N980SW
Service difficulty reports · 202
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 = 'N980SW' 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 = 'N980SW' 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 SWI2025F00326Windshield · arcedCA WINDSHIELD CRACKED AND CAUSING ARCING. REMOVED CA WINDSHIELD IN REFERENCE TO AMM 56-11-01. REFERENCE CP 29735053-1 FOR INSTALLATION.SDR SWI2025F00284Window · arcedCA WINDSHIELD CRACKED AND CAUSING ARCING. (FILED OPEN) REMOVED CA WINDSHIELD IN REFERENCE TO AMM 56-11-01. REFERENCE CP 29735053-1 FOR INSTALLATION.SDR SWIA2025021900018Switch · malfunctionedENGINE OVER SPEED WARNING ON RIGHT ENGINE DURING CLIMB, THERE WAS AN UNCOMMANDED ACCELERATION FROM 93% N1 TO ABOUT 99% N1. THIS OCCURRED LESS THAN A MINUTE AFTER THRUST HAD BEEN ADJUSTED TO THE CLIMB THRUST SETTING. LEFT ENGINE DID SIMILAR ACCELERATION, BUT DISDR SWI202501240078Indication Sys · false activationAT THE NEXT OVERNIGHT MX, T/S REPEAT WRITE UPS FOR YDMCI TYPE: TROUBLESHOOTING PRIORITY 1UNCOMMANDED YAW MOTION (FLIGHT 5219 - FILED CLOSED) JAN 22, 2025 STATION: GRB--REMOVED AND REPLACED FCC #2 CARD IAW AMM 22-12-14. OPS CHECK GOOD AT THIS TIME. AC RESDR SWI202408210700Skin · dentedTRANSFER FROM EAML 1352997 : CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 1352408 FOUND 30 DENTS ON RH FLIGHT SPOILER UPPER SKIN. (FLIGHT 5057 - FILED CLOSED)REMOVED AND REPLACED RH FLIGHT SPOILER IN REFERENCE WITH AMM 27-64-05. OPS CHECKED GOOD AT SDR SWI202408210699Skin · dentedTRANSFER FROM EAML 1352977 : CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 1352408 FOUND 18 DENTS ON RH AILERON UPPER SKIN. (FLIGHT 5057 - FILED CLOSED)REMOVED AND REPLACED RH AILERON IN REFERENCE WITH AMM 27-15-01 AND TASK CARD 27-900-1001-SKY. OPS SDR SWI202408210698Skin · dentedTRANSFER FROM EAML 1352976 : CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 1352408 FOUND 45 DENTS ON LH AILERON UPPER SKIN. (FLIGHT 5057 - FILED CLOSED)REMOVED AND REPLACED LH AILERON ASSEMBLY REFERENCING AMM 27-15-01. COMPLIED WITH TASK CARD 27-900-1SDR SWI202408210697Skin · dentedTRANSFER FROM EAML 1352994 : CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 1352408 FOUND 22 DENTS ON LH FLIGHT SPOILER UPPER SKIN. (FLIGHT 5057 - FILED CLOSED)REMOVED AND REPLACED LH FLIGHT SPOILER IN REFERENCE WITH AMM 27-64-05. REFER TO CP 28456843 SDR SWI202408210696Skin · dentedTRANSFER FROM EAML 1352978 : CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 1352408 FOUND 23 DENTS ON ON LH OTBD FLAP UPPER SKIN. (FLIGHT 5057 - FILED CLOSED)REMOVED AND REPLACED LH OUTB FLAP ASSEMBLY IN REFERENCE WITH AMM 27-54-05. COMPLIED WITH TASK SDR SWIA2024082100602Skin · dentedTRANSFER FROM EAML 1352982 : CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 1352408 FOUND 74 DENTS ON RH INBD FLAP UPPER SKIN. (FLIGHT 5057 - FILED CLOSED)REMOVED AND REPLACED RH INBD FLAP ASSEMBLY IN REFERENCE WITH AMM 27-54-01. COMPLIED WITH TASK CASDR SWI2024082100696Skin · dentedTRANSFER FROM EAML 1352978 : CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 1352408 FOUND 23 DENTS ON ON LH OTBD FLAP UPPER SKIN. (FLIGHT 5057 - FILED CLOSED)REMOVED AND REPLACED LH OUTB FLAP ASSEMBLY IN REFERENCE WITH AMM 27-54-05. COMPLIED WITH TASK SDR SWI2024F00280Warning Message · illuminatedAT NEXT MX OVERNIGHT PLEASE TROUBLESHOOT REPEAT WRITE UPS FOR L 10TH DUCT WARNING MSGSMCI TYPE: TROUBLESHOOTING PRIORITY 1 (FLIGHT 5035 FILED CLOSED)APR 06, 2024 STATION: DEN--INSPECTED AND FOUND FIRE LOOPS CONTACTING ONE ANOTHER AND DUCTING. REPOSITIONED LOOSDR SWIA20240317Skin · bentRH AILERON UPPER SKIN IS BENT BETWEEN HINGES #2 AND #3. (C-CHECK RO 4/3/2024) REMOVED DAMAGED RH AILERON UPPER LEADING EDGE SKIN & INSTALLED NEW RH AILERON UPPER LEADING EDGE SKIN IAW CRJ 200 SRM 51-42-21 & DWG NO. CC670-13000 REV. -DINSTALLED BRACKETS ONTSDR SWIA20240222Doubler · crackedCRACK NOTED ON CARGO DOOR SILL SUPPORT CLIP ATTACHED TO FWD SIDE OF FRAME 589 (MARKED) (C-CHECK RO 4/3/2024) REPLACED LH CARGO DOOR SILL SUPPORT CLIP AT FS 589 WITH NEW FABRICATED CLIP 601R35011-11 REF CRJ 200 SRM 51-42-21 AND DWG 601R35011 REV R. COMPLIESDR SWIA20240216Floor Support · corrodedNUMEROUS CORROSIONS NOTED ON L/H PRESSURE FLOOR SILL ANGLE BETWEEN FS409.00+128 TO FS559.00 (MARKED) (C-CHECK RO 4/3/2024) REMOVED CORROSION ON NUMEROUS AREAS ON LH PRESSURE FLOOR SILL ANGLE BETWEEN FS409.00+128 - FS559 8 AREAS IN TOTAL. AREAS ARE LABELED SDR SWI2024F00273Seat Track · corrodedSEAT RAIL FS364-FS394 LBL9 CORROSION, HN00139361 (C-CHECK RO 4/3/2024) REMOVED AND REPLACED SEAT RAIL FS364 - FS394 LBL9 REF CRJ200 AMM53-01-11-000-802 AND AMM53-01-11-400-802SDR SWI202400270Floorbeam · corrodedCABIN FLOOR FS280 CROSS BEAM LBL9- RBL9 HAS AREAS OF CORROSION, HN00139344 (C-CHECK RO 4/3/2024) REMOVED AND REPLACED F.S. 280 CROSS BEAM FGLOOR SUPPORT ANGLE BETWEEN LBL 9 AND RBL 9 WITH NEW, REF CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-21, CRJ 200 SRMSDR SWI2024F00272Floor Support · corrodedNUMEROUS CORROSIONS NOTED ON R/H PRESSURE FLOOR SILL BETWEEN FS409.00+128 TO FS559.00 (MARKED) (C-CHECK RO 4/3/2024) REMOVED CORROSION ON R/H PRESSURE FLOOR SILL BETWEEN FS409.00+128 TO FS559.00 AT 18 EA AREAS (MARKED) REF CRJ200 SRM 51-21-06. . COMPLIED WSDR SWI2024F00271Floor Support · corrodedNUMEROUS CORROSIONS NOTED ON L/H PRESSURE FLOOR SILL BETWEEN FS409.00+128 TO FS559.00 (MARKED) (C-CHECK RO 4/3/2024) REMOVED CORROSION ON L/H PRESSURE FLOOR SILL BETWEEN FS409.00+128 TO FS559.00 AT 8 EA AREAS (MARKED) REF CRJ200 SRM 51-21-06. . COMPLIED WISDR SWI2024F00270Crossbeam · corrodedCABIN FLOOR FS280 CROSS BEAM LBL9- RBL9 HAS AREAS OF CORROSION, HN00139344 (C-CHECK RO 4/3/2024) REMOVED AND REPLACED F.S. 280 CROSS BEAM FGLOOR SUPPORT ANGLE BETWEEN LBL 9 AND RBL 9 WITH NEW, REF CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-21, CRJ 200 SRMSDR SWI2024F00279Door Sill · corrodedCORROSION NOTED AT CARGO DOOR SILL (MARKED) (C-CHECK RO 4/3/2024) REMOVED AND REPLACED WITH NEW, CARGO FLOOR LANDING PLATE (FLOOR SILL) 601R35011-63 AND RE-INSTALLED EXISTING REPAIR PARTS REF CRJ 200 SRM 51-42-06 , DWG 601R35011 REV R AND REO 601R-53-61-59SDR SWI2024F00278Stringer · corrodedCORROSION NOTED ON STRG SUPPORT FITTING ON STRG 27 AFT OF FRAME 559+112 (MARKED) (C-CHECK RO 4/3/2024) STRINGER TIE CLIP SUPPORT ANGLES P/N 601R31057-139 & -140, FABRICATED FROM S6144-33 ANGLE (.050" 7075-T62, RADIUS .12) PO# 5000008296-000010, IAW DWG 601SDR SWI2024F00277Drain Mast · wornCORROSION NOTED INNER BASE PLATE FOR AFT DRAIN MAST AFT OF FRAME 589 BTWN STRG26R-STRG25R (MARKED) (C-CHECK RO 4/3/2024) REMOVED AND REPLACED AFT DRAIN MAST MOUNTING PLATE WITH NEW, REF CRJ 200 SRM 51-42-06 AND DWG 601R43216 REV -D, OPS TEST GOOD, LEAK CHSDR SWI2024F00276Hinge · wornCOMPLY WITH CUURENT REVISION OF EA RJ3292-52 REPLACEMENT OF PASSENGER DOOR PIANO HINGE OPTION D3 (C-CHECK RO 4/3/2024) REMOVED DOOR HINGE, PERFORMED CUTTING TO CENTER HINGE AND TRIMMED TO FIT 2 EA. FWD AND AFT HINGE SECTIONS. BACK-DRILLED 4 EA HOLES IN NEWSDR SWIA20240215Hinge · wornCOMPLY WITH CURRENT REVISION OF EA RJ3296-53 REPLACEMENT OF PASSENGER DOOR PIANO HINGE OPTION F3 (C-CHECK RO 4/3/2024) COMPLIED WITH E.A. NO. RJ3296-53 REV C DATED: 03/28/2024, REPLACEMENT OF PASSENGER DOOR PIANO HINGE OPTION F3 WITH HINGE REMOVAL. COMPLIESDR SWIA20240214Skin · dentedPROTRUDING DENT NOTED ON L/H EXTERNAL SKIN 3"-6" BELOW L/H WINDSHIELD SIDE POST AT APPROX. FS235.00 (MARKED) (C-CHECK RO 4/3/2024) CUT AWAY FS 235.0 FRAME UPPER FLANGE AND DRESSED BACK DENT ON FUSELAGE SKIN AT FS 235.0 BETWEEN STR 11L-12L TO ORIGINAL CONTOSDR SWIA20240211Stringer · gougedEVALUATE CRACK ON STRINGER 8R BETWEEN FS280 AND FS295.0 INTERIOR CABIN. PERFORMED REPAIR ON STR 8R BETWEEN FS280.00 TO FS 295.00 IAW CRJ 200 REO 601R-53-21-3688 REV -- DATE:2024-04-29,SRM 53-00-00,SRM 51-26-01,SRM 51-42-21,SRM 51-42-06,SRM 51-21-11 AND SRM 5SDR SWIA20240207Seal · corrodedBOTTOM OF SERVICE DOOR HAS CORROSION MARKED (C-CHECK RO 4/3/2024) REMOVED AND REPLACED SERVICE DOOR CORRODED LWR AFT FORMER WITH NEW, REF CRJ 200 SRM 51-42-06 AND DWG 601R38304 REV BN, PRESSURE LEAK CHECK GOODCOMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKYSDR SWIA20240201Skin · dentedDENT NOTED AT R/H INBD FLAP EXTERNAL LOWER SKIN AT APPROX. 2" FROM T/E AND 5" FROM INBD EDGE (MARKED) (C-CHECK RO 4/3/2024) R/H I/B FLAP EXTERNAL LOWER SKIN DENT HAS BEEN REPAIRED REF CRJ 200 SRM 57-52-00. SEE CONTINUATION SHEET FOR DETAILS. COMPLIED FULLSDR SWI2024F00274Fairing · chafedRH INBOARD FLAP HAS CHAFFING 2 AREAS WHERE CANOE FAIRING 683BB AND 686BB CONTACT LOWER SKIN (C-CHECK RO 4/3/2024) BLENDED-OUT DAMAGE AND EVALUATED LIMITATIONS ON RHS INBOARD FLAP LOWER SKIN AT FLAP-STA-74.718 AND FLAP STA-135.512, THE SUBJECT REWORKED CONDSDR SWI2024F00275Vane · chafedLH INBOARD FLAP VANE CHAFFED ON OUTBOARD LEADING EDGE (C-CHECK RO 4/3/2024) L/H I/B FLAP VANE, OUTBOARD LEADING EDGE CHAFFING BLENDED IAW CRJ 200 SRM 51-12-00 AND FOUND TO BE BEYOND LIMITS IAW CRJ 200 SRM 57-20-00 AND REO 601R-57-52-004 REV.-D, DATED 2012-SDR SWIA202266353None · failedON CLIMB OUT IN TEENS ON ENGINE BLEED SOURCE R PACK HI PRESS CAUTION MESSAGE. RAN QRH, DID NOT RECOVER RIGHT HAND PACK. CONTINUED CLIMB, GOT L PACK HI PRESS CAUTION MESSAGE. RAN QRH. WAS ABLE TO RECOVER LH PACK. RETURNED TO FIELD. (FLIGHT #5593 FILED CLOSED)SDR SWIA202265930None · odorSTRONG EXHAUST SMELL IN THE COCKPIT DURING DESCENT. PACK 1 SHOWING TEMPERATURE OUTPUT OF -6C. (FLIGHT 5928 - FILED CLOSED) PERFORMED FIM TASK 21-21-00. FOUND NO DAMAGE OR DEFECTS. RAN BOTH ENGINES REF AMM 71-00-00 AND OPERATED BOTH PACKS ON ENGINE BLEEDS FSDR SWIA202052768Heat Shield · crackedAPU EXHAUST SHEILD CRACKED AT THE 6 O'CLOCK POSITION. FILED CLOSED (9/23/2020). REMOVED AND REPLASED THE APU EXHAUST SHIELD AND SUPPORT ASSY, IAW AMM.SDR SWIA2020041750177Doubler · damagedPAX DOOR SURROUND LOWER FWD CORNER DAMAGED DURING PAX DOOR INSTALL (C-CHECK) RO 4/16/2020 REMOVED DAMAGED DOUBLER AND INSTALLED NEW DOUBLER AND FILLER ON PAX DOOR SURROUND LOWER FWD CORNER REF CRJ200 SRM. SEE CONTINUATION CARD FOR DETAILS.SDR SWIA2020041750176Hinge Fitting · wornUPON REMOVAL ON JOB 2795595 OP 93 CAMP 20686462, FOUND R/H ELEVATOR L/E HINGE FITTING ASSY P/N 600-24043-1 @ ES16.52 TO BE EXCESSIVELY WORN AT BEARING LOCATION. REPLACE HINGE FITTING ASSY. (C-CHECK) RO 4/16/2020 REMOVED WORN R/H ELEVATOR L/E HINGE FITTISDR SWIA2020041750175Retainer · chafedPAX DOOR UPPER CENTER RETAINER SEAL CHAFED/GOUGED (C-CHECK) RO 4/16/2020 BLENDED OUT CHAFE/GOUGE ON PAX DOOR UPPER CENTER SEAL RETAINER. REF CRJ 200 (TR51-44) SRM. PAX DOOR UPPER CENTER SEAL RETAINER ORIGINAL MATERIAL THICKNESS IS 0.050" IAW BOMBARDIER DWSDR SWIA2020041750174Hinge Fitting · wornUPON REMOVAL ON JOB 2795595 OP 92 CAMP 20686457, FOUND L/H ELEVATOR L/E HINGE FITTING ASSY P/N 600-24043-1 @ ES16.52 TO BE EXCESSIVELY WORN AND CORRODED AT BEARING LOCATION. REPLACE HINGE FITTING ASSY. (C-CHECK) RO 4/16/2020 REMOVED WORN L/H ELEVATOR LSDR SWIA2020041750173Angle · crackedRHS BATT RIB CAP ANGLE CRACKED AT WS48.30 (P/N 600-10389-2). (C-CHECK) RO 4/16/2020 REMOVED AND REPLACED RHS BATT RIB ANGLE AT WS48.30 (P/N 600-10389-2) REF DWG AND CRJ200 SRM.SDR SWIA2020041750172Door Frame · corrodedPASSENGER DOOR: FRAME LOCATED AT FS313.56 BETWEEN INTERCOSTALS DD4 AND DD5 HAS CORROSION. (MARKED). (C-CHECK) RO 4/16/2020 WHILE REMOVING CORROSION ON FRAME FS313.56 BETWEEN INTERCOSTAL DD4 AND DD5 FOUND SEVERE CORROSION ON 3EA ELEMENTS AND ON MORE THAN 40SDR SWIA2020041750171Intercostal · corrodedPASSENGER DOOR: INTERCOSTAL DD4 HAS CORROSION (MARKED). (C-CHECK) RO 4/16/2020 CORROSION IS PRESENT ON ALL 3EA ELEMENTS AND COVERS MORE THAN 30% OF PART OUT OF LIMITS REF CRJ200 SRM. REPLACE INTERCOSTAL DD4. REMOVED PAX DOOR MID DD4 INTERCOSTAL IAW CRJ 20SDR SWIA2020041750170Intercostal · corrodedPASSENGER DOOR: INTERCOSTALL DD3 IS CORRODED (MARKED). (C-CHECK) RO 4/16/2020 CORROSION IS PRESENT ON ALL 3EA ELEMENTS AND COVERS MORETHAN 30% OF THE LENGHT OF PART OUT OF LIMITS REF CRJ200 SRM. REMOVED PAX DOOR MID INTERCOSTAL DD3 IAW CRJ 200 SRM. INSTASDR SWIA2020041750169Intercostal · corrodedPASSENGER DOOR: INTERCOSTAL DD2 IS CORRODED (MARKED). (C-CHECK) RO 4/16/2020 CORROSION IS PRESENT ON MORE THAN 80% OF THE LENGHT OF PART AND FOUND ON 3EA ELEMENTS. OUT OF LIMITS REF CRJ200 SRM. REMOVED AND REPLACED NEW PAX DOOR MID DD2 INTERCOSTAL IAW CRJSDR SWIA2020041750168Former · corrodedPASSENGER DOOR: FORMER LOCATED AT FS347.27 IS CORRODED (MARKED). (C-CHECK) RO 4/16/2020 REMOVED AND REPLACED PASSENGER DOOR FORMER LOCATED AT FS 347.27 REF BOMBARDIER DWG, CRJ-200-SRM. SEE CONTINUATION CARD FOR DETAILSSDR SWIA2020041750190Skin · corrodedWHILE REMOVING PASSENGER DOOR INNER SKIN FOUND CORROSION ON INNER SURFACE AT MULTIPLES LOCATIONS. (C-CHECK) RO 4/16/2020 REMOVED AND REPLACED PAX DOOR INNER SKIN. REF CRJ 200 SRM.SDR SWIA2020041750167Stiffener · crackedBOTTOM STIFFENER CRACKED OUTBOARD OF LBL36 ON AFT SIDE OF FS621 BULKHEAD. (C-CHECK) RO 4/16/2020 REMOVED AND REPLACED BOTTOM STIFFENER OUTBOARD OF LBL36 ON AFT SIDE OF FS621 BULKHEAD REF CRJ-200 SRM AND BOMBARDIER DWG. PRESSURIZATION LEAK CHECK GOOD.SDR SWIA2020041750166Angle · crackedLH BATT RIB ANGEL AT WS48.30 HAS A CRACK ON AFT END (P/N 600-10204-27). (C-CHECK) RO 4/16/2020 REMOVED AND REPLACED DAMAGED BATT RIB ANGLE AT WS48.30 LHS PER DWG AND CRJ200 SRM.SDR SWIA2020041750165Skin · worn* R/H WING FUEL ACCESS PANEL LOCATION 650CB HAS PITTING ON EDGE (MARKED) (C-CHECK) RO 4/16/2020 BLENDED OUT DAMAGED AREAS AS REQUIRED ON RH WING FUEL ACCESS PANEL LOCATION 650CB PER REO. GAP CHECK AND LEAK CHECK ARE GOOD. SEE CONTINUATION FOR DETAILS.SDR SWIA2020041750164Skin · worn* L/H WING FUEL ACCESS PANEL LOCATION 510AB INBOARD EDGE HAS PITTING (MARKED) (C-CHECK) RO 4/16/2020 BLENDED OUT DAMAGE AREAS OF LH WING FUEL ACCESS PANEL 510AB PER REO. BLEND OUT IS OUT OF LIMITS. RECEIVED REO. ROTO PEENED AND RESTORED REWORKED AREA. SEESDR SWIA2020041750163Skin · worn* FUEL ACCESS PANEL LOCATION WING PLANK PERIMETER.550HB HAS PITTING AND DEEP WEAR GROOVE MARKING .(MARKED) (C-CHECK) RO 4/16/2020 BLENDED OUT DAMAGE AREAS OF LH WING FUEL ACCESS PANEL 550HB PER REO. BLEND OUT IS OUT OF LIMITS. RECEIVED REO. ROTO PEENED AND
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