [01] REMOVED BUSHINGS AT RIGHT VERTICAL STABILIZER I/B REAR SPAR AS P[ER B737-700 SOPM 20-50-03; [02] AFTER BUSHING REMOVAL ; INSPECTED AREA AT VERTICAL STABILIZER; RIGHTSDR SWAA2021110920607Fitting · corroded>>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; RIGHT I/B REAR SPAR FITTINGS PITTING CORROSION ; / [01] EA EA-GENERAL (EA ATTACHED TO AN AIRCRAFT FAULT); [02] EA EA-GENERAL (EA ATTACHED TO AN AIRCRAFT FAULT); [03] ISSUED SUMMARY EA 21-153-02759; [04] C/WSDR SWAA2021110920604Fitting · corrodedVERTICAL STABILIZER LEFT I/B REAR SPAR FITTINGS CORRODED. REMOVED BUSHINGS AT LEFT VERTICAL STABILIZER I/B REAR SPAR AS PER B737-700 SOPM 20-50-03, AFTER BUSHING REMOVAL, INSPECTED AREA, NO CORROSION FOUND. INSTALLED SERVICEABLE BUSHINGS SOPM 20-50-03 AND SDR SWAA2021110920600Fitting · corroded>>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; LEFT I/B REAR SPAR FITTINGS CORROSION ; / [01] PERFORMED CORRECTIVE ACTION ON BARCODE TTG8Q006LXMS. REF FAULT TTG8Q006KMKF; [02] PERFORMED CORRECTIVE ACTION ON BARCODE TTG8Q006LXMS. REF FAULT TTG8Q006KMKFSDR SWAA2021110920601Fitting · corroded>>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; LEFT O/B REAR SPAR FITTINGS CORROSION ; / [01] PERFORMED CORRECTIVE ACTION ON BARCODE TTG8Q006LXMS. REF FAULT TTG8Q006KMKF; [02] PERFORMED CORRECTIVE ACTION ON BARCODE TTG8Q006LXMS. REF FAULT TTG8Q006KMKFSDR SWAA2021110920606Fitting · corroded>>> CORROSION >> VERTICAL STABILIZER CENTER SECTION; RIGHT O/B REAR SPAR FITTINGS PITTING CORROSION ; / [01] PERFORMED CORRECTIVE ACTION ON BARCODE TTG8Q006LXMS. REF FAULT TTG8Q006KMKF; [02] PERFORMED CORRECTIVE ACTION ON BARCODE TTG8Q006LXMS. REF FAULT TTG8Q0SDR SWAA2021110918244None · brokenFOUND RIGHT UPPER STABILIZER-TO-BODY FRONT SPAR SLIDING SEAL BROKEN ; / [01] REMOVED RIGHT UPPER STABLIZER -TO- BODY FRONT SPAR SLIDING SEAL AS PER BOEING 737 AMM 53-31-31-000-801; [02] REMOVED EXISTING HARDWARE AND LOCATED AND DRILLED NEW SLIDING PER REF. 737SDR SWAA2021110918243None · brokenFOUND LEFT UPPER STABILIZER-TO-BODY FRONT SPAR SLIDING SEAL BROKEN ; / [01] REMOVED LEFT UPPER STABLIZER -TO- BODY FRONT SPAR SLIDING SEAL AS PER BOEING 737 AMM 53-31-31-000-801; [02] LOCATED AND DRILLED LEFT UPPER STABLIZER -TO- BODY FRONT SPAR SLIDING SEAL ASDR SWAA2021110918242Angle · crackedVERTICAL FIN; FWD TERMINAL FITTING ASSY AFT FACE HORIZONTAL T ANGLE CRACKED 2 EA PLACES ; / [01] PERFORMED HFEC INSP ON VERTICAL FIN FWD TERMINAL FITTING ASSY AFT FACE HORIZ T ANGLE IAW B737 NDT P6 51-00-00 PROC.23; CRACKS NOTED MARKED.<BR>TOOL USED : NORTEC 6SDR SWAA2021110818245Gusset · crackedFWD CARGO COMP GUSSET IS CRACKED BETWEEN FRAME BS 500D AND STGR 19L ; / [01] REMOVED GUSSET AT FWD CARGO COMPARTMENT AT FS 500D STRINGER 19L;FOUND OUT OF LIMITS IN REF B737-700 SRM 51-2=10-023-0G-0; LOCATED AND DRILLED NEW GUSSET IN REF B737-700 SRM 51-40-05-0SDR SWAA2021110818246Gusset · crackedFWD CARGO COMP GUSSET IS CRACKED BETWEEN FRAME BS 500D AND STGR 21L ; / [01] REMOVED CRACK GUSSET IN REF B737-700 SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED NEW GUSSET REF. B737-7 SRM #51-40-05-0G-0; [03] VEERIFIED STEP 1 AND 2; [04] OK TO TREAT AND PRIME HOLSDR SWAA2021110818247Gusset · crackedFWD CARGO COMP GUSSET IS CRACKED BETWEEN FRAME BS 500D AND STGR 24L ; / [01] REMOVED GUSSET AT FWD CARGO COMPARTMENT FS 500D;STRINGER 24L;IN REF B737-700 SRM 51-40-02-OG-0;LOCATED AND DRILLED GUSSET IN REF B737-700 SRM 51-40-05-0G-0; [02] VERIFIED STEP #1. OK
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