N983SW

Service difficulty reports · 200

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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 = 'N983SW'
  ORDER BY difficulty_date DESC"

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SDR SWIA2026032375566Flap System · faultedFLAP FAIL CAUTION AT 25,000FT PASSING 290KTS. FLAPS FAILED AT 0. FLAPS WERE RETRACTED AT 1,000FT PER CLIMB PROFILE. AD 2009-06-12/10CAT A DUE IN 10 FC FROM TAC 42226 (DUE AT TAC 42236) (FLIGHT 5047 - FILED CLOSED) MAR 24, 2026 STATION: DEN--RESET AND Mar 23, 2026 · N983SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA2026031175509A/C Pack · odorINTERMITTENT ENGINE OIL ODOR IN CABIN/COCKPIT DURING CRUISE/DESCENT FROM VENTS. WENT AWAY AFTER BLEED SOURCE SWAPPED TO APU DURING DESCENT (FLIGHT 6068). TROUBLESHOT PER FIM 79-20-01 FOR ODORS IN INTERIOR OF THE ACFT. PERFORMED OPS CHECK OF BOTH PACKS IAW AMMar 11, 2026 · N983SW · Cndair CL6002B19 · Airborne Auxiliary Power Unit (APU) SystemSDR SWIA2026011300003Warning Message · illuminatedLEFT REVERSER UNLOCKED IN CLIMB. MEL 78-30-1 CAT: C. : REF FIM 78-30-00 FIG. 103 FOR TROUBLE SHOOTING (FLIGHT 5029) DEFERRED PER MEL 78-30-1 MX ACTION C/W AIRCRAFT OK FOR CONTINUED SERVICE. REFERENCE CP 31495856 AND CP31495864 FOR ALL WORK COMPLETED. DMIJan 3, 2026 · N983SW · Cndair CL6002B19 · Engine Thrust ReverserSDR SWIA2026010500003Thrust Reverser · warning messageLEFT THRUST REVERSER UNLOCKED IN CLIMB. REF FIM 78-30-00 FIG. 103 FOR TROUBLE SHOOTING (FLIGHT 5029) DEFERRED PER MEL 78-30-1 MX ACTION C/W AIRCRAFT OK FOR CONTINUED SERVICEJan 3, 2026 · N983SW · Cndair CL6002B19 · Engine Thrust ReverserSDR SWIA20251002901Rib · damagedRH WING LE RIB AT WS 86.45 HAS DAMAGE AROUND LIGHTENING HOLE. (FILED CLOSED)COMPLIED WITH REO 601R-57-41-1202 DATED: 2025-09-04 REV: --TEMPORARY REPAIR TO RH WING FIXED L/E WS 86.45 RIB LIGHTENING HOLE DAMAGE. ALL NDT'S COMPLIED WITH AND NO DEFECTS NOTED AT TSep 1, 2025 · N983SW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR SWIA20251002802Skin · dentedRH LEADING EDGE 620JL HAS DENT (4.5" X 2.5" X 5/32") ON NOSE @ APPROX. WS.96.34. (FILED CLOSED)REMOVED AND REPLACED THE RH WING LEADING EDGE SKIN FROM WS 86.450 TO WS 139.54 IN REFERENCE WITH THE SRM 51-42-06, SRM 51-40-11 AND SRM 57-41-31. COMPLIED WITH TASAug 2, 2025 · N983SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA20251002702Skin · crackedCOMPLY WITH LATEST REVISION SB NO. 601R-57-044 TITLE: WINGS - LOWER WING PLANK - COLD WORK OF FASTENER HOLES IN THE LOWER WING PLANK PART C LEFT SIDE AT BL45.00, PART D LEFT SIDE AT WS 65.75, PART F RIGHT SIDE AT BL45.00, AND PART G RIGHT SIDE AT WS65.75. (FIJul 2, 2025 · N983SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA20251002627Skin · crackedTRANSFER FROM EAML 1639970 : TRANSFERRED FROM CAMP 30382930. REFERENCE CP 30339577 "DURING REQUESTED EDDY CURRENT OF THE LH WING PLANK (SEE CP 30339238-1), FOUND CRACK INDICATION IN FASTENER HOLE FORWARD OF THE LH MLG TEMINATING AFT IN THE MIDDLE LAYER.THIS NEJun 27, 2025 · N983SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2025051916Skin · dentedSHEETMETAL REPAIR REQUIRED ON DENT LOCATED AT FS 409.00+108 BETWEEN STGR 14 AND STGR 15 ON RH SIDE OF AC FUSELAGE. (FILED CLOSED)SHEETMETAL REPAIR REQUIRED ON DENT LOCATED AT FS 409.00+108 BETWEEN STGR 14 AND STGR 15 ON RH SIDE OF AC FUSELAGE COMPLETED PER REMay 16, 2025 · N983SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA20231023002Windshield · damagedENROUTE LEFT WINDSHIELD IN UPPER LEFT CORNER STARTED TO GLOW AND STRANDS OR VEINS OF ELECTRICITY ABOUT 4 TO 6 INCHES SPREAD BETWEEN LAYERS OF GLASS. TURNED OFF WINDSHIELD HEAT AND IT DID STOP. KEPT IT OFF THE REST OF THE AND RAN QRH. (FLIGHT 5688 FILED CLOSED)Oct 22, 2023 · N983SW · Cndair CL6002B19 · Windshield/Door Rain/Ice RemovalSDR SWIA20230928809Unknown · gougedRT WING TRAILING EDGE, SUPPORT BRACKET BENT AND GOUGED JUST OUTBOARD OF R2 FLAP ACTUATOR. (C-CHECK RO 9/26/2023) REMOVED DAMAGED SECTION OF SUPPORT BRACKET AND INSTALLED REPAIR ANGLE P/N 601R-57-51-1024-1 NDT INSPECTED NO DEFECTS NOTED RESTORED FINISH COMAug 9, 2023 · N983SW · Cndair CL6002B19 · Wing, Control Surface Attach FittingsSDR SWI2023F00387Unknown · dentedFOUND AFT EQ BAY DOOR HAS DENT ON A CENTER INTERCOSTAL (C-CHECK RO 9/26/2023) REPLACED AFT EQUIPMENT BAY DOOR, FWD "CHANNEL" P/N 600-35128-59 REF BOMBARDIER ENG DWG 600-35128 REV H AND CRJ 200 SRM 51-42-06 COMPLIED WITH SKY CARD 51-900-1003 FOR COMPLETE DEAug 5, 2023 · N983SW · Cndair CL6002B19 · DoorsSDR SWIA20230928805Unknown · chafedL/H FUSELAGE APRON SKIN PANEL AT F/S 409+128 TO F/S 559.00 BELOW WL 73.50 HAS DEEP CHAFING (C-CHECK RO 9/26/2023) REPAIRED L/H FUSELAGE APRON SKIN PANEL AT F/S 409+128 TO F/S 559.00 BELOW WL 73.50 IAW REO 601R-53-41-115 REV. A DATED 2005-07-20 AND COMPLIEDAug 5, 2023 · N983SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2023092800803Unknown · corrodedINTERIOR FS409.0+128-FS559.0 RIGHT SILL HAS CORROSION IN VARIOUS AREAS (C-CHECK RO 9/26/2023) REPAIRED CORROSION ON THE R/H FLOOR SILL PANEL BETWEEN FS409.00+128 TO FS559.00 AT VARIOUS LOCATIONS ( 9 EA.) REF REO 601R-53-41-666 REV-C, DATED 2012-11-06. COMPAug 3, 2023 · N983SW · Cndair CL6002B19 · Fuselage Structure (General)SDR SWI2023F00379Unknown · chafedDURING AUDIT OF 2C TASK CARD 53-160-320(EXTERNAL ZONAL INSPECTION OF THE OVERWING-TO-FUSELAGE PANELS,FS409.00+128 TO FS559.00, BELOW WL73.50) FOUND LH AND RH APRON SKIN HAS CHAFING WHERE FLAP IS RUBBING. (C-CHECK RO 9/26/2023) REPAIRED DAMAGE SECTION OF RHAug 3, 2023 · N983SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA20230928002Unknown · corrodedINTERIOR FS409.0+128-FS559.0 LEFT SILL HAS CORROSION IN VARIOUS AREAS (C-CHECK RO 9/26/2023) REPAIRED CORROSION AT VARIOUS AREAS ON THE MAIN CABIN INTERIOR, LEFT SIDE FLOOR SILL BETWEEN FS 409.00+128 - FS 559.00 REF REO 601R-53-41-666 REV -C DATED 2012-11-Aug 2, 2023 · N983SW · Cndair CL6002B19 · Standard Practices/StructuresSDR SWI2023F00380Unknown · crackedFS280 LBL9 INBOARD ANGLE CLIP CRACKED (MARKED) (C-CHECK RO 9/26/2023) REMOVED AND INSTALLED NEW ANGLE CLIP AT F/S 280 INBOARD OF LBL 9.0. IAW REO 601R-53-11-926 REV. B DATED 2006/05/10 STEP 8, 9, 10, 11, 12, 13 AND 14 AND COMPLIED WITH SKYCARD 51-900-1003-Jul 28, 2023 · N983SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWI2023F00383Unknown · corrodedFS280 BEAM BETWEEN RBL9 AND LBL9 ANGLE HAS CORROSION (MARKED). (C-CHECK RO 9/26/2023) REPAIRED CORROSION ON FS280 BEAM BETWEEN RBL9 AND LBL9 ANGLE REF. REO 601R-53-11-3884 REV - A, DATED 2023-08-18 & GREO 601R-53-11-136 REV - A, DATED 2007/11/01. BOMBARDIJul 28, 2023 · N983SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWI2023F00382Unknown · corrodedPAX DOOR FWD HANDRAIL CAP (CLEAT) BETWEEN FS310.00 TO FS319.00 HAS CORROSION (MARKED) (C-CHECK RO 9/26/2023) FOUND FWD HANDRAIL BRACKET/ CLEAT OUT OF LIMITS REF CRJ 200 SRM 53-00-00 FIG 102 AND INSTALLED A NEW BRACKET AND CLEAT REF DRAWING 601R31527 REV AMJul 28, 2023 · N983SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWI2023F00381Unknown · cracked*SUSPECTED CRACK AT R/H TRU SKIN ADJACENT TO FRAME193 (MARKED),MX#26952018 (C-CHECK RO 9/26/2023) REPAIRED RH TRU FLOOR PANEL SKIN ADJACENT TO FRAME AT FS193 PER REO 601R-53-11-245 REV -C DATED: 2019-05-13 REPAIR TYPE II.COMPLETED SKYWEST TASK CARD 51-900Jul 28, 2023 · N983SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA20230928727Unknown · dentedEXTERIOR LOWER SKIN FS589.0-FS605.0 STGR 24-22 RIGHT MULTIPLE DENTS (C-CHECK RO 9/26/2023) REPAIRED EXTERIOR LOWER SKIN AT FS 589.0 -FS 605.0 STGR 24-22 RIGHT AS PER CRJ 200 SRM 51-42-06 AND REO 601R-53-61-8064 REV -- DATED 2023-08-23. M-337 AND SKYWEST TAJul 27, 2023 · N983SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA20230928725Unknown · damagedDURING AUDIT OF 2C TASK CARD 55-320-322 ( INTERNAL ZONAL INSPECTION OF THE VERTICAL STABILIZER TIP ), FOUND THE VERTICAL STABILIZER LH FWD. TRUNNION I/B & O/B FACE HAS SEVERAL AREAS OF IMPACT DAMAGE. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OJul 25, 2023 · N983SW · Cndair CL6002B19 · Vertical StabilizerSDR SWI2023F00386Unknown · damagedDURING THE AUDIT OF 96_72MO TASK CARD 55-320-517 DETAILED INSPECTION OF THE TOP CANTED RIB AND HORIZONTAL STABILIZER TRIM ACTUATOR PIVOT STRUCTURE, FOUND LH INNER PIVOT FITTING UPPER FWD & AFT RADIUS EDGE APPEARS TO HAVE IMPACT DAMAGE PLOT, MAP, AND EVALUATE Jul 25, 2023 · N983SW · Cndair CL6002B19 · Horizontal Stabilizer, Spar/RibSDR SWI2023F00385Unknown · crackedL/H SIDE WHEEL WELL BATT ANGLE FWD STRAP IS CRACKED AT WS 48.30 (MARKED) (C-CHECK RO 9/26/2023) LOCATED AND DRILLED NEW L/H SIDE WHEEL WELL BATT ANGLE P/N 600-10204-27 AT WS 48.30 REF CRJ200 SRM 51-40-11. INSTALLED NEW L/H SIDE WHEEL WELL BATT ANGLE AT WSJul 24, 2023 · N983SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA20230928724Unknown · crackedR/H SIDE MLG WHEEL WELL HAS AT FWD AND AFT END OF BATT RIB EXTRUSION( CRACKS 2EA.) (MARKED) WS 48.30 (C-CHECK RO 9/26/2023) REMOVED AND REPLACED THE R/H SIDE MLG WHEEL WELL BATT RIB CAP ANGLE , P/N 600-10389-2 REF DWG 600-10389 REV NC AND CRJ200 SRM 51-42Jul 24, 2023 · N983SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWI2023F00384Unknown · corrodedOPENING FOR 640CT HAS CORROSION ON UPPER AND LOWER SURFACE OF WING PLANK (C-CHECK RO 9/26/2023) REPAIRED CORROSION ON 640CT OPENING UPPER AND LOWER SURFACE OF WING PLANK REF. MHIRJ REO 601R-57-21-3781 REV - -, DATED 2023-08-04. COMPLIED WITH 51-900-1003-SJul 22, 2023 · N983SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA20230928722Unknown · pulledCAMP #: 26922152RIGHT OUTBOARD FLAP. UPPER SKIN, CENTER SECTION HAS NUMEROUS SMOKING RIVETS AND SERVERAL RIVETS ON THE TRALING EDGE PULLING THRU THE SKIN. (C-CHECK RO 9/26/2023) REMOVED AND REPLACED NUMEROUS (26 EA.) SMOKING AND PULLED THROUGH FASTENERS ONJul 22, 2023 · N983SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA20230928721Unknown · damagedLH WING FLAP BOX ATTACH FITTING WS 178.00 INBOARD AFT SIDE HAS ABRASION DAMAGE AS MARKED. (C-CHECK RO 9/26/2023) REPAIRED ABRASION DAMAGE TO THE LH WING FLAP BOX ATTACH FITTING AT WS 178.00 INBOARD AFT SIDE REF REO 601R-57-21-3779 REV--, DATED 2023-07-27. Jul 21, 2023 · N983SW · Cndair CL6002B19 · Wing, Control Surface Attach FittingsSDR SWIA20230928718Unknown · dentedCOCKPIT EMERGENCY HATCH HAS DENTED EXTERNAL SKIN EDGE ON FWD RH CORNER (C-CHECK RO 9/26/2023) REPAIRED DENTED EXTERNAL SKIN EDGE ON FWD RH CORNER IAW CRJ 200 REO 601R-52-22-050 REV - - DATED 2023-08-06. SEE CONTINUATION CARD FOR WORK ACCOMPLISHED. C/W 51Jul 18, 2023 · N983SW · Cndair CL6002B19 · Emergency ExitsSDR SWI2023F00388Unknown · scratched* RIGHT OUTBOARD FLAP, INBOARD AFT HINGE BOX FITTING HAS A SCRATCH ON THE AFT END. (C-CHECK RO 9/26/2023) BLENDED TOOLING MARKS ON R/H INBD HINGE BOX LUG FITTING P/N 601R10930-6 AT WS178.00 TO A SMOOTH FINISH NDT INSPECTED NO DEFECTS NOTED AND RESTORED FINJul 17, 2023 · N983SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA20230928717Unknown · gougedLH HINGE BOX AT WS.178.00 IS GOUGED DUE TO DEBRIS (SCREW) (C-CHECK RO 9/26/2023) BLENDED OUT DAMAGE ON LH HINGE BOX AT WS178.00. REF. CRJ200 SRM 51-12-00. FOUND OUT OF LIMITS. NO DAMAGE ALLOWED AT HINGE BOX WS178.00. REF. CRJ200 SRM 57-21-55. COMPLIED WITHJul 17, 2023 · N983SW · Cndair CL6002B19 · Wing Main, Frame StructureSDR SWIA20230928716Unknown · wornLEFT AILERON LEADING EDGE UPPER AND LOWER IS WORN (MARKED) (C-CHECK RO 9/26/2023) BLENDED OUT WORN AREAS ON THE LEFT AILERON LEADING EDGE UPPER AND LOWER SKIN SHROUD ON THE INBD AND OTBD SIDES REF CRJ-200 SRM 51-12-00 AND REO 670-57-61-194 REV-C DATE 2019Jul 16, 2023 · N983SW · Cndair CL6002B19 · AileronsSDR SWIA2022122267022Flap System · faultedFLAPS FAIL WHEN SELECTING FLAPS 30, FLAPS FAILED AT 20. (FLIGHT 5019) RESET AND OPERATED FLAPS 5 FULL CYCLES AND COMPLETED AD 2009-06-12/10 COMPLIANCE FORM. OK TO CONTINUE IN SERVICE FOR 10 FLIGHT CYCLES. COMPLIED IAW FIM FMRP 27, RESET PROCEDURES AND AD Dec 21, 2022 · N983SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA202266613None · failedD: CREW REPORTS APU FIRE FAIL CAUTION MESSAGE ON SHORT FINAL. DEFERRED APU FIRE DETECTION LOOPS PER MEL 26-12-1B. NO MX ACTION REQ'D & PLACARD INSTALLED. / C: MEL 26-12-1B / CAT C DUE 10/24/22 / SEE A/C MX LOG #1012872 / CREW REPORTS APU FIRE FAIL CAUTIOct 14, 2022 · N983SW · Cndair CL6002B19 · Overheat DetectionSDR SWIA202266589None · noneUPON STARTING THE APU, WE RECEIVED APU OVERTEMP WARNING MESSAGE FOLLOWED BY APU FIRE FAIL CAUTION MESSAGE. (FLIGHT #5130 FILED CLOSED) PERFORMED OPS CHECK OF APU IN REFERENCE TO AMM 49-10-00 AND OPS CHECK OF APU FIRE DETECTION IN REFERENCE TO AMM 26-12-00.Oct 4, 2022 · N983SW · Cndair CL6002B19 · Overheat DetectionSDR SWIA2020042350248Stringer Clip · crackedFS625.00, STGR 14R CLIP CRACKED. (C-CHECK) RO 4/21/2020 REMOVED DAMAGE CLIP AT FS625.00 STGR 14R. REF CRJ200 SRM. RECEIVED NEW CLIP PN# 601-35012-52. LOCATED HOLES IN REPLACEMENT CLIP REF CRJ200 SRM. INSTALLED REPLACEMENT FS625.00, STGR 14R CLIP REF CRJ200Apr 7, 2020 · N983SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA2020042350255Stiffener · crackedSTIFFNER ON PAX DOOR FWD WEB IS CRACKED AT FASTNER HOLE PN 601R317742-1. (C-CHECK) RO 4/21/2020 REPLACED STIFFNER ON PAX DOOR FWD WEB WITH NEW REF CRJ 200 SRMApr 2, 2020 · N983SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020042350247Stringer Clip · crackedFS 625.00, STGR 14L CLIP CRACKED. (C-CHECK) RO 4/21/2020 REMOVED AND INSTALLED NEW ANGLE CLIP PN# 601-35012-51, AT FS625.00 STGR 14L. REF CRJ200 SRM, BOMBARDIER DWG, AND REO. COMPLIED WITH TASK CARD. SEE CONTINUATION FOR DETAILS.Apr 2, 2020 · N983SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA2020042350246Door Sill · out of limitsRH FLOOR SILL FROM FS 559+112 TO FS 621.00 IS FOUND TO BE OUT OF LIMITS ON MX TRANS# 20678730 JOB# 2796191 OP# 272. REPLACE FLOOR SILL (C-CHECK) RO 4/21/2020 REMOVED AND REPLACED RH FLOOR SILL FROM FS 559+112 TO FS 621.00. REF: CRJ-200 SRM, REO AND DWG.Mar 31, 2020 · N983SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020042350245Floorbeam · crackedFS.280 COCKPIT FLOOR SUPPORT BETWEEN LBL11 AND RBL11 IS CRACKED. (C-CHECK) RO 4/21/2020 REMOVED CRACKED FS280.00 COCKPIT FLOOR SUPPORT BETWEEN LBL11 AND RBL11 AND INSTALLED NEW COCKPIT FLOOR SUPPORT REF BOMBARDIER DWG AND CRJ 200 SRM. SEE CONTINUATION CARMar 31, 2020 · N983SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2020042350254Drag Angle · crackedPASSENGER DOOR AFT DRAG ANGLE FOUND CRACKED. (C-CHECK) RO 4/21/2020 REMOVED AND REPLACED PASSENGER DOOR AFT DRAG ANGLE IN REF CRJ200 SRM. SEE CONTINUATION CARD FOR DETAILS.Mar 26, 2020 · N983SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020042350244Rib · crackedON THE LH IB FLAP, THE OB VANE RIB IS DAMAGED/CRACKED. (C-CHECK) RO 4/21/2020 REMOVED DAMAGED LH FLAP VANE OB RIB AND INSTALLED A NEW RIB REF CRJ 200 SRM AND DRAWING. COMPLIED WITH TASK CARD.Mar 26, 2020 · N983SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020042350242Hinge Fitting · corrodedUPON REMOVAL ON JOB 2796195 OP 76 CAMP 20680285, FOUND R/H ELEVATOR L/E HINGE FITTING ASSY P/N 600-24043-1 @ ES16.52 TO HAVE PITTING CORROSION IN BEARING BORE. REPLACE HINGE FITTING ASSY. (C-CHECK) RO 4/21/2020 REMOVED CORRODED R/H ELEVATOR L/E HINGE FIMar 26, 2020 · N983SW · Cndair CL6002B19 · Elevator StructureSDR SWIA2020042350241Vane · wornLH IB FLAP VANE OUTBOARD CAP NEEDS REPLACED DUE TO OUT OF LIMITS WEAR. (C-CHECK) RO 4/21/2020 REMOVED DAMAGED LH FLAP VANE IB CAP AND INSTALLED A NEW ONE REF CRJ 200 SRM AND DRAWING. COMPLIED WITH TASK CARD.Mar 26, 2020 · N983SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020042350240Vane · wornLH INBOARD FLAP CENTER VANE CAP NEEDS REPLACED DUE TO OUT OF LIMITS WEAR. (C-CHECK) RO 4/21/2020 LOCATED AND DRILLED NEW CENTER VANE CAP REF CRJ 200 SRM AND INSTALLED THE CENTER CAP REF DRAWING AND CRJ 200 SRM, SKY CARD COMPLETED.Mar 26, 2020 · N983SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020042350235Floorbeam · crackedFS.280.00 LOWER WEB IS CRACKED AT LBL9 AND RBL9. (C-CHECK) RO 4/21/2020 REMOVED AND INSTALLED NEW F.S 280 FWD FLOOR SUPPORT ANGLE AND REPAIRED F.S 280 FLOOR BEAM BETWEEN LBL 20.75 TO RBL 20.75 REF. BOMBARDIER REO. COMPLIED WITH TASK CARD. FOR COMPLETE DETAMar 26, 2020 · N983SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2020042350239Intercostal · crackedPASSENGER DOOR FWD SIDE INTERCOSTAL DD7 FOUND CRACKED. (C-CHECK) RO 4/21/2020 REMOVED AND REPLACED THE PAX DOOR FWD DD7 INTERCOSTAL REF CRJ 200 SRM & DWG. CHECKS GOOD. COMPLIED WITH SKYWEST TASK CARD.Mar 25, 2020 · N983SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020042350238Intercostal · crackedPASSENGER DOOR INTERCOSTAL DD7 FOUND CRACKED. (C-CHECK) RO 4/21/2020 RE3MOVED AND REPLACED THE PAX DOOR DD7 INTERCOSTAL REF CRJ 200 SRM & DWG. CHECKS GOOD. COMPLIED WITH SKYWEST TASK CARD.Mar 25, 2020 · N983SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020042350237Stringer · corrodedSTRG. 20R BETWEEN FS 310.00 TO FS 349.00 FOUND TO BE CORRODED UPON REMOVAL OF THE AFT INTERCOSTAL. (C-CHECK) RO 4/21/2020 REMOVED AND REPLACED STRINGER 20R, FS319-7 - FS349. REF CRJ-200 SRM AND BOMBARDIER DWG. SEE CONTINUATION CARD FOR DETAILS.Mar 24, 2020 · N983SW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA2020042350236Bracket · cracked* " T " BRACKET AT FS 461.50 OBD SIDE OF RBL 9 FLOOR BEAM CRACKED AT FS 461.50 AFT UPPER SIDE. (C-CHECK) RO 4/21/2020 REMOVED CRACKED "T" BRACKET AT FS461.50 OTBD SIDE OF RBL9 FLOOR BEAM AND INSTALLED NEW "T" BRACKET PN #600-31068-19 REF BOMBARDIER DWG, CRMar 24, 2020 · N983SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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