# Service difficulty reports: N466SW

A list on [N466SW](https://openairdocs.org/aircraft/N466SW.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 · 153 reports

- [SDR SWIA2026040976354](https://openairdocs.org/sdr/SWIA2026040976354.md): Fitting · gouged · Apr 9, 2026 · N466SW · Cndair CL6002B19 · Wing, Attach Fittings
  > LEFT WING REAR SPAR AT WS162.49 HAS A FITTING GOUGED & DAMAGED. REMOVED, REPLACED, AND INSTALLED FITTING ON LT WING REAR SPAR AT WS 162.49 IAW SRM 57-51-14,51-40-11,51-21-11,51-25-06,51-25-16,51-42-06, & 51-42-20,51-23-00.
- [SDR SWI2025F00644](https://openairdocs.org/sdr/SWI2025F00644.md): Bracket · loose · May 16, 2025 · N466SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > AFTER SELECTING GEAR LEVER UP, GEAR DISAGREE MESSAGE CAME ON AND RAN QRH BUT MESSAGE PERSISTS AND RETURNED TO IAH TO LAND. (FLIGHT 5297 - FILED CLOSED)PLEASE REFERENCE AML 1606345 FOR FDR DOWNLOAD. PER FDR ANALYSIS. RH MLG NEVER REGISTERED IN THE UPLOCK POSITI
- [SDR SWI2025F00066](https://openairdocs.org/sdr/SWI2025F00066.md): Electrical Sys · power loss · Jan 10, 2025 · N466SW · Cndair CL6002B19 · Alternator-Generator Drive
  > COMPLETE LOSS OF AC POWER IN FLIGHT. ADG DEPLOYED AUTOMATICALLY. POWER LOSS OCCURRED WHILE SELECTING FLAPS 8. RAN QRC/QRH AND RESTORED ALL AC POWER. NORMAL LANDING AND TAXI IN. (FLIGHT 5333) REFERENCE AML 1512638, AML 1512639, AML 1512641, AML 1512642, AML
- [SDR SWIA202501130](https://openairdocs.org/sdr/SWIA202501130.md): Electrical Sys · power loss · Jan 10, 2025 · N466SW · Cndair CL6002B19 · DC Power Distribution System
  > COMPLETE LOSS OF AC POWER IN FLIGHT. ADG DEPLOYED AUTOMATICALLY. POWER LOSS OCCURRED WHILE SELECTING FLAPS 8. RAN QRC/QRH AND RESTORED ALL AC POWER. NORMAL LANDING AND TAXI IN. (FLIGHT 5333 - FILED CLOSED) PLEASE REFERENCE AML 1512638 PLEASE REFERENCE
- [SDR SWIA202501105](https://openairdocs.org/sdr/SWIA202501105.md): Electrical Sys · power loss · Jan 10, 2025 · N466SW · Cndair CL6002B19 · Electrical Power System
  > COMPLETE LOSS OF AC POWER IN FLIGHT. ADG DEPLOYED AUTOMATICALLY. POWER LOSS OCCURRED WHILE SELECTING FLAPS 8. RAN QRC/QRH AND RESTORED ALL AC POWER. NORMAL LANDING AND TAXI IN. (FLIGHT 5333 - FILED OPEN)
- [SDR SWIA2024091900006](https://openairdocs.org/sdr/SWIA2024091900006.md): Frame · cracked · Sep 6, 2024 · N466SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FOUND 2 CRACKS AND SKIN OIL CANNING ON CENTER FRAME SECTOR P/N 600-34014-277 LOCATED OFF FS235.00 AND BETWEEN STGR-26L AND STGR-26R AFT OF NLG. THIS HAS BEEN CLASSIFED AS A MAJOT REPAIR. FORM M-337 INITIATED. (FILED CLOSED) PERFORMED SHORING OF THE AIRCR
- [SDR SWIA2024090900800](https://openairdocs.org/sdr/SWIA2024090900800.md): Skin · cracked · Sep 6, 2024 · N466SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FOUND 2 CRACKS AND SKIN OIL CANNING ON CENTER FRAME SECTOR P/N 600-34014-277 LOCATED OFF FS235.00 AND BETWEEN STGR-26L AND STGR-26R AFT OF NLG. THIS HAS BEEN CLASSIFED AS A MAJOT REPAIR. FORM M-337 INITIATED. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROG
- [SDR SWIA202405200017](https://openairdocs.org/sdr/SWIA202405200017.md): Skin · dented · May 17, 2024 · N466SW · Cndair CL6002B19 · Passenger/Crew Doors
  > COMPLY WITH REPAIR FOR TEMPORARYREO 601R-52-11-3014 (DENTS TO PASSENGER DOOR OUTER SKIN BETEEN FS338.963-FS347.250 ABOVE DATUM LINE #1). (FILED CLOSED)COMPLIED WITH PERMANENT REPAIR ON PAX DOOR OUTER SKIN. PER REO 601R-52-11-3015 PRELIMINARY P1 REV -(P1) DAT
- [SDR SWIA2024052000014](https://openairdocs.org/sdr/SWIA2024052000014.md): Door · dented · May 14, 2024 · N466SW · Cndair CL6002B19 · Passenger/Crew Doors
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA90491-REO 601R-52-11-3014 MXCODEID74202-PR - MAIN CABIN DOOR HIT THE RAMP. COMPLIED WITH TEMPORARY REPAIR PER REO 601R-52-11-3014. FINAL REPAIR DUE WITHIN 100FH REF REO 601R-52-11-3014., PART NUMBER: -, SERIAL NUMB
- [SDR SWIA20230410](https://openairdocs.org/sdr/SWIA20230410.md): Unknown · cracked · Apr 10, 2023 · N466SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CRACK IN FORWARD PRESSURE BULKHEAD AT PARKING BRAKE ROD THROUGH HOLE. THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR, FORM M-337 WILL BE REQUIRED. (FILED CLOSED) APPLIED REPAIR DOUBLER TO FORWARD PRESSURE BULKHEAD AT PARKING BRAKE ROD THROUGH HOLE IN REF. TO
- [SDR SWIA2023041100001](https://openairdocs.org/sdr/SWIA2023041100001.md): Unknown · cracked · Apr 10, 2023 · N466SW · Cndair CL6002B19 · Fuselage Structure (General)
  > CRACK IN FORWARD PRESSURE BULKHEAD AT PARKING BRAKE ROD THROUGH HOLE. THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR, FORM M-337 WILL BE REQUIRED. (FILED OPEN)
- [SDR SWIA2023020007](https://openairdocs.org/sdr/SWIA2023020007.md): None · cracked · Feb 7, 2023 · N466SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING AUDIT OF TRU BAY SUSPECTED CRACK REPAIR FOUND REPAIR ANGLE -3 AND REPAIR DOUBLER -2 FABRICATED USING WRONG MATERIALS PER REO 601R-53-11-111 (C-CHECK RO 2/26/2023) UPON FURTHER INVESTIGATION FOUND -3 ANGLE WAS FABRICATED USING CORRECT MATERIAL AN
- [SDR SWIA202301026](https://openairdocs.org/sdr/SWIA202301026.md): None · corroded · Jan 26, 2023 · N466SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > LEFT FLOOR SILL FS349.00 - 364.00 HAS AN AREA OF CORROSION. (MARKED) (C-CHECK RO 2/26/2023) REPAIRED LH FLOOR SILL AT FS 349.00 -364.00 REF REO 601R-53-21-3601 REV -- DATE 2023-02-08. ALL STEPS OF REO COMPLIED WITH, SEE CONTINUE CARD FOR DETAILS. M337
- [SDR SWIA2023010026](https://openairdocs.org/sdr/SWIA2023010026.md): None · corroded · Jan 26, 2023 · N466SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > SEAT TRACK FS379.00 - 400.00 RBL9 HAS CORROSION. (C-CHECK RO 2/26/2023) REPLACED NEW SEAT TRACK AT RBL9 BETWEEN FS364.00 - FS409.00 REF CRJ200 AMM 53-01-11
- [SDR SWIA20230100126](https://openairdocs.org/sdr/SWIA20230100126.md): None · corroded · Jan 26, 2023 · N466SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > RIGHT HAND PRESSURE FLOOR SEAT RAIL BETWEEN FS409.0+128 TO FS559.0, CORRODED AND GOUGED IN SEVERAL PLACES OF THE RAIL SECTION. (C-CHECK RO 2/26/2023) INSTALLED NEW SEAT RAIL BETWEEN FS 409.00 +128 AND FS 559.00 +5 PER FCRJ 200 AMM 53-01-11-400-802 AND
- [SDR SWIA20230124](https://openairdocs.org/sdr/SWIA20230124.md): None · corroded · Jan 24, 2023 · N466SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > L/H FLOOR SILL SHOWS EVIDENCE OF CORROSION IN MULTIPLE AREAS (MARKED) (C-CHECK RO 2/26/2023) CORROSION BLENDED OUT IN MARKED AREAS AND FOUND WITHIN LIMITS PER REO 601R-53-41-666 REV. -C, DATED 2012-11-06. 2EA FASTENERS WERE REPLACED WITH ALTERNATES AT
- [SDR SWIA202301023](https://openairdocs.org/sdr/SWIA202301023.md): None · damaged · Jan 23, 2023 · N466SW · Cndair CL6002B19 · Fuselage, Wing Attach Fittings
  > FRETTING ON WING PLANK AT ACCESS HOLE PANEL LANDING FOR FUEL PANEL 510AB (C-CHECK RO 2/26/2023) BLENDED WITHIN LIMITS, WING PLANK LANDING FOR 510AB PANEL REF REO 601R -57-21-030 REV L DATED 2014-02-05ORIGINAL MATERIAL 0.182", REMAINING 0.179", REMOVED
- [SDR SWIA20230118](https://openairdocs.org/sdr/SWIA20230118.md): None · cracked · Jan 18, 2023 · N466SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > NLG WHEEL WELL CUTOUT - EXTERNAL SKIN - AFT L/H CORNER HAS SUSPECTED CRACK - FS 235 LBL 6 (C-CHECK RO 2/26/2023) COMPLIED WITH THE REPAIR FOR AFT L/H CORNER OF NLG WHEEL WELL CUTOUT. REF REO 601R-53-11-048 REV-D DATED 2015-06-10 AND REO 601R-53-11-3824
- [SDR SWIA2023010018](https://openairdocs.org/sdr/SWIA2023010018.md): None · cracked · Jan 18, 2023 · N466SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > RH FWD DRAIN HOLE AFT ATTACH HOLE CRACKED AT 2 O'CLOCK POSITION AND RH AFT DRAIN HOLE BY BOOST PUMP AFT ATTACH HOLE CRACKED AT 9 O'CLOCK (C-CHECK RO 2/26/2023): REPAIRED R/H FWD DRAIN HOLE AFT ATTACH HOLE BY OPENING UP THE DAMAGED HOLE AND REAMING PER
- [SDR SWIA2023010017](https://openairdocs.org/sdr/SWIA2023010017.md): None · cracked · Jan 17, 2023 · N466SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > AFT EQUIPMENT BAY - CLEAT SECURING INTERCOSTAL AT STGR 14L TO FRAME @ FS 625 CRACKED (C-CHECK RO 2/26/2023) REMOVED AND INSTALLED NEW AFT EQUIPMENT BAY - CLEAT/ INTERCOSTAL P/N 601-35012-52 AT STGR 14L TO FRAME @ FS 625 REF CRJ200 SRM 51-42-21 AND DWG 6
- [SDR SWIA2023010016](https://openairdocs.org/sdr/SWIA2023010016.md): None · corroded · Jan 16, 2023 · N466SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > CABIN - L/H FLOOR SILL, JUST AFT OF FRAME @ FS 439, SHOWS EVIDENCE OF CORROSION AROUND NUTPLATE HOLE (C-CHECK RO 2/26/2023) REMOVED CORROSION FROM LH PRESSURE FLOOR SILL JUST AFT OF FRAME @ FS 439 REF REO 601R-53-41-666, REV -C, DATED: 2012-11-06, 1.2 D
- [SDR SWIA20230113](https://openairdocs.org/sdr/SWIA20230113.md): None · gouged · Jan 13, 2023 · N466SW · Cndair CL6002B19 · Wing Structure
  > LEFT AILERON - UPPER LEADING EDGE SKIN INNER SURFACE BETWEEN THE PCU ATTACHING LUGS IS GOUGED. (MARKED) (C-CHECK RO 2/26/2023) LH UPPER AILERON LEADING EDGE SKIN OUT OF LIMITS, REPLACED WITH NEW AILERON UPPER LEADING EDGE SKIN REF. CRJ200 SRM 51-42-06 A
- [SDR SWIA2023010012](https://openairdocs.org/sdr/SWIA2023010012.md): None · corroded · Jan 12, 2023 · N466SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > INTERCOSTAL AT DD3 CENTER HAS CORROSION AROUND LIGHTNING HOLE. (C-CHECK RO 2/26/2023) REPLACED WITH NEW SERVICEABLE DD3 INTERCOSTAL (P/N 601R31056-1S) ONTO PAX DOOR USING ALL NEW FASTENERS. REF BOMBARDIER DWG# 601R31702 REV N AND CRJ200 SRM 51-42-06 RE
- [SDR SWIA2023011001](https://openairdocs.org/sdr/SWIA2023011001.md): None · chafed · Jan 11, 2023 · N466SW · Cndair CL6002B19 · Aerodynamic Fairings
  > *RH LOWER WING PLANK AT FS513.00 WS45.0 HAS CHAFFE DAMAGED FROM THE BODY FAIRING (MARKED) (C-CHECK RO 2/26/2023) BLENDED WITHIN LIMITS ZONE A (**), ORIGINAL MATERIAL THICKNESS 0.300", REMAINING 0.296", MATERIAL REMOVED 0.004"REF REO 601R-57-21-3692, R
- [SDR SWIA202301000011](https://openairdocs.org/sdr/SWIA202301000011.md): None · corroded · Jan 11, 2023 · N466SW · Cndair CL6002B19 · Passenger/Crew Doors
  > *PAX DOOR AFT OUTER FORMER CORRODED UNDER PANEL 832GR (MARKED) (C-CHECK RO 2/26/2023) REPLACED PAX DOOR AFT FORMER REF CRJ 200 SRM 51-42-06 AND DRAWING 601R31702 REV N. M337 AND SKYWEST TASK CARD 51-900-1003-SKY COMPLIED WITH. SEE CONTINUE CARD FOR DETA
- [SDR SWIA20230100005](https://openairdocs.org/sdr/SWIA20230100005.md): None · damaged · Jan 5, 2023 · N466SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD FORWARD FACE - SIX OF THE PICKET FENCE REPAIR PLATES HAVE DAMAGE FROM LINER SCREWS WL103.00. (MARKED) (C-CHECK RO 2/26/2023) COMPLIED WITH REO 601R-53-61-7951 REV-- DATED 2023-01-22 FOR REAR PRESSURE BULKHEAD FORWARD FACE REPAIR M
- [SDR SWIA20230100003](https://openairdocs.org/sdr/SWIA20230100003.md): None · cracked · Jan 3, 2023 · N466SW · Cndair CL6002B19 · Doors
  > SUSPECTED CRACK ON THE LH TRU BAY AT APPROX. FS.202 ON CORNER RADIUS (MARKED) (C-CHECK RO 2/26/2023) COMPLIED WITH REPAIR FOR CRACKED L/H TRU BAY REF CRJ 200 SRM 51-42-06 REV 39, DATED: MAR 10/21 AND REO 601R-53-11-111 REV NC DATE 98-MAR-18, COMPLIED WI
- [SDR SWIA202266604](https://openairdocs.org/sdr/SWIA202266604.md): None · cracked · Oct 3, 2022 · N466SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > FS280 BEAM, FWD FLOOR SUPPORT ANGLE BETWEEN LBL9 & RBL9, CRACKS IN RADIUS ON BOTH ENDS. (FILED CLOSED) REMOVED AND REPLACED FWD FLOOR SUPPORT ANGLE BETWEEN LBL9 AND RBL9 IN REFERENCE TO SRM 51-42-06.
- [SDR SWIA202266603](https://openairdocs.org/sdr/SWIA202266603.md): None · cracked · Oct 3, 2022 · N466SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > FS280 BEAM, AFT FLOOR SUPPORT ANGLE REPAIR SPLICE, OB OF RBL9, CRACK IN RADIUS ON IB END. (FILED CLOSED) FABRICATED REPAIR SPLICE PER SRM 53-21-43. REMOVED AND REPLACED FS280 BEAM, AFT FLOOR SUPPORT ANGLE REPAIR SPLICE, OB OF RBL9 IAW SRM 51-42-21
- [SDR SWIA202266602](https://openairdocs.org/sdr/SWIA202266602.md): None · cracked · Oct 3, 2022 · N466SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > FS280 BEAM/FLOOR SUPPORT BEAM CLIP, OB, RBL9, IS CRACKED IN RADIUS, UPPER END. (FILED CLOSED) FABRICATED BEAM CLIP PER SRM 53-21-43. REMOVED AND REPLACED FS280 BEAM/FLOOR SUPPORT BEAM CLIP, OB, RBL9, IAW SRM 51-42-21
- [SDR SWIA202266601](https://openairdocs.org/sdr/SWIA202266601.md): None · cracked · Oct 3, 2022 · N466SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > FS280 BEAM/FLOOR SUPPORT BEAM CLIP, IB, RBL9, IS CRACKED IN RADIUS, UPPER END. (FILED CLOSED) FABRICATED BEAM CLIP PER SRM 53-21-43. REMOVED AND REPLACED FS280 BEAM/FLOOR SUPPORT BEAM CLIP, IB, RBL9, IAW SRM 51-42-21
- [SDR SWIA202265646](https://openairdocs.org/sdr/SWIA202265646.md): None · damaged · May 9, 2022 · N466SW · Cndair CL6002B19 · Window/Windshield System
  > RH OVERWING EMERGENCY EXIT WINDOW SCRATCHED BEYOND LIMITS. (FILED - CLOSED) REMOVED & REPLACED RH OVERWING EMERGENCY EXIT WINDOW IN REFERENCE TO APPLICABLE STEPS IN AMM 56-21-01. REMOVED WINDOW MFG DATE: 08-02
- [SDR SWIA2020071451326](https://openairdocs.org/sdr/SWIA2020071451326.md): Actuator · failed · Jul 14, 2020 · N466SW · Cndair CL6002B19 · Landing Gear Actuator
  > GEAR DISAGREE ON LANDING WHEN SELECTED. COMPLIED WITH QRH AND MESSAGE CLEARED. INDICATION WAS RIGHT MAIN LANDING GEAR. FLIGHT 5253 - FILED CLOSED. REFERENCE CP 21230240 FOR INSPECTION OF THE RT MLG UPLOCK ASSEMBLY. REFERENCE CP 2123043 FOR INSPECTION OF T
- [SDR SWIA2020020648244](https://openairdocs.org/sdr/SWIA2020020648244.md): Frame · cracked · Jan 9, 2020 · N466SW · Cndair CL6002B19 · Fuselage Main, Frame
  > * FRAME AT FS 333.0 STR 2L IS CRACKED (C-CHECK) RO 2/04/2020 REPAIRED FRAME AT FS 333.0 STR 2L REF BOMBARDIER DWG, CRJ200 SRM AND CRJ200 SRM. LEAK CHECK GOOD
- [SDR SWIA2020020648243](https://openairdocs.org/sdr/SWIA2020020648243.md): Frame · corroded · Jan 8, 2020 · N466SW · Cndair CL6002B19 · Fuselage Main, Frame
  > F.S. 333 FRAME HAS CORROSION ON FWD> AND AFT SIDE AS MARKED IN RED IN AVIONICS BELLY AREA (C-CHECK) RO 2/04/2020 REPAIRED F.S. 333 FRAME REF CRJ200 SRM, CRJ200 SRM, AND BOMBARDIER DWG. LEAK CHECK GOOD
- [SDR SWIA2020020648242](https://openairdocs.org/sdr/SWIA2020020648242.md): Mount · corroded · Jan 8, 2020 · N466SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > GALLEY INBD. AFT FLOOR MOUNT AT APROX. RBL 9 EXFOLIATED (C-CHECK) RO 2/04/2020 REMOVED AND REPLACED GALLEY INBD. AFT FLOOR MOUNT AT APROX. RBL 9 REF BOMBARDIER DWG AND CRJ200 SRM. SEE CONTINUE CARD FOR DETAILS. SEE ATTACHED TASK.
- [SDR SWIA2020020648241](https://openairdocs.org/sdr/SWIA2020020648241.md): Floorbeam · cracked · Jan 8, 2020 · N466SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > 280 BEAM LBL 9 CRACKED CLIP AT UPPER ANGLE (C-CHECK) RO 2/04/2020 REMOVED AND REPLACED FS280, LBL9 CLIP REF CRJ200 SRM. AND USED BOMBARDIER REO FOR MATERIAL ID AND FASTENER CALL OUT ONLY. SEE CONTINUE CARD FOR DETAILS. SEE ATTACHED TASK.
- [SDR SWIA2020020648240](https://openairdocs.org/sdr/SWIA2020020648240.md): Floor Support · corroded · Jan 7, 2020 · N466SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * RIGHT PRESSURE FLOOR SILL PANEL FROM FS 409+128 O FS 559.0 HAS SEVERAL AREAS OF CORROSION (C-CHECK) RO 2/04/2020 REPAIRED RIGHT PRESSURE FLOOR SILL CORROSION L FROM FS 409+128 TO FS 559.0 REF REO. LEAK CHECK GOOD.
- [SDR SWIA2020020648239](https://openairdocs.org/sdr/SWIA2020020648239.md): Floor Support · corroded · Jan 7, 2020 · N466SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * LEFT PRESSURE FLOOR SILL PANEL FROM FS 409+128 O FS 559.0 HAS SEVERAL AREAS OF CORROSION (C-CHECK) RO 2/04/2020 REPAIRED LEFT PRESSURE FLOOR SILL PANEL FROM FS 409+128 O FS 559.0 REF REO. LEAK CHECK GOOD
- [SDR SWIA2020020648238](https://openairdocs.org/sdr/SWIA2020020648238.md): Frame · corroded · Jan 7, 2020 · N466SW · Cndair CL6002B19 · Fuselage Main, Frame
  > * FRAME AT FS 574.0 FWD SIDE HAS CORROSION IN THE AREA OF STR 26L TO 26R (C-CHECK) RO 2/04/2020 REPAIRED FRAME AT FS574 BETWEEN STR26L AND STR26R PER REO.
- [SDR SWIA2020020648237](https://openairdocs.org/sdr/SWIA2020020648237.md): Frame · corroded · Jan 7, 2020 · N466SW · Cndair CL6002B19 · Fuselage Main, Frame
  > * FRAME AT FS 589.0 FWD SIDE HAS CORROSION IN THE AREA OF STR 26L TO 26R (C-CHECK) RO 2/04/2020 REPAIRED FRAME AT FS589 BETWEEN STR26L AND STR25R PER REO.
- [SDR SWIA2020020648236](https://openairdocs.org/sdr/SWIA2020020648236.md): Post · damaged · Jan 7, 2020 · N466SW · Cndair CL6002B19 · Fuselage Main, Structure
  > F.S 409+128 BL 0.0 DEFECTS NOTED AT LH / RH AFT RADIUS OF VERTICAL POSTS. (C-CHECK) RO 2/04/2020 REPLACED LH/RH VERTICAL POSTS AND 2EA CLIPS @ FS409.00 + 128 BL0.0. REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-22, BOMBARDIER DWG 601R32208 REV-T, AND BOMBARDIE
- [SDR SWIA2020020648235](https://openairdocs.org/sdr/SWIA2020020648235.md): Frame · corroded · Jan 7, 2020 · N466SW · Cndair CL6002B19 · Fuselage Main, Frame
  > * FRAME AT FS 605.0 FWD SIDE HAS CORROSION IN THE AREA OF STR 26L TO 26R (C-CHECK) RO 2/04/2020 REPAIRED FRAME AT FS605 BETWEEN STR26L AND STR26R PER REO.
- [SDR SWIA2020020648234](https://openairdocs.org/sdr/SWIA2020020648234.md): Shim · migrated · Jan 7, 2020 · N466SW · Cndair CL6002B19 · Elevator Structure
  > SIX LOOSE BOLTS ( 3 OTBD R/H & 3 OTBD L/H) AND MIGRATED SHIMS FOUND ON THE HORIZONTAL STABILIZER STEADY FITTING. (C-CHECK) RO 2/04/2020 REPAIRED HORIZONTAL STEADY FITTING, REAMED HOLES AND INSTALLED NEW FASTENERS REF CRJ 200 REO. OPS AND GAP CHECKS GOO
- [SDR SWIA2020020648250](https://openairdocs.org/sdr/SWIA2020020648250.md): Doubler · corroded · Jan 6, 2020 · N466SW · Cndair CL6002B19 · Fuselage Main, Structure
  > *DOUBLER ON PASSENGER DOOR FRAME, FS349.00 STGR18L, IS CORRODED. (MARKED) (C-CHECK) RO 2/04/2020 REMOVED AND BLENDED OUT CORROSION IS WITHIN LIMITS AT PAX DOOR FRAME DOUBLER, FS349.00 STGR18L. REF. CRJ 200 SRM, SRM(SEE DETAILS FOR CORRECTIVE ACTION)
- [SDR SWIA2020020648233](https://openairdocs.org/sdr/SWIA2020020648233.md): Door Sill · gouged · Jan 6, 2020 · N466SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *PASSENGER DOOR UPPER SILL GOUGED, 4 PLACES, UNDER THE CEILING PANEL ATTACH POINTS FS310.00 Ï¿½ FS349.00. (C-CHECK) RO 2/04/2020 BLENDED OUT GOUGE DAMAGE TO PAX DOOR UPPER SILL DOUBLER AT STR3L BETWEEN FS310.00 - FS349.00 IS STRUCTURALLY ACCEPTABLE. COMPLI
- [SDR SWIA2020020648232](https://openairdocs.org/sdr/SWIA2020020648232.md): Door Sill · corroded · Jan 6, 2020 · N466SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *PASSENGER DOOR SILL ANGLE HAS CORROSION AT MULTIPLE AREAS AND EXFOLIATION THRU THE ANGLE AT THE DOOR CLOSED SENSOR. (MARKED) (C-CHECK) RO 2/04/2020 PAX DOOR SILL ANGLE IS OUT OF LIMITS PER REF CRJ 200 SRM, REMOVED AND REPLACED PAX DOOR SILL ANGLE WITH NEW
- [SDR SWIA2020020648249](https://openairdocs.org/sdr/SWIA2020020648249.md): Anchor Fitting · corroded · Jan 3, 2020 · N466SW · Cndair CL6002B19 · Passenger/Crew Doors
  > * AFT PASS DOOR ANCHOR FITTING HARDWARE RUSTED AND CORRODED MARKED (C-CHECK) RO 2/04/2020 REPLACED PASSENGER DOOR AFT COUNTERBALANCE ANCHOR FITTING. REF CRJ200 AMM TASK.
- [SDR SWIA2020020648248](https://openairdocs.org/sdr/SWIA2020020648248.md): Plate · corroded · Jan 3, 2020 · N466SW · Cndair CL6002B19 · Passenger/Crew Doors
  > * AFT SERRATED PLATE CORRODED MARKED (C-CHECK) RO 2/04/2020 REPLACED WITH NEW PAX DOOR AFT COUNTERBALANCE ANCHOR FITTING SERRATED PLATE REF CRJ 200 AMM.
- [SDR SWIA2020020648231](https://openairdocs.org/sdr/SWIA2020020648231.md): Skin · gouged · Jan 3, 2020 · N466SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > * APU EXHAUST CUTOUT EXTERIOR SKIN Ï¿½ GOUGES AND EDGE DAMAGE ON AFT SIDE OF CUTOUT (MARKED). (C-CHECK) RO 2/04/2020 REMOVED DAMAGE ON APU EXHUAST CUTOUT EXTERIOR SKIN, REF CRJ 200 SRM. SKIN IS WITHIN LIMITS PER BOMBARDIER REO. SEE CONTINUATION CARD FOR DE

Next page: https://openairdocs.org/aircraft/N466SW/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 = 'N466SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N466SW/reports

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