# Service difficulty reports: N958SW

A list on [N958SW](https://openairdocs.org/aircraft/N958SW.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 5 · 210 reports

- [SDR SWIA2026053076740](https://openairdocs.org/sdr/SWIA2026053076740.md): Skin · cracked · May 30, 2026 · N958SW · Cndair CL6002B19 · Wing, Plate/Skin
  > ONE CRACK, LT WING AFT LOWER PLANK. DWG 601R10046, 7475 T7351. AFT EDGE AT WS 45. CRACK IS 1.3? LONG AND STARTS FROM AFT EDGE OF LT AFT LOWER WING PLANK AT WS 45. OPEN.
- [SDR SWIA2026042175906](https://openairdocs.org/sdr/SWIA2026042175906.md): Skin · gouged · Apr 21, 2026 · N958SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA83611-601R-52-31-401. PERFORM PERMANENT REPAIR OF THE TEMPORARY DISPOSITION FOR GOUGE DAMAGE TO THE CARGO DOOR OUTER SKIN UPPER EDGE BETWEEN FS 589 & FS 605 PER REO 601R-52-31-401REV -- DATED 4/11/2023. COMPLIED PER
- [SDR SWIA2026020975905](https://openairdocs.org/sdr/SWIA2026020975905.md): Skin · dented · Feb 9, 2026 · N958SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DURING ADM INSPECTION, FOUND QUARTER SIZE DENT AFT AND BELOW GROUND AIR CONNECTION DOOR, ON RHS AFT FUSLEAGE AT APPROXIMATELY BETWEEN FS605 AND FS621, BELOW WL73.50 AT APPROXIMATE BETWEEN STGR 22R TO STGR19R. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE
- [SDR SWIA2025110575904](https://openairdocs.org/sdr/SWIA2025110575904.md): Lock Fastener · corroded · Nov 5, 2025 · N958SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA93631-601R-53-61-8227 N958SW MXCODEID77499-PR - COMPLY WITH PERMANENT REPAIR ON RA ID: 93631CARGO DOOR SURROUNDING STRUCTURE, AFT CORNER SILL ANGLE AT WL73.50 & FS621.00 HAS MSSING PAINT/SURFACE CORROSION. PERFORMED
- [SDR SWIA2025042106](https://openairdocs.org/sdr/SWIA2025042106.md): Retainer · bent · Apr 16, 2025 · N958SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR SEAL RETAINER BENT TOPSIDE FLOOR LEVEL FWD SIDE (FLIGHT 5049) REMOVED AND REPLACED PAX DOOR LOWER FWD AND LOWER CENTER SEAL RETAINERS WITH REFERENCE TO REO 601R-52-11-915 REV--. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA202503190018](https://openairdocs.org/sdr/SWIA202503190018.md): Bleed Valve · malfunctioned · Mar 18, 2025 · N958SW · Cndair CL6002B19 · Compressor Bleed Valve
  > DUE TO PACK AND PRESSURIZATION ISSUES A/C REQUIRES SMOD APPROVAL BEFORE FURTHER FLIGHT. REF. EAML 1564978MCI TYPE: SERVICEABLE / NEEDS ATTENTION (FLIGHT 5762 - FILED CLOSED) MAR 18, 2025 STATION: DEN--REMOVED AND REPLACED RH 10TH STAGE BLEED AIR SOV PER
- [SDR SWIA20240903](https://openairdocs.org/sdr/SWIA20240903.md): Skin · damaged · Sep 3, 2024 · N958SW · Cndair CL6002B19 · Passenger/Crew Doors
  > DAMAGE FOUND ON THE PAX DOOR FORWARD SIDE, HALFWAY DOWN FROM THE TOP WITH DOOR OPEN. (FILED CLOSED) REPAIRED DAMAGE ON THE PAX DOOR FORWARD SIDE, HALFWAY DOWN FROM THE TOP WITH THE DOOR OPEN (INNER SKIN BETWEEN DATUM 3-4 AT FS 311.75) WITH REFERENCE TO R
- [SDR SWIA2024092000004](https://openairdocs.org/sdr/SWIA2024092000004.md): Door · damaged · Sep 3, 2024 · N958SW · Cndair CL6002B19 · Passenger/Crew Doors
  > DAMAGE FOUND ON THE PAX DOOR FORWARD SIDE, HALFWAY DOWN FROM THE TOP WITH DOOR OPEN. (FILED OPEN) REPAIRED DAMAGE ON THE PAX DOOR FORWARD SIDE, HALFWAY DOWN FROM THE TOP WITH THE DOOR OPEN (INNER SKIN BETWEEN DATUM 3-4 AT FS 311.75) WITH REFERENCE TO REO
- [SDR SWI2024F01101](https://openairdocs.org/sdr/SWI2024F01101.md): Door Frame · corroded · Sep 2, 2024 · N958SW · Cndair CL6002B19 · Fuselage Main, Structure
  > CARGO DOOR SURROUNDING STRUCTURE, AFT CORNER SILL ANGLE AT WL73.50 & FS621.00 HAS MSSING PAINT/SURFACE CORROSION. (FILED CLOSED) PERFORMED TEMPORARY REPAIR OF CORNER SILL ANGLE AT WL73.50 & FS621.00 WITH REFERENCE TO REO 601R-53-61-8227 REV "--" DATED 20
- [SDR SWIA20240902](https://openairdocs.org/sdr/SWIA20240902.md): Track · cracked · Sep 2, 2024 · N958SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR FORWARD TRACK LOWER BRACKET CRACKED, JUST ABOVE CARGO LIGHT SWITCH. (FILED CLOSED) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA2024092000003](https://openairdocs.org/sdr/SWIA2024092000003.md): Angle · corroded · Sep 2, 2024 · N958SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR SURROUNDING STRUCTURE, AFT CORNER SILL ANGLE AT WL73.50 & FS621.00 HAS MSSING PAINT/SURFACE CORROSION. (FILED OPEN) PERFORMED TEMPORARY REPAIR OF CORNER SILL ANGLE AT WL73.50 & FS621.00 WITH REFERENCE TO REO 601R-53-61-8227 REV "--" DATED 2024
- [SDR SWIA2024090300002](https://openairdocs.org/sdr/SWIA2024090300002.md): Bracket · cracked · Sep 2, 2024 · N958SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CARGO DOOR FORWARD TRACK LOWER BRACKET CRACKED, JUST ABOVE CARGO LIGHT SWITCH. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA2024092000002](https://openairdocs.org/sdr/SWIA2024092000002.md): Pressure Blkhd · gouged · Aug 27, 2024 · N958SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD FORWARD FACE HAS 1 GOUGE ON DOUBLER AT LBL27.50, 3 GOUGES AT LBL18.00, 2 GOUGES AT LBL9.50, 1 GOUGE AT RBL18.00, 1 GOUGE AT RBL 27.50, AND 1 GOUGE AT RBL35.20 (MARKED WITH TAPE) (FILED CLOSED) COMPLIED WITH REO 601R-53-61-8224 DATED
- [SDR SWIA202411150826](https://openairdocs.org/sdr/SWIA202411150826.md): Frame · chafed · Aug 26, 2024 · N958SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FOUND CHAFE DAMAGE ON FS 718.00 BETWEEN STGR 16R AND STGR 17R (FILED CLOSED) COMPLIED WITH REO 601R-53-61-8219 DATED: 2024-09-11 REV -- REPAIR TO FRAME FS718.00 BETWEEN STR16R - STR17R. ALL NDTS COMPLIED WITH AND NO DEFECTS NOTED AT THIS TIME. COMPLIED W
- [SDR SWIA2024092000826](https://openairdocs.org/sdr/SWIA2024092000826.md): Frame · chafed · Aug 26, 2024 · N958SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FOUND CHAFE DAMAGE ON FS 718.00 BETWEEN STGR 16R AND STGR 17R (FILED OPEN) COMPLIED WITH REO 601R-53-61-8219 DATED: 2024-09-11 REV -- REPAIR TO FRAME FS718.00 BETWEEN STR16R - STR17R. ALL NDTS COMPLIED WITH AND NO DEFECTS NOTED AT THIS TIME. COMPLIED WIT
- [SDR SWIA20240825](https://openairdocs.org/sdr/SWIA20240825.md): Floor Skin · corroded · Aug 25, 2024 · N958SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > CORROSION FOUND ON SEVERAL AREAS OF THE RH PRESSURE FLOOR SILL FS424.00, FS439.00, FS461.00, AND FS473.15 (FILED CLOSED) BLENDED CORROSION ON THE RH PRESSURE FLOOR SILL FS424.00, FS439.00, FS461.00, AND FS473.15 WITH REFERENCE TO SRM 51-21-06. PERFORMED
- [SDR SWI20240920000837](https://openairdocs.org/sdr/SWI20240920000837.md): Floor Support · corroded · Aug 25, 2024 · N958SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON SEVERAL AREAS OF THE LH PRESSURE FLOOR SILL AT FS439.00, FS449.85, FS461.00, FS 473.15, FS499.00, FS513.00, AND FS529.00 (FILED CLOSED) BLENDED CORROSION ON THE LH PRESSURE FLOOR SILL FS439.00, FS449.85, FS461.00, FS 473.15, FS499.00,
- [SDR SWIA2024092000001](https://openairdocs.org/sdr/SWIA2024092000001.md): Floor Support · corroded · Aug 25, 2024 · N958SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON SEVERAL AREAS OF THE RH PRESSURE FLOOR SILL FS424.00, FS439.00, FS461.00, AND FS473.15 (FILED OPEN) BLENDED CORROSION ON THE RH PRESSURE FLOOR SILL FS424.00, FS439.00, FS461.00, AND FS473.15 WITH REFERENCE TO SRM 51-21-06. PERFORMED U
- [SDR SWIA202156963](https://openairdocs.org/sdr/SWIA202156963.md): Strut · failed · Mar 14, 2021 · N958SW · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > GEAR DISAGREE WARNING MESSAGE AFTER DEPARTURE, NOSE GEAR DID NOT RETRACT, COMPLIED WITH QRH PROCEDURE. FLIGHT 5038. REMOVED AND REPLACED SERVICEABLE NLG DRESSED ASSEMBLY REFERENCE CAMP #22467199 FOR INSTALLATION.
- [SDR SWIA202156856](https://openairdocs.org/sdr/SWIA202156856.md): Fitting · cracked · Feb 4, 2021 · N958SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > UPPON REMOVAL OF PAX DOOR AFT FRAME FORMER FOUND UPPER FITTING FOR AFT FRAME FORMER TO BE CRACKED (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED FITTING IAW CRJ 200 SRM 51-42-21, REFER TO CONTINUE CARD FOR WORK PERFORMED
- [SDR SWIA202156840](https://openairdocs.org/sdr/SWIA202156840.md): Intercostal · corroded · Feb 2, 2021 · N958SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR MIDDLE INTERCOSTAL AT DD3 IS CORRODED (C-CHECK) RO 3/10/2021 REMOVED AND INSTALLED SERVICEABLE PAX DOOR MIDDLE INTERCOSTAL AT DD3 IAW CRJ 200 SRM 51-40-11, 51-42-06 AND 51-42-21 REV 38B DATED 11/25/2020. COMPLIED WITH TASK CARD 51-900-1003-SKY (
- [SDR SWIA202156841](https://openairdocs.org/sdr/SWIA202156841.md): Window Frame · damaged · Feb 1, 2021 · N958SW · Cndair CL6002B19 · Fuselage Main, Structure
  > FOUND INDICATION R/H LOWER OUTER FLANGE WINDSHIELD SIDE POST WL 110 PROTRUDING FROM FASTNER HOLE 80% FSH APPROX..250 LONG FAILS NDT (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED RH SIDE POST IAW CRJ 200 SRM 51-42-21 AND REF DWG PL601R3307. COMPLETED TASK
- [SDR SWIA202156843](https://openairdocs.org/sdr/SWIA202156843.md): Intercostal · corroded · Jan 28, 2021 · N958SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR FWD INTERCOSTAL BETWEEN DD4 AND DD5 IS CORRODED (C-CHECK) RO 3/10/2021 REMOVED AND INSTALLED SERVICEABLE PAX DOOR FWD INTERCOSAL BETWEEN DD4 AND DD5 IAW CRJ 200 SRM 51-42-06 AND 51-40-11 REV 38B DATED 25 NOV 2020. COMPLIED WITH TASK CARD 51-90
- [SDR SWIA202156842](https://openairdocs.org/sdr/SWIA202156842.md): Intercostal · corroded · Jan 28, 2021 · N958SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL AT DD2 IS CORRODED (C-CHECK) RO 3/10/2021 REMOVED AND INSTALLED SERVICEABLE DD2 INTERCOSAL IAW CRJ 200 SRM 51-42-06 AND 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY (CL600-2B19). FORM 337 COMPLETED. PART FOR PART REPLACEMENT, NO
- [SDR SWIA202156835](https://openairdocs.org/sdr/SWIA202156835.md): Intercostal · corroded · Jan 28, 2021 · N958SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR FWD INTERCOSTAL AT DD3 IS CORRODED (C-CHECK) RO 3/10/2021 REMOVED AND INSTALLED SERVICEABLE DD3 INTERCOSAL IAW CRJ 200 SRM 51-40-11 AND 51-42-06 REV 38B DATED 11-25-2020. COMPLIED WITH TASK CARD 51-900-1003-SKY (CL600-2B19). FORM 337 COMPLETED. P
- [SDR SWIA202156852](https://openairdocs.org/sdr/SWIA202156852.md): Drain · gouged · Jan 26, 2021 · N958SW · Cndair CL6002B19 · Fuselage Structure (General)
  > FOUND LH & RH DRAIN HOLES LOCATED AT BOOST PUMP BL11 BETWEEN STGR 5 AND STGR 7 FWD AND AFT ATTACHMENT HOLES HAS GOUGES LOCATED IN BORES FAILED VISUAL INSPECTION ( 4 HOLES IN TOTAL) (C-CHECK) RO 3/10/2021 REMOVED DAMAGE AND COMPLIED WITH REO 601R-57-21-3
- [SDR SWIA202156865](https://openairdocs.org/sdr/SWIA202156865.md): Support Angle · corroded · Jan 25, 2021 · N958SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND SUPPORT ANGLE AT F.S 349 LBL 38 TO 27 TO BE CORRODED. (C-CHECK) RO 3/10/2021 REPLACED THE SUPPORT ANGLE AT FS 349 LBL 38 TO 27 IAW CRJ 200 SRM 51-42-06.
- [SDR SWIA202156864](https://openairdocs.org/sdr/SWIA202156864.md): Skin · corroded · Jan 22, 2021 · N958SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > EXTERIOR SKIN SURFACE HAS MINOR CORROSI0ON IN MULTIPLE SPOTS FROM F.S. 559.00+32 TO F.S. 559.00+48 FROM STRGR 25L TO 25R (C-CHECK) RO 3/10/2021 COMPLIED W. REO 601R-53-51-557 REV-- DATED 2021-02-04. REFERENCE CONTINUATION TO SEE WORK PERFORMED
- [SDR SWIA202156838](https://openairdocs.org/sdr/SWIA202156838.md): Skin · corroded · Jan 22, 2021 · N958SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > EXTERIOR SKIN SURFACE HAS MINOR CORROSI0ON IN MULTIPLE SPOTS FROM F.S. 559.00+80 TO F.S. 559.00+112 FROM STRGR 25L TO 25R (C-CHECK) RO 3/10/2021 REPAIRED MINOR CORRODED AREAS OF EXTERIOR SKIN FROM FS559.00+80 TO FS 559.00+112 FROM STRGR 25L TO 25R IAW M
- [SDR SWIA202156863](https://openairdocs.org/sdr/SWIA202156863.md): Floor Support · corroded · Jan 21, 2021 · N958SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR BEAM AT RBL 9 HAS MULTIPLE SPOTS OF CORROSION FROM F.S. 409.00+128 TO F.S. 559.00 (C-CHECK) RO 3/10/2021 COMPLIED W. MHIRJ REO 601R-53-41-2863 REV-- DATED 2021-02-08 AND MHIRJ 601R-53-00-005 REV-B DATED 2011-01-06
- [SDR SWIA202156855](https://openairdocs.org/sdr/SWIA202156855.md): Intercostal · cracked · Jan 21, 2021 · N958SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CLIP AT F.S. 484.00 BETWEEN RBL27 AND RBL36 IS CRACKED (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED INTERCOSTAL CLIP AT F.S. 484.00 BETWEEN RBL27 AND RBL36. REFER TO THE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA202156854](https://openairdocs.org/sdr/SWIA202156854.md): Intercostal · cracked · Jan 21, 2021 · N958SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CLIP AT F.S. 484.00 CRACKED BETWEEN LBL27 AND LBL36 (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED INTERCOSTAL CLIP AT F.S. 484.00 REFERENCE THE CONTINUATION CARD FOR THE WORK PERFORMED.
- [SDR SWIA202156846](https://openairdocs.org/sdr/SWIA202156846.md): Floor Support · corroded · Jan 21, 2021 · N958SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH PRESSURE FLOOR SILL HAS MULTIPLE SPOTS CORROSION FROM F.S. 409.00=128 TO F.S. 559.00 (C-CHECK) RO 3/10/2021 REMOVED CORROSION FORM RH PRESSURE FLOOR SILL FROM FS 409+128 TO FS 559 AND FOUND TO BE WITHIN LIMITS IAW REO 601R-53-41-666 REV C DATED 2012-11
- [SDR SWIA202156839](https://openairdocs.org/sdr/SWIA202156839.md): Floor Support · cracked · Jan 21, 2021 · N958SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT F.S. 484.00 AND RBL18 IS CRACKED. (C-CHECK) RO 3/10/2021 REPAIRED INTERCOSTAL AT FS 484.00 AND RBL 18 IAW MHIRJ REO 601R-53-41-2869 REV -- DATED 2021-02-17 AND SKYCARD 51-900-1003-SKY NO WEIGHT CHANGE, M-337 AND M-131 ARE ATTACHED.
- [SDR SWIA202156836](https://openairdocs.org/sdr/SWIA202156836.md): Floor Support · corroded · Jan 21, 2021 · N958SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LH PRESSURE FLOOR SILL HAS MULTIPLE SPOTS CORROSION FROM F.S. 409.00=128 TO F.S. 559.00 (C-CHECK) RO 3/10/2021 REMOVED CORROSION FRO, LH PRESSURE FLOOR SILL AT FS 425, FS 453, FS 475, AND FS 494 AND FOUND TO BE WITHIN LIMITS IAW REO 601R-53-41-666 REV C D
- [SDR SWIA202156845](https://openairdocs.org/sdr/SWIA202156845.md): Frame · damaged · Jan 20, 2021 · N958SW · Cndair CL6002B19 · Fuselage Main, Frame
  > WHILE EVALUATING CORROSION REMOVAL ON FS 605 FRAME FOUND SEVERAL MIS DRILLED HOLES FROM PREVIOUS REPAIR ON EXTERNAL SKIN. (C-CHECK) RO 3/10/2021 REMOVED DAMAGED SKIN AND REPAIRED AREA IAW REO 601R-53-61-7556 REV -- DATED 2021-02-09. COMPLIED WITH TASK CAR
- [SDR SWIA202156862](https://openairdocs.org/sdr/SWIA202156862.md): Seat Track · corroded · Jan 19, 2021 · N958SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN FLOOR SEAT TRACK RBL 9 BETWEEN FS 559.00 TO FS 559+68 IS CORRODED (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED CABIN SEAT TRACK AT RBL9 BETWEEN FS559.00 TO FS559+68 IAW CRJ200 AMM 53-01-11-946/400-003/802 REFER TO CONTINUATION CARD FOR WORK PERFORME
- [SDR SWIA202156861](https://openairdocs.org/sdr/SWIA202156861.md): Crossbeam · corroded · Jan 18, 2021 · N958SW · Cndair CL6002B19 · Fuselage Main, Structure
  > LHS CABIN FS 349 CROSSBEAM IS CORRODED AT RBL 39 OB END OF CROSSBEAM (C-CHECK) RO 3/10/2021 REMOVED ITEMS SUPPORT ANGLE PART NUMBER (601R38673-43), PART NUMBER 601R38672-9 & IAW CRJ200 SRM 51-42-06 AND 51-42-21 REFERENCE THE CONTINUATION CARD FOR THE WOR
- [SDR SWIA202156851](https://openairdocs.org/sdr/SWIA202156851.md): Former · corroded · Jan 18, 2021 · N958SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT FRAME FORMER IS CORRODED (C-CHECK) RO 3/10/2021 REMOVED AND INSTALLED SERVICEABLE PAX DOOR AFT FORMER IAW CRJ 200 SRM 51-40-11,51-42-06 AND 51-42-21 REV 38B DATED 25NOV 2020. COMPLIED WITH TASK CARD 51-900-1003-SKY (CL600-2B19). FORM 337 COM
- [SDR SWIA202156850](https://openairdocs.org/sdr/SWIA202156850.md): Intercostal · corroded · Jan 18, 2021 · N958SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR DD6 INTERCOSTAL IS CORRODED (C-CHECK) RO 3/10/2021 REMOVED AND INSTALLED SERVICEABLE PAX DOOR DD6 INTERCOSAL IAW CRJ 200 SRM 51-42-06, 51-40-11, 51-21-11 AND 51-42-21 REV 38B DATED 25 NOV 2020. COMPLIED WITH TASK CARD 51-900-1003-SKY (CL600-2B19
- [SDR SWIA202156847](https://openairdocs.org/sdr/SWIA202156847.md): Skin · corroded · Jan 18, 2021 · N958SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INNER SKIN HAS AREAS OF CORROSION ADJACENT TO DATUM 6 AND INSIDE CUTOUTS FOR PANELS 832HL AND 832GR AFT SIDE OF THE DOOR (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED PAX DOOR INNER SKIN IAW CRJ 200 SRM 51-42-06,51-42-13, 51-42-21 AND 51-42-15.
- [SDR SWIA202156844](https://openairdocs.org/sdr/SWIA202156844.md): Former · corroded · Jan 18, 2021 · N958SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FWD FORMER IS CORRODED (C-CHECK) RO 3/10/2021 REMOVED AND INSTALLED SERVICEABLE PAX DOOR FWD FORMER IAW CRJ 200 SRM 51-40-11, 51-42-06 AND 51-42-21 REV 38B DATED 25 NOV 2020. COMPLIED WITH TASK CARD 51-900-1003-SKY (CL600-2B19). FORM 337 COMPLE
- [SDR SWIA202156860](https://openairdocs.org/sdr/SWIA202156860.md): Tube · corroded · Jan 17, 2021 · N958SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RH IB FLAP IB FLAP VANE ACTUATOR IS CORRODED WHERE IT ATTACHES TO THE FLAP VANE REMOVED AND REPLACED THE TUBE ASSY ON THE RH IB FLAP IB VANE ACTUATOR IAW BOMBARDIER CMM 57-59-00. REFER TO THE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA202156859](https://openairdocs.org/sdr/SWIA202156859.md): Pcu · corroded · Jan 17, 2021 · N958SW · Cndair CL6002B19 · Aileron Control System
  > RH AILERON IB PCU AFT CLEVIS IS CORRODED (C-CHECK) RO 3/10/2021 REMOVED REPLACED RH AILERON IB PCU IAW CRJ 200 AMM 27-14-01-400-801
- [SDR SWIA202156858](https://openairdocs.org/sdr/SWIA202156858.md): Pcu · corroded · Jan 17, 2021 · N958SW · Cndair CL6002B19 · Aileron Control System
  > RH WING AILERON OB PCU IS CORRODED ON THE AFT CLEVIS (C-CHECK) RO 3/10/2021 REMOVED REPLACED RH WING OB PCU IAW CRJ 200 AMM27-14-01-400-801
- [SDR SWIA202156870](https://openairdocs.org/sdr/SWIA202156870.md): Stop Fitting · chafed · Jan 15, 2021 · N958SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR FORWARD UPPER STOP FITTING ON FUSELAGE AFT CORNER IS CHAFED INTO BARE METAL. (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED PAX DOOR UPPER STOP FIITTING IAW CRJ 200 SRM 51-41-02
- [SDR SWIA202156869](https://openairdocs.org/sdr/SWIA202156869.md): Fitting · chafed · Jan 15, 2021 · N958SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR AFT UPPER CAM FITTING ON FUSELAGE LOWER CORNER IS CHAFED INTO BARE METAL. (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED PAX DOOR AFT CAM FITTING IAW CRJ200 AMM 53-21-23-000/400-803 OPS TEST GOOD
- [SDR SWIA202156868](https://openairdocs.org/sdr/SWIA202156868.md): Fitting · chafed · Jan 15, 2021 · N958SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR FORWARD UPPER CAM FITTING ON FUSELAGE LOWER CORNER IS CHAFED INTO BARE METAL. (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED PAX DOOR UPPER FWD CAM FITTING IAW CRJ200 AMM 53-21-23-000/400-803 OPS TEST GOOD
- [SDR SWIA202156857](https://openairdocs.org/sdr/SWIA202156857.md): Bolt · corroded · Jan 15, 2021 · N958SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LOWER SILL FORWARD AND AFT ATTACHMENT FITTINGS HAVE CORRODED ATTCHMNET BOLTS ( QTY 12) INTO FRAME AND THROUGH BOLTS FOR LATCH MECHANISM ( QTY 2). (C-CHECK) RO 3/10/2021 FOUND 8 EA OF THE 12 EA BOLTS IN THE SERVICE DOOR LOWER SILL, FWD AND A
- [SDR SWIA202156837](https://openairdocs.org/sdr/SWIA202156837.md): Skin · corroded · Jan 14, 2021 · N958SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > SURFACE CORROSION ON FUSELAGE SKIN AROUND MULTIPLE NUTPLATE HOLES FOR FUSELAGE TO WING FAIRINGS 191BB AND 192BB (C-CHECK) RO 3/10/2021 REMOVED CORROSION AND REPAIRED FUSELAGE SKIN AT FUSELAGE TO WING FAIRING 191BB AND 192 BB IAW REO 601R-53-31-1176 REV --

Next page: https://openairdocs.org/aircraft/N958SW/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 = 'N958SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N958SW/reports

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