# Service difficulty reports: N983SW

A list on [N983SW](https://openairdocs.org/aircraft/N983SW.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 4 · 200 reports

- [SDR SWIA2026032375566](https://openairdocs.org/sdr/SWIA2026032375566.md): Flap System · faulted · Mar 23, 2026 · N983SW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP 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
- [SDR SWIA2026031175509](https://openairdocs.org/sdr/SWIA2026031175509.md): A/C Pack · odor · Mar 11, 2026 · N983SW · Cndair CL6002B19 · Airborne Auxiliary Power Unit (APU) System
  > INTERMITTENT 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 AM
- [SDR SWIA2026011300003](https://openairdocs.org/sdr/SWIA2026011300003.md): Warning Message · illuminated · Jan 3, 2026 · N983SW · Cndair CL6002B19 · Engine Thrust Reverser
  > LEFT 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. DMI
- [SDR SWIA2026010500003](https://openairdocs.org/sdr/SWIA2026010500003.md): Thrust Reverser · warning message · Jan 3, 2026 · N983SW · Cndair CL6002B19 · Engine Thrust Reverser
  > LEFT 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 SERVICE
- [SDR SWIA20251002901](https://openairdocs.org/sdr/SWIA20251002901.md): Rib · damaged · Sep 1, 2025 · N983SW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > RH 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 T
- [SDR SWIA20251002802](https://openairdocs.org/sdr/SWIA20251002802.md): Skin · dented · Aug 2, 2025 · N983SW · Cndair CL6002B19 · Wing, Plate/Skin
  > RH 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 TAS
- [SDR SWIA20251002702](https://openairdocs.org/sdr/SWIA20251002702.md): Skin · cracked · Jul 2, 2025 · N983SW · Cndair CL6002B19 · Wing, Plate/Skin
  > COMPLY 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. (FI
- [SDR SWIA20251002627](https://openairdocs.org/sdr/SWIA20251002627.md): Skin · cracked · Jun 27, 2025 · N983SW · Cndair CL6002B19 · Wing, Plate/Skin
  > TRANSFER 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 NE
- [SDR SWIA2025051916](https://openairdocs.org/sdr/SWIA2025051916.md): Skin · dented · May 16, 2025 · N983SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > SHEETMETAL 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 RE
- [SDR SWIA20231023002](https://openairdocs.org/sdr/SWIA20231023002.md): Windshield · damaged · Oct 22, 2023 · N983SW · Cndair CL6002B19 · Windshield/Door Rain/Ice Removal
  > ENROUTE 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)
- [SDR SWIA20230928809](https://openairdocs.org/sdr/SWIA20230928809.md): Unknown · gouged · Aug 9, 2023 · N983SW · Cndair CL6002B19 · Wing, Control Surface Attach Fittings
  > RT 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 COM
- [SDR SWI2023F00387](https://openairdocs.org/sdr/SWI2023F00387.md): Unknown · dented · Aug 5, 2023 · N983SW · Cndair CL6002B19 · Doors
  > FOUND 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 DE
- [SDR SWIA20230928805](https://openairdocs.org/sdr/SWIA20230928805.md): Unknown · chafed · Aug 5, 2023 · N983SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > L/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 COMPLIED
- [SDR SWIA2023092800803](https://openairdocs.org/sdr/SWIA2023092800803.md): Unknown · corroded · Aug 3, 2023 · N983SW · Cndair CL6002B19 · Fuselage Structure (General)
  > INTERIOR 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. COMP
- [SDR SWI2023F00379](https://openairdocs.org/sdr/SWI2023F00379.md): Unknown · chafed · Aug 3, 2023 · N983SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING 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 RH
- [SDR SWIA20230928002](https://openairdocs.org/sdr/SWIA20230928002.md): Unknown · corroded · Aug 2, 2023 · N983SW · Cndair CL6002B19 · Standard Practices/Structures
  > INTERIOR 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-
- [SDR SWI2023F00380](https://openairdocs.org/sdr/SWI2023F00380.md): Unknown · cracked · Jul 28, 2023 · N983SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FS280 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-
- [SDR SWI2023F00383](https://openairdocs.org/sdr/SWI2023F00383.md): Unknown · corroded · Jul 28, 2023 · N983SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS280 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. BOMBARDI
- [SDR SWI2023F00382](https://openairdocs.org/sdr/SWI2023F00382.md): Unknown · corroded · Jul 28, 2023 · N983SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX 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 AM
- [SDR SWI2023F00381](https://openairdocs.org/sdr/SWI2023F00381.md): Unknown · cracked · Jul 28, 2023 · N983SW · Cndair CL6002B19 · Fuselage Main, Structure
  > *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 51-900
- [SDR SWIA20230928727](https://openairdocs.org/sdr/SWIA20230928727.md): Unknown · dented · Jul 27, 2023 · N983SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > EXTERIOR 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 TA
- [SDR SWIA20230928725](https://openairdocs.org/sdr/SWIA20230928725.md): Unknown · damaged · Jul 25, 2023 · N983SW · Cndair CL6002B19 · Vertical Stabilizer
  > DURING 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 O
- [SDR SWI2023F00386](https://openairdocs.org/sdr/SWI2023F00386.md): Unknown · damaged · Jul 25, 2023 · N983SW · Cndair CL6002B19 · Horizontal Stabilizer, Spar/Rib
  > DURING 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
- [SDR SWI2023F00385](https://openairdocs.org/sdr/SWI2023F00385.md): Unknown · cracked · Jul 24, 2023 · N983SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > L/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 WS
- [SDR SWIA20230928724](https://openairdocs.org/sdr/SWIA20230928724.md): Unknown · cracked · Jul 24, 2023 · N983SW · Cndair CL6002B19 · Fuselage Main, Structure
  > R/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 51-42
- [SDR SWI2023F00384](https://openairdocs.org/sdr/SWI2023F00384.md): Unknown · corroded · Jul 22, 2023 · N983SW · Cndair CL6002B19 · Wing, Plate/Skin
  > OPENING 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-S
- [SDR SWIA20230928722](https://openairdocs.org/sdr/SWIA20230928722.md): Unknown · pulled · Jul 22, 2023 · N983SW · Cndair CL6002B19 · Trailing Edge Flaps
  > CAMP #: 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 ON
- [SDR SWIA20230928721](https://openairdocs.org/sdr/SWIA20230928721.md): Unknown · damaged · Jul 21, 2023 · N983SW · Cndair CL6002B19 · Wing, Control Surface Attach Fittings
  > LH 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.
- [SDR SWIA20230928718](https://openairdocs.org/sdr/SWIA20230928718.md): Unknown · dented · Jul 18, 2023 · N983SW · Cndair CL6002B19 · Emergency Exits
  > COCKPIT 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 51
- [SDR SWI2023F00388](https://openairdocs.org/sdr/SWI2023F00388.md): Unknown · scratched · Jul 17, 2023 · N983SW · Cndair CL6002B19 · Trailing Edge Flaps
  > * 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 FIN
- [SDR SWIA20230928717](https://openairdocs.org/sdr/SWIA20230928717.md): Unknown · gouged · Jul 17, 2023 · N983SW · Cndair CL6002B19 · Wing Main, Frame Structure
  > LH 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 WITH
- [SDR SWIA20230928716](https://openairdocs.org/sdr/SWIA20230928716.md): Unknown · worn · Jul 16, 2023 · N983SW · Cndair CL6002B19 · Ailerons
  > LEFT 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 2019
- [SDR SWIA2022122267022](https://openairdocs.org/sdr/SWIA2022122267022.md): Flap System · faulted · Dec 21, 2022 · N983SW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS 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
- [SDR SWIA202266613](https://openairdocs.org/sdr/SWIA202266613.md): None · failed · Oct 14, 2022 · N983SW · Cndair CL6002B19 · Overheat Detection
  > D: 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 CAUTI
- [SDR SWIA202266589](https://openairdocs.org/sdr/SWIA202266589.md): None · none · Oct 4, 2022 · N983SW · Cndair CL6002B19 · Overheat Detection
  > UPON 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.
- [SDR SWIA2020042350248](https://openairdocs.org/sdr/SWIA2020042350248.md): Stringer Clip · cracked · Apr 7, 2020 · N983SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FS625.00, 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 CRJ200
- [SDR SWIA2020042350255](https://openairdocs.org/sdr/SWIA2020042350255.md): Stiffener · cracked · Apr 2, 2020 · N983SW · Cndair CL6002B19 · Passenger/Crew Doors
  > STIFFNER 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 SRM
- [SDR SWIA2020042350247](https://openairdocs.org/sdr/SWIA2020042350247.md): Stringer Clip · cracked · Apr 2, 2020 · N983SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FS 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.
- [SDR SWIA2020042350246](https://openairdocs.org/sdr/SWIA2020042350246.md): Door Sill · out of limits · Mar 31, 2020 · N983SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH 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.
- [SDR SWIA2020042350245](https://openairdocs.org/sdr/SWIA2020042350245.md): Floorbeam · cracked · Mar 31, 2020 · N983SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS.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 CAR
- [SDR SWIA2020042350254](https://openairdocs.org/sdr/SWIA2020042350254.md): Drag Angle · cracked · Mar 26, 2020 · N983SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER 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.
- [SDR SWIA2020042350244](https://openairdocs.org/sdr/SWIA2020042350244.md): Rib · cracked · Mar 26, 2020 · N983SW · Cndair CL6002B19 · Trailing Edge Flaps
  > ON 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.
- [SDR SWIA2020042350242](https://openairdocs.org/sdr/SWIA2020042350242.md): Hinge Fitting · corroded · Mar 26, 2020 · N983SW · Cndair CL6002B19 · Elevator Structure
  > UPON 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 FI
- [SDR SWIA2020042350241](https://openairdocs.org/sdr/SWIA2020042350241.md): Vane · worn · Mar 26, 2020 · N983SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LH 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.
- [SDR SWIA2020042350240](https://openairdocs.org/sdr/SWIA2020042350240.md): Vane · worn · Mar 26, 2020 · N983SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LH 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.
- [SDR SWIA2020042350235](https://openairdocs.org/sdr/SWIA2020042350235.md): Floorbeam · cracked · Mar 26, 2020 · N983SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS.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 DETA
- [SDR SWIA2020042350239](https://openairdocs.org/sdr/SWIA2020042350239.md): Intercostal · cracked · Mar 25, 2020 · N983SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER 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.
- [SDR SWIA2020042350238](https://openairdocs.org/sdr/SWIA2020042350238.md): Intercostal · cracked · Mar 25, 2020 · N983SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER 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.
- [SDR SWIA2020042350237](https://openairdocs.org/sdr/SWIA2020042350237.md): Stringer · corroded · Mar 24, 2020 · N983SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRG. 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.
- [SDR SWIA2020042350236](https://openairdocs.org/sdr/SWIA2020042350236.md): Bracket · cracked · Mar 24, 2020 · N983SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * " 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, CR

Next page: https://openairdocs.org/aircraft/N983SW/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N983SW/reports

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