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 = 'N799SW' 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 = 'N799SW' 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 SWAA2022011260075Battery Pack · inoperativeEMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1675 ARE INOP. ; / [01] REPLACED BATTERY PACK M1675 AND PERFORMED GOOD INSTALLATION TEST PER PER AMM 33-51-06-960-905.; [02] UPDATED REMOVED PARTS REQUIREMENT.; [03] VERIFIED CORRECTIVE ACTION ENTRIES 1 AND 2SDR SWAA2022011260076Battery Pack · inoperativeEMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1672 ARE INOP ; / [01] EMERGENCY LIGHTS BATTERY PACK M1672 REPLACED WITH SERVICEABLE BATTERY PACK AND PERFORMED GOOD INSTALLATION TEST PER AMM33-51-06-960-805; [02] UPDATED PART INFORMATION.; [03] VERIFIED COSDR SWAA2021091015055Lamp · inoperativeFWD SERVICE DOOR SLIDE EMERGENCY LIGHT INOP ; / [01] REPLACED LAMP PER MM 33-51-04SDR SWAA2021080400541Cover · looseLH OVERWING EXIT COVER FELL OFF ; / [01] REATTACHED COVER PER SIPSDR SWAA2021080298996Battery Pack · failedEMERGENCY EXIT LIGHT BATTERY PACK M1668 (STA 603 WL 213 LBL67) INOP; WILL NOT TAKE CHARGE / [01] REPLACED EMERGENCY EXIT LIGHT BATTERY PACK M1668 PER AMM 33-51-06-960-805 ATAG PS0937 OPS CHECK GOOD.; [02] JOB COMPLETED; [03] VERIFIED ITEM 1 AND 2<BR>AUDIT C/WSDR SWAA2021080298995Battery Pack · inoperativeEMER AISLE LIGHT BETWEEN SEAT ROW 6ABC AND 7ABC INOP / [01] REPLACED EMERGENCY EXIT LIGHT BATTERY PACK M1668 PER AMM 33-51-06-960-805 ATAG PS0937 OPS CHECK GOOD. REFERENCE TTG8Q005YFPM FOR REPLACEMENT OF THE BATTERY M1668; [02] VERIFIED ITEM 1<BR>AUDIT C/WSDR SWAA2021072697812Scuff Plate · crackedAFT CARGO CENTER SCUFF PLATE FOUND TO BE CRACKED DURING INSPECTION. REMOVED DAMAGED CENTER SCUFF PLATE FROM AFT CARGO DOOR CUTOUT IAW SRM 51-40-02-0G-0. INSTALLED SCUFF PLATE IAW AMM 53-11-02-420-801.SDR SWAA2021071994541Fastener · missingPASSENGER CABIN RIGHT EMERGENCY EXIT HANDLE MISSING HARDWARE ; / [01] INSTALLED MISSING 1/4 TURN FASTENER PER S.I.P.SDR SWAA2021062586282Slide · out of positionFORWARD SERVICE DOOR SLIDE NEEDS TO BE REPACKED- COMING LOOSE ; / [01] REPOSITIONED SLIDE PER STEP C OF MX TASK 725-61-06SDR SWAA2021050768140Handle · exposedFWD SERVICE DOOR SLIDE HANDLE EXPOSED ; FWD SERVICE DOOR SLIDE HANDLE EXPOSED / REPOSITIONED FWD SVC DOOR SLIDE HANDLE IAW AMM 25-66-01SDR SWAA2020122938623Slide · out of positionTHE RED 'PULL HANDLE' IS VISIBLE WHEN RIGHT (FIRST OFFICER) SIDE SERVICE DOOR IS ARMED. REPACKED SLIDE IN SHELL, PER MT 725-61-06 FOR R2 DOOR CHECKS OK.SDR SWAA2020032442783Retainer · faultyL2 HEADER PANEL EMERGENCY EXIT SIGN LENS RETAINER WILL NOT ENGAGE REMOVED AND REPLACED/REINSTALLED L2 HEADER PANEL EMERGENCY EXIT SIGN LENS RETAINER IAW BOEING AMM 33-51-01-960-802 OPS CHECK GOOD ATAG #PS0891SDR SWAA2020040131301Door Frame · crackedPASSENGER CABIN; L-2 DOOR CUTOUT; STA 951+5; 15' ABOVE FLOOR; STUB FRAME IS CRACKED JUST ABOVE ROLLER LATCH RECIVER (MARKED IN RED) MOD / REPAIRED THE L2 DOOR SURROUND; FWD LOWER STUB FRAME AT BS 951; BELOW S-16L BY CUTTING OUT CRACK IAW EA # 200352 REV. IR. TSDR SWAA2021082727071Balance Weight · corrodedRIGHT AILERON 2 BALANCE WEIGHTS BETWEEN 2 AND 3 HINGE CORRODED / REMOVED AND REPLACED THE R/H AILERON 2 BALANCE WEIGHTS BETWEEN 2 AND 3 HINGE IAW SOPM 20-50-01 STEP 3F AND AMM 20-50-11-910-801 STEP 2 D (1) TABLE 203 THE WEIGHTS THAT WERE CHANGED WERE THE TWO ISDR SWAA2020032442782Wire · pulledPASSENGER CABIN EMERGENCY LIGHTS, GROUND BLOCK NO. GD03764 AT STATION 767 STRINGER 4L WIRE NO. W3142-0456-20 PULLED FROM CONNECTION. REPAIRED WIRE W3142-0456-20 IAW B737 WDM 33-51-14 AND BOEING SWPM 20-90-15. PERFORMED OPS TEST OF EMERGENCY EXIT LIGHTSSDR SWAA2020040127052Splice Plate · damaged(AD RELATED REF. SWA SI # 11932-53) UPPER FUSELAGE BUTT JOINT SPLICE PLATE AT STA 360 BETWEEN STR 4L-6L HAS SCRIBE DAMAGE APPROX 4' LONG. / REPAIRED SCRIBE DAMAGE ON BS 360 BUTT JOINT SPLICE STRAP AT S-5L BY SPLICING IN NEW SECTION OF STRAP IAW EA# 200262 REV.SDR SWAA2020040127044Seat Track · crackedCOCKPIT FLOOR CAPTAIN FWD INBD SEAT TRACK RAIL IS CRACKED AT FWD STOP PIN HOLE. / INSTALLED REPLACEMENT SEAT TRACK FOR CAPTAIN FWD INBD POSITION IAW AMM 25-11-11-400-801 AND AMM 20-50-11-910-801 AAR 35673 DUE 04-11-20 AAR 40183 DUE 05-15-20 WN9129SDR SWAA2020040127045Seat Track · crackedCOCKPIT FLOOR CAPTAIN AFT INBD SEAT TRACK STOP PIN RAIL HAS HEAVY WEAR. / INSTALLED REPLACEMENT SEAT TRACK FOR CAPTAIN AFT INBD TRACK IAW AMM 25-11-11-400-801 AND AMM 20-50-11-910-801 AAR 35673 DUE 04-11-20 AAR 40183 DUE 05-15-20 WN8161SDR SWAA2020040127046Seat Track · wornCOCKPIT FLOOR CAPTAIN AFT OTBD SEAT TRACK & STOP PIN RAILS HAVE HEAVY WEAR. / INSTALLED REPLACEMENT SEAT TRACK FOR CAPTAIN AFT OUTBD TRACK IAW AMM 25-11-11-400-801 AND AMM 20-50-11-910-801 AAR 35673 DUE 04-11-20 AAR 40183 DUE 05-15-20 WN4315SDR SWAA2020040127047Seat Track · crackedCOCKPIT FLOOR FIRST OFFICER FWD INBD SEAT TRACK RAIL IS CRACKED AT FWD STOP PIN HOLE. / INSTALLED REPLACEMENT SEAT TRACK FOR FIRST OFFICER FWD INBD POSITION IAW AMM 25-11-11-400-801 AND AMM 20-50-11-910-801 AAR 35673 DUE 04-11-20 AAR 40183 DUE 05-15-20 WN8925SDR SWAA2020040127048Seat Track · wornCOCKPIT FLOOR FIRST OFFICER AFT INBD SEAT TRACK STOP PIN RAIL HAS HEAVY WEAR. / INSTALLED REPLACEMENT SEAT TRACK FOR FIRST OFFICER AFT INBD POSITION IAW AMM 25-11-11-400-801 AND AMM 20-50-11-910-801 AAR 35673 DUE 04-11-20 AAR 40183 DUE 05-15-20 WN5962SDR SWAA2021082727040Balance Weight · corrodedRIGHT WING AILERON NOSE FITTING BAY #5; 5 EACH BALANCE WEIGHTS SHOW SIGNS OF CORROSION / REMOVED; REPLACED; AND VERIFIED PARTS FOR RIGHT WING AILERON NOSE FITTING BAY #5; 5 EACH BALANCE WEIGHTS IAW SRM 51-60-01-0G-0 STEP 5(A)(5)(D) AND AMM 20-50-11-910-801 ANDSDR SWAA2020040127039Splice · corrodedAFT CARGO BAY FLOOR SPLICE AT BS 887; LBL16 TO RBL 16; WL 162 CORRODED. / REFERENCE NRC Y174595 FOR WORK ACCOMPLISHED. AFT CARGO BAY FLOOR SPLICE AT BS 887 LBL 16 TO RBL 16; W/L 162 REPLACEDSDR SWAA2020030642207Floor Panel · delaminatedFLOOR PANEL 221DF LOWER SURFACE O/B SCALLOPED AREA IS DELAMED. REPAIRED FLOOR PANEL 221 DF LOWER SURFACE O/B SCALLOPED AREA IAW B 737-700 SRM'S 53-00-50-2R-1 REV 69 & 53-00-50-2R-0 REV 69 (A87485) (A14438) (A98132) (A21946) (A10203) (A94755) (A28395)SDR SWAA2020040127029Fitting · corrodedAFT CARGO COMPT. STA 727D+6; S-27R; WL150 (FWD) CLIP P/N 146A7734-2 HAS CORROSION REPLACED ON NON-ROUTINE Y174547 / AFT CARGO COMPARTMENT STA 727D+6' S-27R WL 150 (FWD) CLIP P/N 146A7734-2 NO PUBLISHED LIMITS FOR CLIP REPLACED ON NRC Y174547 P/N 146A7734-2SDR SWAA2020040127030Fitting · corrodedAFT CARGO COMPT. STA 727D+6; S-27R; WL150 (AFT) CLIP P/N 146A7734-2 HAS CORROSION REPLACED ON NON-ROUTINE Y174547 / AFT CARGO COMPARTMENT STA 727D+6' WL 150 (AFT) CLIP P/N 146A7734-2 NO PUBLISHED LIMITS FOR CLIP REPLACED ON NRC Y174547 P/N 146A7734-2SDR SWAA2020040127031Fitting · corrodedAFT CARGO COMPT. STA 727D+6; S-27L; WL150 (AFT) CLIP P/N 146A7734-2 HAS CORROSION REPLACED ON NON-ROUTINE Y174548 / AFT CARGO COMPARTMENT STA 727D+6' S-27L WL 150 (AFT) CLIP P/N 146A7734-2 NO PUBLISHED LIMITS FOR CLIP REPLACED ON NRC Y174548 P/N 146A7734-2SDR SWAA2020040127027Floor Panel · frayedFLOOR PANEL 221DF; TOP SURFACE FRAYED IN SEVERAL AREAS. (NOTE: RED DOT IS NUMBER 101-002) / REAPIRED FLOOR PANEL 221DF TOP SURFACE AS MARKED FRAYED SURFACES I/A/W SRM 53-00-50-2R-1 REV 69 AND SRM 53-00-50-2R-0 REV 69 A79470;A72547;A55972SDR SWAA2020022874835Floor Support · crackedAFT CARGO INTERCOSTAL CRACKED BETWEEN BS. 927 TO BS. 947.5, RBL 20. / R&R INTERCOSTAL IAW SRM & DWG.SDR SWAA2020032442803Attach Angle · crackedRIGHT LOWER FUSELAGE - STA. 663 - WHERE VAPOR BARRIER ANGLE ATTACHES TO THE 663 ANGLE - IS CRACKED AT RBL 7. REPAIRED LOWER FUSELAGE BS 663 VAPOR BARRIER ANGLE THAT ATTACHES AT 663 19T RBL 7 IAW EA 200130 IR AND SWA EA 1-757-16838 IR.SDR SWAA2020031242403Stringer Splice · corrodedCUSTOMER REQUEST SWA QC REP MDB. AD DRIVEN. E&E COMPARTMENT AFT OF STA 360, STR 27R STRINGER SPLICE IS CORRODED (STA 362, STR 27R, WL 150). STRINGER SPLICE IN E&E COMPARTMENT AFT OF BS 360 S-27R. WL 150. 100% MATERIAL LOSS. ORIGNAL ALL WORK FOR SPLICE SDR SWAA2020040126970Stiffener · crackedBS 663; VAPOR BARRIER WEB; VERTICAL STIFFENER AT RBL 28; LOWER END CRACKED. / REMOVED AND REPLACED STIFFNER PART# 111A130816 AT STA 663 RBL 25 PER SRM 51-40-02-0G-0 AND DWG 111A100 REV-SDR SWAA2020040126988Stringer · corrodedE/E COMPARTMENT AFT END OF STRINGER 29 STA 312+11 HAS CORROSION ON RIGHT VERTICAL WEB CAUSING A LARGE FLAKE TO COME OFF / REPAIRED S-29 AT BS 312+11' IAW EA# 200213 REV. IR N AND SWA EA# 1-753-36650 REV. IR. CORROSION WAS 100% MATERIAL LOSS P/N: 141A3532-7SDR SWAA2020021941465Bulkhead Web · crackedEXISTING REPAIR ON VAPOR BARRIER WEB CRACKED AND DISBONDED AT BS. 663, RBL 11. / REPAIRED WEB IAW SRM.SDR SWAA2020022741779Intercostal · crackedINTERCOSTAL CRACKED BETWEEN BS. 294 TO BS. 312, STR. 4L. / R&R INTERCOSTAL IAW SRM AND DWG.SDR SWAA2020040126838Floor Panel · damagedFLOOR PANEL 231XF HAS FIBERS PULLED FROM TOP SURFACE FROM TAPE REMOVAL / FABRICATED NEW PASSENGER CABIN FLOOR PANEL 231 XF PER SAMPLE OF ORIGINAL I/A/W SRM 53-00-50-2R-0 REV 69; BAC 5085 STEP 8.4.2 REV E AND PER BOEING DWG: 144A5810 ID: 0007 REV.E WN4933; A290SDR SWAA2020040126839Floor Panel · damagedFLOOR PANEL 232RF HAS FIBERS PULLED FROM TOP SURFACE FROM TAPE REMOVAL / FABRICATED NEW PASSENGER CABIN FLOOR PANEL 232 RF PER SAMPLE OF ORIGINAL I/A/W SRM 53-00-50-2R-0 REV 69; BAC 5085 STEP 8.4.2 REV E AND PER BOEING DWG: 144A5810 ID: 0004 REV:- WN4933; A290SDR SWAA2020040126840Floor Panel · damagedFLOOR PANEL 231ZF HAS FIBERS PULLED FROM TOP SURFACE FROM TAPE REMOVAL / FABRICATED NEW FLOOR PANEL 231ZF (NEW) PER SAMPLE OF ORIGINAL I/A/W SRM 53-00-50-2R-0 REV 69; PER BOEING DWG: 144A5810 ID: 0011 REV:- AND I/A/W BAC 5085 REV E. WN4933; A29079; A25968SDR SWAA2020040126841Floor Panel · damagedFLOOR PANEL 232SF HAS FIBERS PULLED FROM TOP SURFACE FROM TAPE REMOVAL / FABRICATED NEW FLOOR PANEL 232SF PER SAMPLE OF ORIGINAL I/A/W SRM 53-00-50-2R-0 REV 69; PER BOEING DWG: 144A5810 ID: 0001 REV:- AND I/A/W BAC 5085 REV E. WN4933; A29079; A25968SDR SWAA2020040126842Floor Panel · damagedFLOOR PANEL 242BF HAS FIBERS PULLED FROM TP SURFACE FROM TAPE REMOVAL / FABRICATED NEW FLOOR PANEL 242 BF PER SAMPLE OF ORIGINAL I/A/W SRM 53-00-50-2R-0 REV 69; BOEING DWG: 144A5810 ID: 0002 REV:A AND BAC 5085 REV.E WN4933; A29079; A25968SDR SWAA2020040126843Floor Panel · damagedFLOOR PANEL 231YF HAS FIBERS PULLED FROM TOP SURFACE FROM TAPE REMOVAL / FABRICATED NEW FLOOR PANEL 231 XF PER SAMPLE OF ORIGINAL I/A/W SRM 53-00-50-2R-0 REV 69; BOEING DWG: 144A5810 ID: 0004 REV:- AND BAC 5085 (8.4.2) REV E. WN4933; A29079; A25968SDR SWAA2020040126877Floorboard · damagedAFT GALLEY/LAV WET AREA; FLOORBOARD 241ABF; HAS COMPOSITE FIBER DAMAGE. / REPAIRED PASSENGER CABIN FLOOR PANEL 241ABF IAW SRM 53-00-50-2R-0 GENERAL REPAIR REV 69 AND SRM 53-00-50-2R-1 REP 1 REV 69 (A72547)(A79470)SDR SWAA2020040126872Floorboard · damagedAFT GALLEY/LAV WET AREA; FLOORBOARD 241ACF;HAS COMPOSITE FIBER DAMAGE . / REPAIRED PASSENGER CABIN FLOOR PANEL 241ACF IAW SRM 53-00-50-2R-0 GENERAL REPAIR 69 AND SRM 53-00-50-2R-1 REPAIR 1 REV 69 (A72547);(A79470);(A55972)SDR SWAA2020040126867Floorboard · damagedAFT GALLEY/LAV WET AREA; FLOORBOARD 241XF;HAS COMPOSITE FIBER DAMAGE . / REPAIRED PASSENGER CABIN FLOOR PANEL 241XF IAW SRM 53-00-50-2R-0 GENERAL REPAIR AND SRM 53-00-50-2R-1 REPAIR 1 REV 69 ON UPPER SURFACE (A72547) (A79470)SDR SWAA2020040126860Floorboard · damagedPASSENGER CABIN FLOOR BOARD # 242 AF TOP SKIN PLY SURFACE AREA ;IN THE CENTER FWD SECTION OF BOARD; FIBERS ARE DAMAGED / REPAIRED PASSENGER CABIN FLOOR PANEL 242AF IAW SRM 53-00-50-2R-0 GENERAL REPAIR REV 69 AND SRM 53-00-50-2R-1 REPAIR 1 REV 69 A72547; A79470SDR SWAA2020040126861Floorboard · puncturedPASSENGER CABIN FLOOR BOARD # 242 AF OUTBD OF #4 INSERT ON THE L/H/S TOP SKIN PLIES OF BOARD ARE PUNTURED AS MARKED / REPAIRED PASSENGER CABIN FLOOR PANEL 242 AF IAW SRM 53-00-50-2R-0 GENERAL REPAIR REV 69 AND SRM 53-00-50-2R-1 REPAIR 1 REV 69 A72347; A79470; SDR SWAA2020040126862Floorboard · damagedPASSENGER CABIN FLOOR BOARD # 241 AF TOP SKIN PLY SURFACE THE LENGTH AND WIDTH OF BOARD; IN SEVERAL AREAS FIBERS ARE DAMAGED / FABRICATED NEW PASSENGER CABIN FLOORBOARD #241AF PER SAMPLE OF ORIGINAL I/A/W SRM 53-00-50-2R-0 REV 69; PER BOEING DWG: 144A5810 ID: SDR SWAA2020040126859Floorboard · damagedPASSENGER CABIN FLOOR BOARD # 241 BF TOP SKIN PLY SURFACE THE LENGTH AND WIDTH OF BOARD; IN SEVERAL AREAS FIBERS ARE DAMAGED / FABRICATED NEW PASSENGER CABIN FLOOR PANEL 241 BF I/A/W SRM 53-00-50-2R-0 REV 69; BOEING DWG: 144A5810 ID: 0037 REV:- WN4933; A29079;SDR SWAA2020040126858Floorboard · damagedPASSENGER CABIN FLOOR BOARD # 241 DF TOP SKIN PLY SURFACE THE LENGTH AND WIDTH OF BOARD; IN SEVERAL AREAS FIBERS ARE DAMAGED / FABRICATED NEW PASSENGER CABIN FLOOR BOARD #241 DF PER SAMPLE OF ORIGINAL I/A/W SRM 53-00-50-2R-0 REV 69; BOEING DRAWING: 144A5810 IDSDR SWAA2020040126857Floorboard · damagedPASSENGER CABIN FLOOR BOARD # 241 EF TOP SKIN PLY SURFACE THE LENGTH AND WIDTH OF BOARD; IN SEVERAL AREAS FIBERS ARE DAMAGED / FABRICATED NEW PASSENGER CABIN FLOOR BOARD #241EF PE WN4933; A29079; A25968
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