N939SW
Service difficulty reports · 191
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 = 'N939SW' AND registry_match = 'registration' 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 = 'N939SW' AND registry_match = 'registration' 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 SWIA2024111501252Anti-Skid Sys · warning messageON TO, AFTER MOVING LANDING GEAR LEVER UP, ANTI SKID OUTBOARD CAUTION MESSAGE. FOLLOWED 20-30 SECONDS LATER BY A GEAR DISAGREE WARNING. NOSEHWEEL UP, MAINS DOWN. RAN THE QRH SLOWED FROM 250 TO 200, TURNED ON HYDRAULIC PUMP 2 AND 3B MESSAGE PERSISTED. AS WE WERSDR SWI2024F00492Floor Panel · damagedD: SINGULAR FLOOR PANEL IN CARGO BAY IS SLIGHTLY DAMAGED (INDENTS A FEW INCHES WHEN STEPPED UPON AND SHOWING VERY SMALL HOLES IN THE MIDDLE) STILL STRUCTURALLY SOUNDC: MEL 25-52-1CAT C DUE 6/26/24SINGULAR FLOOR PANEL IN CARGO BAY IS SLIGHTLY DAMAGED (INDENTS ASDR SWIA2024032000212Structure · chafedRH MLG WHEEL WELL AT WING BOX LOWER PLANK AFT EDGE BL45.00 AND STR3 HAS SIGN OF CHAFFING (C-CHECK RO 3/19/2024) PERFORMED REPAIR ON R/H MLG WHEEL WELL AT WING BOX LWR PLANK AFT EDGE ON LBL 45.00 STR 3 IAW CRJ 200 REO 601R-57-21-3824. PERFORMED NDT ET INSPESDR SWIA20240320201Structure · chafedLEFT MAIN LDG GEAR WHEEL WELL OB CORNER FS511.0 AND WS50.54 AREA EVAL CHAFFING (C-CHECK RO 3/19/2024) PERFORMED REPAIR ON DAMAGE AREA AT L/H MLG WHEEL WELL O/B CORNER ON LWR WING PLANK LBL 45.00 STR #3 IAW CRJ 200 REO 601R-57-21-3824, AND CRJ 200 SRM 57-21SDR SWI2024F00251Seat Track · corrodedL/H FLOOR SEAT TRACK AT FS 559.00 + 80- FS 559.00 + 96 AT LBL27 HAS SIGNS OF CORROSION (C-CHECK RO 3/19/2024) REMOVED ANN INSTALLED NEW L/H FLOOR SEAT TRACK AT FS559.00+80 - FS559.00+96 AT LBL27 IAW CRJ200 AMM 53-00-49TORQUE DRIVER: AV-1623 CAL DUE: JAN202SDR SWI2024F00250Seat Track · corrodedL/H FLOOR SEAT TRACK AT FS 559.00 + 80- FS 559.00 + 96 AT LBL9 HAS SIGNS OF CORROSION (C-CHECK RO 3/19/2024) REMOVED AND REPLACED LH SEAT TRACK AT FS559.00 + 80 - FS559.00 + 96 AT LBL9, WET SEALED AND TORQUED IAW CRJ 200 AMM 53-00-49CAL TOOL: AV-1623CAL DSDR SWI2024F00249Seat Track · corrodedR/H FLOOR SEAT TRACK AT FS 559.00 + 80- FS 559.00 + 96 AT RBL9 HAS SIGNS OF CORROSION (C-CHECK RO 3/19/2024) REMOVED AND REPLACED RH FLOOR SEAT TRACK AT FS 559.00 + 80 - FS 559.00 + 96 AT RBL 9 IAW CRJ AMM 53-00-49 CALIBRATED TOOL: AJ-1336DUE: JANUARY 2025SDR SWI2024F00248Seat Track · corrodedR/H FLOOR SEAT TRACK AT FS 559.00 + 80 - FS 559.00 + 96 AT RBL27 HAS SIGNS OF CORROSION (C-CHECK RO 3/19/2024) REMOVED AND INSTALLED NEW RH SEAT TRACK AT FS559.00+80 TO FS559.00+96 AT RBL27 IAW CRJ200 AMM 53-01-11SDR SWI2024F00247Seat Track · corrodedR/H FLOOR SEAT TRACK AT FS 559.00 + 96- FS- 559 + 112 AT RBL27 HAS SIGNS OF CORROSION (C-CHECK RO 3/19/2024) INSTALLED RH FLOOR SEAT TRACK @ FS559.00+96 TO FS559.00+112 IAW CRJ200 AMM 53-00-49-400-801.SDR SWI2024F00246Seat Track · corrodedR/H FLOOR SEAT TRACK AT FS 559.00 + 96 - FS 559 + 112 AT RBL9 HAS SIGNS OF CORROSION (C-CHECK RO 3/19/2024) REMOVED AND INSTALLED NEW RH SEAT TRACK FROM FS559.00+96 TO FS559.00+112 AT RBL9 IAW CRJ200 AMM 53-01-11SDR SWI2024F00245Seat Track · corrodedL/H FLOOR SEAT TRACK AT FS 559.00 + 96- FS 559 + 112 AT LBL9 HAS SIGNS OF CORROSION (C-CHECK RO 3/19/2024) REMMOVED AND INSTALLED FLOOR SEAT TRACK AT LH FS 559.00 +112 AT LBL 9 IAW CRJ200 AMM 53-01-11SDR SWI2024F00244Seat Track · corrodedL/H FLOOR SEAT TRACK AT FS 559.00 + 96 - FS 559 + 112 AT LBL27 HAS SIGNS OF CORROSION (C-CHECK RO 3/19/2024) REMOVED AND REPLACED LH FLOOR SEAT TRACK AT F.S 559.00+96 TO F.S 559.00+112 AT LBL27 IAW CRJ 200 SRM 51-40-11CAL TOOL: TD S/N AV1623 CAL DATE 01/25SDR SWI2024F00243Seat Track · corrodedL/H FLOOR SEAT TRACK AT FS 559 + 112- FS 621 AT LBL27 HAS SIGNS OF CORROSION (C-CHECK RO 3/19/2024) REMOVED AND REPLACED LH FLOOR SEAT TRACK AT FS 559+112 - FS 621 AT LBL 27 IAW CRJ 200 AMM 53-00-49.CAL TOOLS: TORQUE DRIVER AJ 1336 CAL DATE JAN 2025SDR SWI2024F00242Seat Track · corrodedL/H FLOOR SEAT TRACK AT FS 559 + 112- FS 621 AT LBL9 HAS SIGNS OF CORROSION (C-CHECK RO 3/19/2024) REMOVED AND INSTALLED NEW LH SEAT TRACK AT FS559.00+112 TO FS621.00 AT LBL9 IAW CRJ200 AMM 53-01-11CAL TOOLS: TW AV 1627 CAL DATE 01/25SDR SWI2024F00241Seat Track · corrodedR/H FLOOR SEAT TRACK AT FS 559 + 112- FS 621 AT RBL9 HAS SIGNS OF CORROSION (C-CHECK RO 3/19/2024) REMOVED AND REPLACED SEAT TRACK FROM FS559+112 - FS621 AT RBL9 IAW CRJ 200 AMM 53-00-49CAL TOOL : TORQUE DRIVER AV-1623CAL DUE: JAN 25SDR SWIA20240320128Seat Track · corrodedR/H FLOOR SEAT TRACK AT FS 559 + 112- FS 621 AT RBL27 HAS SIGNS OF CORROSION (C-CHECK RO 3/19/2024) RH FLOOR SEAT TRACK AT FS 559.+112-FS621 AT RIB 27L REPLACED IAW CRJ 200-AMM 53-00-49SDR SWIA20240320127Angle · crackedFOUND ANGLE CRACK AT AFT PRESS BULKHEAD REAR FS625.0 STR12R (C-CHECK RO 3/19/2024) REMOVED AND REPLACE NEW INTERCOSTAL P/N 601-35012-52 AT AFT PRESS BULKHEAD REAR FS 625.0 STR 12R IAW CRJ 200 SRM 51-42-20SDR SWIA20240320117Skin · dentedUPPER AFT FUSELAGE FS672.00 TO F.S. 682.20 AT STR 3 HAS DENT (C-CHECK RO 3/19/2024) PERFORMED PERMANENT REPAIR ON UPPER AFT FUSELAGE F.S 672.00 TO F.S 682.00 STGR 3 LH IAW MHIRJ REO 601R-53-61-8148 REV -- DATED 2024-01-25 NDT PERFORMED BY BARRON NDT FAA CSDR SWIA20240320115Skin · damagedADM# N939SW-8619 BETWEEN STGR 15L/16L F.S. 404.00. 7/8" LONG BY 3/8 WIDE WITH A DEPTH OF .0040" DEEP. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED. ELIMINATE EVIDENCE OF DAMAGE USING STANDARD ACFT PRACTICES. (C-CHECK RO 3/19/2024SDR SWIA202264099None · malfunctionedDURING A GO AROUND AFTER RETRACTING THE GEAR RECEIVED A €ŒGEAR DISAGREE€?. NOSE WHEEL SHOWED NOT UP AND LOCKED. AFTER ABOUT 1 MINUTE, NOSE WHEEL SHOWED UP AND LOCKED AND DISAGREE EXTINGUISHED. RAN QRH PROCEDURE , NO FURTHER ISSUES. (FLIGHT 5452 - FILED CSDR SWIA202163097None · crackedUPON BOARDING AIRPLANE CAPTAINS FRONT WINDSHIELD IS CRACKED. (FILED CLOSED)REPLACED CAPTAINS WIND SHIELD IN REFERENCE TO TASK CARD 56-220-1000-SKY AND CRJ 200 MM 56-11-01, OPS CHECK GOODSDR SWIA202054611Skin · chafedLT AILERON UPPER LEADING EDGE SKIN CHAFED IN 2 EA PLACES ON BOTTOM SIDE OF SKIN ABOVE THE CENTER HINGE NUTS. FILED CLOSED. LT AILERON UPPER LEADING EDGE SHROUD FOUND OUT OF LIMITS, REF CRJ 200 SRM AND INSTALLED A NEW LEADING EDGE SHROUD, REF DRAWING AND CRJ SDR SWIA202054610Skin · bentRT AILERON LEADING EDGE SKIN IS BENT UP AT THE CENTER HINGE. FILED CLOSED. REMOVED DAMAGED RT AILERON LEADING EDGE UPPER SHROUD, REF CRJ 200 SRM AND INSTALLED A NEW SHROUD, REF CRJ 200 SRM AND DRAWING AND REO.SDR SWIA202054556Hinge Fitting · corrodedRT ELEVATOR HINGE FITTING PN 600-24043-1 NEEDS REPLACING DUE TO PITTING. C-CHECK RO 12/05/2020. INSTALLED NEW RT ELEVATOR HINGE FITTING PN 600-24043-1 P/O 7742-00008/136, REF BOMBARDIER DWG CRJ 200 SRM.SDR SWIA202054555Hinge Fitting · corrodedLT ELEVATOR HINGE FITTING PN 600-24043-1 NEEDS REPLACING DUE TO PITTING. C-CHECK RO 12/05/2020. INSTALLED NEW LT ELEVATOR HINGE FITTING PN 600-24043-1 PO 7742-00008/135, REF BOMBARDIER DWG AND CRJ 200 SRM.SDR SWIA202054554Structure · bentLT AILERON LEADING EDGE AT THE CENTER HINGE POINT, IS BENT UPWARD. C-CHECK RO 12/05/2020. REPLACED WITH NEW LT AILERON LEADING EDGE AT THE CENTER HINGE POINT, REF DWG, CRJ 200SRM. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH SKYWEST TASK CARD.SDR SWIA202054553Fairing · chafedRIGHT WING TRAILING EDGE TO FUSELAGE APRON CHAFED, MARKED. C-CHECK RO 12/05/2020. REPAIRED RIGHT WING TRAILING EDGE TO FUSELAGE APRON, REF REO. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH SKYWEST TASK CARD.SDR SWIA202054552Floor Support · damagedRT FLOOR SILL FROM FS 559+84.9-FS 562.69 REQUIRES REPLACEMENT. C-CHECK RO 12/05/2020. REPLACED RT FLOOR SILL (P/N 601R31133-102) BETWEEN FS 559.00+84.9 AND FS 562.69, REF CRJ200 SRM AND DWG. COMPLIED WITH TASK CARD. LEAK CHECK SATISFACTORY.SDR SWIA202054551Intercostal · corrodedINTERCOSTAL DD1 IS CORRODED IN SEVERAL LOCATIONS (NOTED AFTER INTERNAL SKIN WAS REMOVED). C-CHECK RO 12/05/2020. PAX DOOR MID DD1 INTERCOSTAL ORIGINAL MATERIAL THICKNESS IS 0.050", IAW CRJ 200 SRM. EXFOLIATED CORROSION AT MULTIPLE LOCATION AND MORE TWO ELEMSDR SWIA202054550Intercostal · corrodedINTERCOSTAL DD2 IS CORRODED IN SEVERAL LOCATIONS (NOTED AFTER INNER SKIN WAS REMOVED). C-CHECK RO 12/05/2020. PAX DOOR MID DD2 INTERCOSTAL ORIGINAL MATERIAL THICKNESS IS 0.050", IAW CRJ 200 SRM. EXFOLIATED CORROSION AT MULTIPLE LOCATION AND MORE TWO ELEMENTSDR SWIA202054549Intercostal · corrodedPAX DOOR AFT DD1 INTERCOSTAL IS CORRODED. C-CHECK RO 12/05/2020. PAX DOOR AFT DD1 INTERCOSTAL ORIGINAL MATERIAL THICKNESS IS 0.050", IAW CRJ 200 SRM. EXFOLIATED CORROSION AT MULTIPLE LOCATION AND MORE TWO ELEMENT AT GIVEN CROSS-SECTION OUT OF LIMITS, IAW CRSDR SWIA202054548Skin · damagedWHILE REMOVING PANEL 132AL FOUND EXISTING DAMAGE AROUND SCREW HOLE. C-CHECK RO 12/05/2020. BLENDED OUT TOOLING DAMAGE ON SKIN RING AT PANEL 132AL, REF CRJ 200 SRM. EVALUATED AND FOUND TO BE OUT OF LIMITS. SUBMITTED AND RECEIVED ENGINEERING REF REO, ALL STESDR SWIA202054547Door Frame · corrodedPAX DOOR FRAME FS 313.56 AND CLEAT HAS CORROSION. C-CHECK RO 12/05/2020. REMOVED FS 313.56 PAX DOOR FRAME & CLEAT. BLENDED CORROSION TO A SMOOTH CONTOUR. REMAINING MATERIAL ON FS 313.56 FRAME WITHIN LIMITS & CLEAT WAS NOT. REINSTALLED FS 313.56 PAX DOOR FSDR SWIA202054546Intercostal · corrodedPAX DOOR INTERCOSTAL DD4 CORRODED, MARKED. C-CHECK RO 12/05/2020. PAX DOOR MID DD4 ORIGINAL MATERIAL THICKNESS IS 0.050", IAW CRJ 200 SRM. EXFOLIATED CORROSION AT MULTIPLE LOCATION AND MORE TWO ELEMENT AT GIVEN CROSS-SECTION OUT OF LIMITS, IAW CRJ 200 SRM. SDR SWIA202054545Attach Angle · corrodedPAX DOOR FWD UPPER ATTACH CORNER ANGLE FOR DD6 IS CORRODED, MARKED. C-CHECK RO 12/05/2020. REMOVED AND INSTALLED NEW PAX DOOR ANGLE COMON TO FWD DD6 INTERCOSTAL, IAW CRJ 200 SRM AND BOMBARDIER DWG.SDR SWIA202054544Intercostal · corrodedPAX DOOR INTERCOSTAL DD3 CORRODED, MARKED. C-CHECK RO 12/05/2020. PAX DOOR MID DD3 ORIGINAL MATERIAL THICKNESS IS 0.050", IAW CRJ 200 SRM. EXFOLIATED CORROSION AT MULTIPLE LOCATION AND MORE TWO ELEMENT AT GIVEN CROSS-SECTION OUT OF LIMITS, IAW CRJ 200 SRM. SDR SWIA202054543Intercostal · corrodedPAX DOOR INTERCOSTAL 4TH FROM TOP ON AFT SIDE IS CORRODED, MARKED (NOTED AFTER INNER SKIN WAS LIFTED). C-CHECK RO 12/05/2020. PAX DOOR AFT DD4 INTERCOSTAL ORIGINAL MATERIAL THICKNESS IS 0.050", IAW CRJ 200 SRM. EXFOLIATED CORROSION AT MULTIPLE LOCATION AND SDR SWIA202054542Former · corrodedPAX DOOR AFT FORMER CORRODED IN SEVERAL OF THE UPPER BAYS ON THE INNER SIDE, MARKED (NOTED AFTER INNER SKIN WAS LIFTED). C-CHECK RO 12/05/2020. PAX DOOR AFT FORMER ORIGINAL MATERIAL THICKNESS IS 0.063", IAW CRJ 200 SRM. EXFOLIATED CORROSION AT MULTIPLE LOCASDR SWIA202054541Former · corrodedPAX DOOR FWD FORMER CORRODED IN SEVERAL OF THE UPPER BAYS ON THE INNER SIDE, MARKED (NOTED AFTER INNER SKIN WAS LIFTED). C-CHECK RO 12/05/2020. PAX DOOR FWD FORMER ORIGINAL MATERIAL THICKNESS IS 0.063", IAW CRJ 200 SRM. EXFOLIATED CORROSION AT MULTIPLE LOCASDR SWIA202054574Anchor Fitting · corrodedPASSENGER DOOR FWD COUNTERBALANCE ANCHOR FITTING HAS CORRODED ATTACHMENT HARDWARE. C-CHECK RO 12/05/2020. REMOVED AND INSTALLED NEW SERRATED PLATE AND ANCHOR FITTING, PER REFERENCE CRJ 200 AMM. ADJUSTMENT CHECK GOOD.SDR SWIA202054573Anchor Fitting · corrodedPAX DOOR AFT ANCHOR FITTING SERRATE PLATE IS CORRODED. C-CHECK RO 12/05/2020. REPLACED THE ORIGINAL PAX DOOR AFT ANCHOR PLATE WITH NEW, REF CRJ 200 AMM. TORQUE WRENCH: TUC5660, CAL DUE: 31-JAN-21. NEW PARTS INSTALLED AS FOLLOWS: 1 EA PLATE, 10 EA NUT, 4 EASDR SWIA202054540Attach Angle · crackedFS 484.00 RBL 27 RT SILL, FLIGHT CONTROL CABLES ROLLER GUIDE BRACKET BOTH ATTACH ANGLES CRACKED, MARKED. C-CHECK RO 12/05/2020. REMOVED INBOARD AND OUTBOARD ANGLE AT FS 484, RBL 27-RBL 36, REF CRJ200 SRM. REPLACED WITH NEW INBOARD AND OUTBOARD REPAIR ANGLE SDR SWIA202054539Bracket · crackedFS 484.00 LBL 27 LT SILL, FLIGHT CONTROL CABLES ROLLER GUIDE BRACKET OUTBOARD ATTACH ANGLE CRACKED, MARKED. C-CHECK RO 12/05/2020. REMOVED AND INSTALLED NEW OUTBOARD REPAIR ANGLE AT FS 484, LBL 27-LBL 36, REF REO. COMPLIED WITH TASK CARD. PRESSURE CHECKS GSDR SWIA202054538Floor Support · damagedRT FLOOR SILL INTERCOSTAL FROM FS 559.00-FS 559+16 HAS 100% MATERIAL LOSS AND REQUIRES REPLACEMENT. C-CHECK RO 12/05/2020. REMOVED RT FLOOR SILL INTERCOSTAL AND 3 EA ATTACHING ANGLES FROM FS 559.00-FS 559.00+16, REF CRJ200 SRM. INSTALLED NEW RT FLOOR SILL ISDR SWIA202054572Cover Plate · corrodedSERVICE DOOR SILL COVER PLATE HAS CORROSION. C-CHECK RO 12/05/2020. REPLACED DOOR SILL PLATE P/N 601R38957-31. LOCATED NEW HOLES, INSTALLED 6 NEW 8-32 DOME NUTS, IAW CRJ200 DWG 601R38957 REV F CRJ200 SRM SOLID RIVETS AND CRJ200 SRM HOLE PREPERATION.SDR SWIA202054537Intercostal · corrodedINTERCOSTAL BETWEEN FS 295.00 AND FS 310.00, BETWEEN STGR 17L AND 18L CORRODED. C-CHECK RO 12/05/2020. REMOVED CORRODE INTERCOSTAL AND INSTALLED A NEW INTERCOSTAL AT FS 295 TO FS 310 AT SRINGER 17L AND 18L, REF CRJ 200 SRM AND DRAWING. PRESSURE CHECKS AND OSDR SWIA202054536Stringer · crackedSTGR 3L CRACKED AT FS 379.00. C-CHECK RO 12/05/2020. REMOVED FASTENERS, CUT OUT BETWEEN FS 379.0 & FS 394.0 AND DISCARDED STR 3L DAMAGED SECTION, REF CRJ 200 SRM. FABRICATED REPAIR PARTS. INSTALLED REPAIR PARTS AT STR 3L BETWEEN FS 379.0 & FS 394.0 AND APPSDR SWIA202054560Attach Angle · crackedCLIP ATTACHED TO RT INTERCOSTAL ON FS 621 BULKHEAD CONNECTING TO FRAME AT FS 625, STGR 13R IS CRACKED. C-CHECK RO 12/05/2020. RECEIVED NEW INTERCOSTAL CLIP P/N 601-35012-52. REMOVED DAMAGED CLIP AT FS 625.00 AT STR 13R, IAW CRJ200 SRM. LOCATED AND DRILLED SDR SWIA202054559Attach Angle · crackedCLIP ATTACHED TO LT INTERCOSTAL ON FS 621 BULKHEAD CONNECTING TO FRAME AT FS 625, STGR 13L IS CRACKED. C-CHECK RO 12/05/2020. RECEIVED NEW INTERCOSTAL CLIP P/N 601-35012-51. REMOVED DAMAGED CLIP AT FS 625.00 AT STR 13L, IAW CRJ200 SRM. LOCATED AND DRILLED SDR SWIA202054535Angle · crackedCLIP ATTACHED TO LT INTERCOSTAL ON FS 621 BULKHEAD CONNECTING TO FRAME AT FS 625, STGR 14L IS CRACKED. C-CHECK RO 12/05/2020. REMOVED CRACKED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL P/N 601-35012-53 AT FS 625 STGR 14L, REF DWG, CRJ200 SRM.
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