# Service difficulty reports: N464SW

A list on [N464SW](https://openairdocs.org/aircraft/N464SW.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 · 213 reports

- [SDR SWI2026F00086](https://openairdocs.org/sdr/SWI2026F00086.md): Fuel Control · broken · Jan 13, 2026 · N464SW · Cndair CL6002B19 · Fuel Control/Turbine Engines
  > NUMBER 1 ENGINE STUCK AT 70% N1 WITH THRUST LEVER AT IDLE. ENGINE 1 INDICATED MCT DURING THIS TIME. NO CAUTION MESSAGE, NO WARNING MESSAGE. WE CYCLED THE THRUST LEVER BY MOVING IT FORWARD AND BACK TO UNBIND THE THRUST LEVER CABLE. I DID NOT FEEL ANY BINDING OR
- [SDR SWI2026F00077](https://openairdocs.org/sdr/SWI2026F00077.md): Engine · malfunctioned · Jan 13, 2026 · N464SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > NUMBER 1 ENGINE STUCK AT 70% N1 WITH THRUST LEVER AT IDLE. ENGINE 1 INDICATED MCT DURING THIS TIME. NO CAUTION MESSAGE, NO WARNING MESSAGE. WE CYCLED THE THRUST LEVER BY MOVING IT FORWARD AND BACK TO UNBIND THE THRUST LEVER CABLE. I DID NOT FEEL ANY BINDING OR
- [SDR SWIA2025082500014](https://openairdocs.org/sdr/SWIA2025082500014.md): Smoke Detector · false activation · Aug 14, 2025 · N464SW · Cndair CL6002B19 · Smoke Detection
  > CREW REPORTS 2 LAV SMOKE TOILET IN CRUISE 32000 (FLIGHT 5070) REPLACEMENT AND OPS CHECK OF THE LAV SMOKE DETECTOR. AMM 21-51-10-000-801 SUBTASK 21-51-00-210-001 & VISUALLY INSPECT THE INLET FACE & CORE OF THE RT DUAL HEAT EXCHANGER AND FAN SECTION OF THE ACM
- [SDR SWIA2025081500014](https://openairdocs.org/sdr/SWIA2025081500014.md): Smoke Detector · warning message · Aug 14, 2025 · N464SW · Cndair CL6002B19 · Smoke Detection
  > CREW REPORTS 2 LAV SMOKE TOILET IN CRUISE 32000 (FLIGHT 5070 - FILED OPEN)
- [SDR SWIA2025011700010](https://openairdocs.org/sdr/SWIA2025011700010.md): Idg · power loss · Jan 10, 2025 · N464SW · Cndair CL6002B19 · AC Generator-Alternator
  > IDG1 CAUTION MESSAGE RAN QRH. DISCONNECTED PER QRH. AFTER IDG DISCONNECTED GEN 2 WENT OFFLINE. (FLIGHT 4651 - FILED CLOSED) PLEASE REFERENCE AML 1511384. ALL WORK ACCOMPLISHED. REVIEW AMLS. R&R IDG 2, #1 AND #2 GCU. R&R FILTERS ON #1 IDG. ALL OPS AND
- [SDR SWIA202410210015](https://openairdocs.org/sdr/SWIA202410210015.md): Window · cracked · Oct 15, 2024 · N464SW · Cndair CL6002B19 · Flight Compartment Windows
  > RIGHT COCKPIT WINDOW CRACKED INFLIGHT. (FLIGHT 5431 - FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 29004301 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVED AND REPLACED RH SIDE WINDOW IN REFERENCE TO AMM 56-12-01 AND TASK CARD 56-220-1000-SKY."
- [SDR SWIA202410160005](https://openairdocs.org/sdr/SWIA202410160005.md): Window · cracked · Oct 15, 2024 · N464SW · Cndair CL6002B19 · Flight Compartment Windows
  > RIGHT COCKPIT WINDOW CRACKED INFLIGHT. (FLIGHT 5431 - FILED OPEN)
- [SDR SWI2024F00100](https://openairdocs.org/sdr/SWI2024F00100.md): Skin · cracked · Jan 25, 2024 · N464SW · Cndair CL6002B19 · Horizontal Stabilizer, Plate/Skin
  > R/H H-STAB TRAILING EDGE SKIN CRACKED AND DENTED (C-CHECK RO 2/1/2024) COMPLIED WITH MHIRJ REO 601R-55-11-755 REV.-- DATED 2024-01-12 FOR REPAIR TO R/H H-STAB LOWER T/E SKIN. PERFORMED NDT ET INSPECTION OF DRESSED BACK AREA BY BARON NDT LLC, CRS # 5NDR545D
- [SDR SWIA20240202125](https://openairdocs.org/sdr/SWIA20240202125.md): Skin · gouged · Jan 25, 2024 · N464SW · Cndair CL6002B19 · Elevator, Plate/Skin
  > R/H ELEVATOR SKIN GOUGED AT PANEL 344BB WITH OUTBD LANDING TAB BENT (C-CHECK RO 2/1/2024) COMPLIED WITH MHIRJ REO 601R-55-21-590 REV.-- DATED 2024-01-12 FOR REPAIR TO R/H ELEVATOR SKIN AND OB LANDING TAB. PERFORMED NDT ET/UT INSPECTION OF THE BLENDED OUT G
- [SDR SWIA2024020231209](https://openairdocs.org/sdr/SWIA2024020231209.md): Floor Support · corroded · Dec 9, 2023 · N464SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SIGNS OF CORROSION ON FLOOR SUPPORT AT FS409.00+8 AND LBL9 AROUND FASTENER HOLE, NEEDS EVAL (FILED CLOSED)CORROSION REMOVAL FOUND TO BE OUT OF LIMITS ON FLOOR SUPPORT AT F.S.409.00+8 LBL9 IAW CRJ200 SRM 53-00-00, PERFORMED SPECIAL DETAILED ET/UT INSPECTION OF
- [SDR SWI2024F00099](https://openairdocs.org/sdr/SWI2024F00099.md): Seat Track · corroded · Nov 29, 2023 · N464SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > SEAT RAIL FROM F.S. 559.00 + 112 - 621 AT RBL 9 HAS CORROSION OUT OF LIMITS (FILED CLOSED)REMOVED AND REPLACED SEAT RAIL FROM F.S.559.00+112-621 AT RBL 9 IAW CRJ 200 AMM 53-00-49.
- [SDR SWIA2024020231129](https://openairdocs.org/sdr/SWIA2024020231129.md): Door Frame · damaged · Nov 29, 2023 · N464SW · Cndair CL6002B19 · Fuselage Main, Structure
  > PERFORM PERMANENT REPAIR TO FWD LOWER CORNER OF CARGO DOOR CUT OUT (C-CHECK RO 2/1/2024) REPAIRED FWD LOWER CORNER OF CARGO DOOR CUT-OUT IAW CRJ200 SRM 53-61-31 AND MHIRJ REO 601R-53-61-8128 REV.-- 2023-12-20, NDT PERFORMED BY BARON NDT,LLC, FAA CRS#5NDR54
- [SDR SWI2024F00107](https://openairdocs.org/sdr/SWI2024F00107.md): Seat Track · corroded · Nov 28, 2023 · N464SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAIL FROM F.S. 559.00 + 80 - 559.00 + 96 AT LBL 27 HAS SIGNS OF CORROSION (FILED CLOSED)REMOVED AND REPLACED SEAT RAIL FROM F.S, 559.00 + 80 - 559.00 + 96 AT LBL 27 IAW CRJ 200 AMM 53-01-11
- [SDR SWI2024F00106](https://openairdocs.org/sdr/SWI2024F00106.md): Seat Track · corroded · Nov 28, 2023 · N464SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAIL FROM F.S. 559.00 + 80 - 559.00 + 96 AT LBL 9 HAS SIGNS OF CORROSION (FILED CLOSED)REPLACED SEAT RAIL AT F.S. 559.00+80- F.S. 559.00 +96 AT LBL 9 IAW CRJ 200 AMM 53-01-11.
- [SDR SWI2024F00105](https://openairdocs.org/sdr/SWI2024F00105.md): Seat Track · corroded · Nov 28, 2023 · N464SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAIL FROM F.S. 559.00 + 80 - 559.00 + 96 AT RBL 27 HAS SIGNS OF CORROSION (FILED CLOSED)REMOVED AND REPLACED SEAT RAIL FROM F.S. 559.00+80- 559.00+96 AT RBL 27 IAW CRJ 200 AMM 53-01-11.
- [SDR SWI2024F00104](https://openairdocs.org/sdr/SWI2024F00104.md): Seat Track · corroded · Nov 28, 2023 · N464SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAIL FROM F.S. 559.00 + 80 - 559.00 + 96 AT RBL 9 HAS SIGNS OF CORROSION (FILED CLOSED)REMOVED AND REPLACED SEAT RAIL FROM F.S. 559.00+80 TO F.S. 559.00+96 AT RBL 9 IAW CRJ 200 AMM 53-01-11.
- [SDR SWI2024F00103](https://openairdocs.org/sdr/SWI2024F00103.md): Seat Track · corroded · Nov 28, 2023 · N464SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAIL FROM F.S. 559.00 + 112 - 621 AT LBL 27 HAS SIGNS OF CORROSION (FILED CLOSED)OK TO INSTALL MB910263REMOVED AND REPLACED SEAT RAIL FROM FS559.00+112 - FS621.00 AT LBL27 IAW CRJ200 AMM 53-00-49TOOL: AV-BX301 AUG2024
- [SDR SWI2024F00102](https://openairdocs.org/sdr/SWI2024F00102.md): Seat Track · corroded · Nov 28, 2023 · N464SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAIL FROM F.S. 559.00 + 112 - 621 AT LBL 9 HAS SIGNS OF CORROSION (FILED CLOSED)REMOVED AND INSTALLED SEAT TRACK RAIL FROM F.S. 559.00+112 - F.S.621 AT LBL 9 IAW AMM 53-00-49.CALIBRATED TOOLS USED: TORQUE DRIVER AV-BX301 DUE: AUGUST 2024
- [SDR SWI2024F00101](https://openairdocs.org/sdr/SWI2024F00101.md): Seat Track · corroded · Nov 28, 2023 · N464SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > SEAT RAIL FROM F.S. 559.00 + 112 - 621 AT RBL 27 HAS SIGNS OF CORROSION (FILED CLOSED)REMOVED AND REPLACED SEAT RAIL FROM F.S. 559.00+112 - F.S 621 AT RBL 27 IAW CRJ 200 AMM 53-00-49CALIBRATED TOOLS: TORQUE WRENCH DRIVER AV-BX301 DUE: AUGUST 2024
- [SDR SWIA2024020231128](https://openairdocs.org/sdr/SWIA2024020231128.md): Seat Track · corroded · Nov 28, 2023 · N464SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAIL FROM F.S. 559.00 + 96 - 559.00 + 112 AT LBL 27 HAS SIGNS OF CORROSION (FILED CLOSED)REMOVED AND REPLACED SEAT RAIL FROM FS. 559.00+96-559.00+112 AT LBL27 IAW CRJ200 AMM 53-00-49.
- [SDR SWIA202402021114](https://openairdocs.org/sdr/SWIA202402021114.md): Hinge Fitting · gouged · Nov 14, 2023 · N464SW · Cndair CL6002B19 · Ailerons
  > EVAL RIGHT AILERON #4 HINGE FITTING GOUGE ON IB SIDE (C-CHECK RO 2/1/2024) REPAIRED GOUGE ON R/H AILERON #4 HINGE FITTING ON I/B SIDE IAW MHIRJ REO# 601R-57-51-1037
- [SDR SWIA2024020231114](https://openairdocs.org/sdr/SWIA2024020231114.md): Gutter · cracked · Nov 14, 2023 · N464SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > EVAL PAX DOOR RAIN GUTTER CRACKED (C-CHECK RO 2/1/2024) REMOVED AND REPLACED PASSENGER DOOR RAIN GUTTER IAW CRJ 200 SRM 51-11-00, 51-42-06, 51-25-21
- [SDR SWIA2024020231106](https://openairdocs.org/sdr/SWIA2024020231106.md): Nut Plate · broken · Nov 6, 2023 · N464SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > PANEL #141 AL HAS SEIZED SCREW & BROKEN NUTPLATE (C-CHECK RO 2/1/2024) OK TO INSTALL KH 910266REMOVED AND REPLACED SCREW AND NUTPLATE ON PANEL 141 AL NUTPLATE IAW CRJ200 SRM 51-42-10, 51-45-00, AND CRJ 200 AMM 21-32-00.
- [SDR SWIA2024020231105](https://openairdocs.org/sdr/SWIA2024020231105.md): Panel · gouged · Nov 5, 2023 · N464SW · Cndair CL6002B19 · Fuselage Main, Structure
  > GOUGE AT LOWER AFT CORNER OF PNL 325AR APPROXIMATELY 3" LONG (C-CHECK RO 2/1/2024) PERFORMED REPAIR ON LOWER AFT CORNER OF PANEL 325AR IAW MHIRJ REO 601R-55-31-454. REV.
- [SDR SWIA202402021103](https://openairdocs.org/sdr/SWIA202402021103.md): Gutter · cracked · Nov 3, 2023 · N464SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > EVAL PAX DOOR RAIN GUTTER CRACKED (C-CHECK RO 2/1/2024) REMOVED AND REPLACED PASSENGER DOOR RAIN GUTTER IAW CRJ 200 SRM 51-42-06,51-25-21, AND 51-40-11. ALL WORK TRANSFERRED TO SKYWEST CP 27428099.
- [SDR SWIA202302021101](https://openairdocs.org/sdr/SWIA202302021101.md): Nut Plate · broken · Nov 1, 2023 · N464SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > NUTPLATE BROKEN AT FRONT CARGO DOOR STEP SCUFF PLATE IN TOP FORWARD SECTION OF FASTNERS (C-CHECK RO 2/1/2024) REMOVED AND REPLACED NUTPLATE AT FRONT CARGO DOOR STEP PLATE IN TOP FARWARD SECTION OF FASTENERS IAW CRJ 200 SRM 51-45-00
- [SDR SWIA20230601](https://openairdocs.org/sdr/SWIA20230601.md): Unknown · unknown · Jun 1, 2023 · N464SW · Cndair CL6002B19 · Landing Gear System
  > D:GEAR DISAGREE WARNING MESSAGE WHEN EXTENDING GEAR FOR LANDING, FLAPS 20* AND APPROXIMATELY 180 KTS. NOSE GEAR DOOR OPENED, BUT NOSE GEAR DID NOT EXTEND. FOLLOWED QRH, CYCLED GEAR 4 TIMES WITH NO RESULT, PULLING MANUAL GEAR EXTENSION HANDLE WAS SUCCESSFUL IN
- [SDR SWIA20230327001](https://openairdocs.org/sdr/SWIA20230327001.md): Unknown · dented · Mar 21, 2023 · N464SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > TRANSFER FROM EAML 1106677: DENT ON FUSELAGE SKIN BETWEEN FS736.00-FS755.00 & STGR15L-STGR18L. MAXIMUM DEPTH OF 0.229" ON TOP OF STRG 17L: MAX DEFORMATION OF 0.113" ON TOP OF STRG 16L: MAX DEFORMATION OF 0.135".PLEASE REFERENCE AML 1105320. DAMAGE IS OUT OF
- [SDR SWIA2022111466851](https://openairdocs.org/sdr/SWIA2022111466851.md): Selector Valve · failed · Nov 11, 2022 · N464SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR EXTENSION AT DESTINATION RECEIVED GEAR DISAGREE. RAN QRH, CYCLED GEAR SEVERAL TIMES IAW QRH DISAGREEMENT PERSISTED. HAD TO EXTEND GEAR WITH MANUAL GEAR EXTENSION. LANDING SUCCESSFUL. AA&E MX C/W GVI OF ALL LANDING GEAR, NO OBVIOUS DEFECTS NOTED. C/W MX
- [SDR SWIA202264071](https://openairdocs.org/sdr/SWIA202264071.md): None · malfunctioned · Jan 27, 2022 · N464SW · Cndair CL6002B19 · Landing Gear Door Actuator
  > AFTER TAKE OFF I SELECTED GEAR UP. GOT GEAR DISAGREE, MASTER WARNING, NOSE WHEEL STEERING CAUTION AND WOW CAUTION. / RAN QRH, GOT GEAR DOWN 3 GREEN AND RESET NW STEERING. LANDING UNEVENTFUL / (FLIGHT 6955 - FILED CLOSED) TROUBLESHOT CODES IN PSEU PER FIM 32-
- [SDR SWIA202156591](https://openairdocs.org/sdr/SWIA202156591.md): Windshield · cracked · Mar 4, 2021 · N464SW · Cndair CL6002B19 · Flight Compartment Windows
  > CLIMBING THROUGH 27000 FEET GOT A L WNDSHLD CAUTION MESSAGE AND CAPTAINS SIDE WINDSHIELD CRACKED. RAN QRH AND RETURNED TO TUS. FLIGHT 5992 - FILED CLOSED THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 22407183 WITH THE FOLLOWING CORRECTIVE ACTION: "RE
- [SDR SWIA202053101](https://openairdocs.org/sdr/SWIA202053101.md): Floorboard · damaged · Sep 17, 2020 · N464SW · Cndair CL6002B19 · Fuselage Floor Panel
  > REPAIR FLOORBOARD 251CLF, AS REQUIRED. C-CHECK RO 10/4/2020. REPAIRED FLOORBOARD 251CLF AS REQUIRED, PER REO ALL STEPS APPLIED. COMPLIED WITH.
- [SDR SWIA202053100](https://openairdocs.org/sdr/SWIA202053100.md): Retainer · dented · Sep 17, 2020 · N464SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR SEAL RETAINER DENTED IN MULTIPLE PLACES ALONG BOTTOM AFT EDGE. C-CHECK RO 10/4/2020. REMOVED AND REPLACED CARGO DOOR SEAL RETAINERS P/N CC670-38742-1 AND P/N CC670-38746-1 AT BOTTOM AFT EDGE, REF CRJ 200 SRM AND BOMBARDIER DWG. DETAILS SEE CONTIN
- [SDR SWIA202053099](https://openairdocs.org/sdr/SWIA202053099.md): Post · cracked · Sep 10, 2020 · N464SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 409.00+128 RBL 27 INTERIOR BULKHEAD POST POSSIBLE CRACK INNER BOTTOM AFT CORNER AREA, MARKED. C-CHECK RO 10/4/2020. REMOVED AND REPLACED THE FS 409+128 RBL 27 BULKHEAD POST, REF REO SRM AND DWG. COMPLIED WITH SKYWEST TASK CARD. ALL CHECKS GOOD.
- [SDR SWIA202053098](https://openairdocs.org/sdr/SWIA202053098.md): Post · cracked · Sep 10, 2020 · N464SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 409.00+128 LBL 18 INTERIOR BULKHEAD POST POSSIBLE CRACK OUTER BOTTOM AFT CORNER AREA, MARKED. C-CHECK RO 10/4/2020. PERFORMED NDT ON FS 409.00+128 LBL INTERIOR BULKHEAD POS, REF CRJ 200 AMM NDTM PART 6, 51-20-06. VERIFIED CRACK. REMOVED AND INSTALLED NE
- [SDR SWIA202053097](https://openairdocs.org/sdr/SWIA202053097.md): Hand Rail · damaged · Sep 10, 2020 · N464SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FWD HANDRAIL UPPER POST HAS LOOSE FASTENERS, MARKED. C-CHECK RO 10/4/2020. REPLACED CHERRYMAX RIVETS AT PAX DOOR FWD HANDRAIL UPPER POST, IAW REF CRJ200 SRM.
- [SDR SWIA202053096](https://openairdocs.org/sdr/SWIA202053096.md): Hinge · damaged · Sep 5, 2020 · N464SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX DOOR PIANO-HINGE (FUSELAGE) SIDE, APPEARS TO HAVE HEAVY WEAR AT EVERY LUG EXCEPT THE FWD MOST LUG. ALL LOOK ELONGATED AND THE HINGE PIN HAS PLAY, FLAGGED. C-CHECK RO 10/4/2020. REMOVED AND REPLACED PAX DOOR PIANO HINGE ON FUSELAGE SIDE, REF CRJ200SRM RE
- [SDR SWIA202053095](https://openairdocs.org/sdr/SWIA202053095.md): Floor Support · corroded · Sep 4, 2020 · N464SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT AT LBL 27 BETWEEN FS 569-607. C-CHECK RO 10/4/2020. INSTALLED NEW FLOOR BEAM SUPPORT ASSEMBLY LBL 27.0 FS 569.0-FS 607.0 INSTALLED, REF CRJ 200 SRM AND BOMBARDIER DWG.
- [SDR SWIA202053094](https://openairdocs.org/sdr/SWIA202053094.md): Floor Support · corroded · Sep 4, 2020 · N464SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT AT LBL 27 BETWEEN FS 559+112-569. C-CHECK RO 10/4/2020. REPAIRED FLOOR SUPPORT, PER MHI RJ REO. SEE CONTINUATION FOR DETAILS.
- [SDR SWIA202053093](https://openairdocs.org/sdr/SWIA202053093.md): Frame · corroded · Sep 2, 2020 · N464SW · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION ON FWD AND AFT SIDE OF FRAME BETWEEN STGR 25L-26R AT FS 319.00. C-CHECK RO 10/4/2020. REMOVED AND REPLACED FS 319 LOWER FRAME SECTOR, REF DWG AND CRJ200 SRM. SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH TASK.
- [SDR SWIA202053092](https://openairdocs.org/sdr/SWIA202053092.md): Cup · corroded · Sep 1, 2020 · N464SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FWD PAX DOOR AFT SIDE CUP ON DOOR SILL IS CORRODED. C-CHECK RO 10/4/2020. REMOVED AND REPLACED FWD PAX DOOR AFT SIDE CUP ON DOOR SILL, REF CRJ200 SRM. SEE CONTINUE CARD FOR DETAILS ON WORK PERFORMED.
- [SDR SWIA202053091](https://openairdocs.org/sdr/SWIA202053091.md): Cup · corroded · Sep 1, 2020 · N464SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FWD PAX DOOR FWD SIDE CUP ON DOOR SILL IS CORRODED. C-CHECK RO 10/4/2020. REMOVED AND REPLACED FWD PAX DOOR SIDE CUP ON FLOOR SILL, REF CRJ200 SRM. SEE CONTINUE CARD FOR DETAILS ON WORK PERFORMED.
- [SDR SWIA202053090](https://openairdocs.org/sdr/SWIA202053090.md): Doubler · cracked · Sep 1, 2020 · N464SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > REPAIR DOUBLER ON FS 280.00 FLOOR BEAM (AFT FACE) IS CRACKED AT APPROXIMATELY RBL 12. C-CHECK RO 10/4/2020. REPAIRED -4 REPAIR ANGLE ON FS 280.00 FLOOR BEAM AFT FACE AT APPROXIMATELY RBL 12, REF REO. SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH ATTACHED TA
- [SDR SWIA202053089](https://openairdocs.org/sdr/SWIA202053089.md): Doubler · cracked · Sep 1, 2020 · N464SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > REPAIR DOUBLER ON FS 280.00 FLOOR BEAM (AFT FACE) IS CRACKED AT APPROXIMATELY LBL 12. C-CHECK RO 10/4/2020. REPAIRED -1 REPAIR DOUBLER ON FS 280.00 FLOOR BEAM AFT FACE AT APPROXIMATELY LBL 12, REF REO. SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH ATTACHED
- [SDR SWIA202053088](https://openairdocs.org/sdr/SWIA202053088.md): Floorbeam · corroded · Sep 1, 2020 · N464SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOOR SUPPORT AT FS 280.00 BETWEEN LBL 9 AND RBL 9 IS CORRODED. C-CHECK RO 10/4/2020. REMOVED AND REPLACED FLOOR SUPPORT AT FS 280 BETWEEN LBL 9 AND RBL 9, REF CRJ200 SRM AND DWG. SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH TASK CARD.
- [SDR SWIA202053087](https://openairdocs.org/sdr/SWIA202053087.md): Floor Support · corroded · Sep 1, 2020 · N464SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON RT SIDE FLOOR SILL FWD OF FS 310.00. C-CHECK RO 10/4/2020. REPAIRED CORROSION DAMAGE ON RT SIDE FLOOR SILL AT STATED LOCATION, REF CRJ-200 SRM.
- [SDR SWIA202053086](https://openairdocs.org/sdr/SWIA202053086.md): Pressure Blkhd · corroded · Sep 1, 2020 · N464SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > 621 PRESS BULKHEAD FWD SIDE AT INTERSECTION OF PLANES FOR STGR 11L AND LBL 43. BLIND RIVET INSTALLED WITHOUT HOLE HAVING BEEN DRILLED THRU DOUBLER ON BACKSIDE, AS A RESULT, DOUBLER IS NOW BROKEN, CRACKED, AND DEFORMED. BOTH SIDES OF BULKHEAD HAVE BEEN MARKED
- [SDR SWIA202053085](https://openairdocs.org/sdr/SWIA202053085.md): Skin · corroded · Sep 1, 2020 · N464SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > BELLY SKIN FS 559+96 BETWEEN STGRS 23R/24R AS VIEWED FROM OUTSIDE AND BELOW WASTE DRAIN VALVE ASSEMBLY RIVETS/SKIN CORRODED, AS MARKED. C-CHECK RO 10/4/2020. REPAIRED BELLY SKIN FS 559+96 BETWEEN STGRS 23R/24R AS VIEWED FROM OUTSIDE AND BELOW WASTE DRAIN VAL
- [SDR SWIA202053084](https://openairdocs.org/sdr/SWIA202053084.md): Skin · corroded · Sep 1, 2020 · N464SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > BELLY SKIN BETWEEN FS 559+80/559+112 AND STGRS 25L/26R SKIN/RIVETS CORRODED, AS MARKED. VISIBLE FROM OUTSIDE/BOTTOM. C-CHECK RO 10/4/2020. REPAIRED BELLY SKIN BETWEEN FS 559+80/559+112 AND STGRS 25L/26R SKIN/RIVETS CORROSION, REF REO. LEAK CHECK GOOD.
- [SDR SWIA202053083](https://openairdocs.org/sdr/SWIA202053083.md): Frame · corroded · Aug 31, 2020 · N464SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 605-STGR 25L/25R FRAME CORRODED. C-CHECK RO 10/4/2020. REMOVED CORROSION AT FS 605 STGR 25L TO 25R, REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS. PERFORMED FRAME REPAIR AT FS 605 BETWEEN STGR 26R TO 27R, REF CRJ200 SRM AND DWG. COMPLIED WITH TASK CARD.

Next page: https://openairdocs.org/aircraft/N464SW/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 = 'N464SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N464SW/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.