# Service difficulty reports: N973SW

A list on [N973SW](https://openairdocs.org/aircraft/N973SW.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 SWIA2026072576673](https://openairdocs.org/sdr/SWIA2026072576673.md): Sensing Element · out of position · Jul 25, 2026 · N973SW · Cndair CL6002B19 · Pneumatic Indicating System
  > ANTI-ICE DUCT MASTER WARNING MSG ENROUTE. FOLLOWED QRH. (FLIGHT 4709) ON ARRIVAL PERFORMED OPS CHK OF WING ANTI-ICE REF AMM 30-12-00. OPS CHKD GOOD. COULD NOT DUPLICATE FAULT ON GRND. TROUBLESHOT ANTI-ICE DUCT WARNING MSG REF FIM 36-20-00, FOLLOWING SECTION W
- [SDR SWIA2026050475992](https://openairdocs.org/sdr/SWIA2026050475992.md): Floorbeam · damaged · May 4, 2026 · N973SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > OUTBOARD FLOORBEAM REF SRM 53-51-43 ITEM 24 PN 601R31117-35. AT RBL 9, BS 559+64 - 559+80 HAS ELONGATED HOLE IN FLANGE JOINING CROSS MEMBER. COMPLIED WITH REO 601R-53-51-741 DATED: 2026-05-28 REV- STEPS: 3A, 3B AND 3C BY INSTALLING A FREEZE PLUG FOR THE ELO
- [SDR SWIA2026041676203](https://openairdocs.org/sdr/SWIA2026041676203.md): Floorbeam · corroded · Apr 16, 2026 · N973SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORRODED NUTPLATE ON FLOOR BOARD LANDING JUST AFT OF FS 559.00+80 ON RBL 9. REMOVED AND REPLACED UPPER FLOOR BEAM (FLOORBOARD LANDING/SEAT TRACK MOUNT), SPLICE CHANNELS, SUPPORTS & REMOVED AND REINSTALLED 4 INTEGRATED CROSSBEAM WEBS, INTERCOSTAL CLIPS/BRACKET
- [SDR SWIA2026041076211](https://openairdocs.org/sdr/SWIA2026041076211.md): Floorbeam · damaged · Apr 10, 2026 · N973SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOOR BOARD LANDING IS DAMAGED AT FS559+48 ON RBL27.5 OUTBOARD SIDE. (C-CHECK RO 06/04/2026)REPAIRED DAMAGED FLOOR BOARD LANDING AT FS559+48 ON RBL27.5 OUTBOARD SIDE IN REFERENCE TO SRM 53-00-43. PERFORMED EDDY CURRENT INSPECTION IN REFERENCE TO NDTM PART 1 5
- [SDR SWIA2026040976208](https://openairdocs.org/sdr/SWIA2026040976208.md): Floorbeam · torn · Apr 9, 2026 · N973SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RH CABIN SILL @ FS589.00 HAS TORN NUTPLATE HOLE FOR FLOORBOARD. REPAIRED TORN NUTPLATE HOLE IN RH CABIN SILL AT FS589.00 IN REFERENCE TO REO 601R-53-61-8519 REV-- 2026-04-22. PERFORMED EDDY CURRENT INSPECTION IN REFERENCE TO NDTM PART 1 51-20-06 AND PART 6 5
- [SDR SWIA2026040676207](https://openairdocs.org/sdr/SWIA2026040676207.md): Intercostal · cracked · Apr 6, 2026 · N973SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT SIDE OF PRESSURE BULKHEAD FS 621 INTERCOSTAL INLINE WITH STRINGER 14L IS CRACKED. REMOVED AND REPLACED INTERCOSTAL ON AFT SIDE OF PRESSURE BULKHEAD FS621.00 INLINE WITH STRINGER 14L WITH REFERENCE TO SRM 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026040676206](https://openairdocs.org/sdr/SWIA2026040676206.md): Intercostal · cracked · Apr 6, 2026 · N973SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT SIDE OF PRESSURE BULKHEAD BS 621 INTERCOSTAL INLINE WITH STRINGER 14R IS CRACKED. REMOVED AND REPLACED THE AFT SIDE OF PRESSURE BULKHEAD BS 621 INTERCOSTAL INLINE WITH STRINGER 14R IAW SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026040376210](https://openairdocs.org/sdr/SWIA2026040376210.md): Skin · dented · Apr 3, 2026 · N973SW · Cndair CL6002B19 · Rudder, Plate/Skin
  > FOUND DENT ON RT SIDE OF RUDDER ASSY APPROX. 1.5" FROM RS 78.82 AND 5.2" FROM THE TRAILING EDGE. COMPLIED WITH REO 601R-55-41-315 REV--. REPAIR FOR DENT TO RUDDER RHS SKIN BETWEEN RS78.818 - RS85.070. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026040376202](https://openairdocs.org/sdr/SWIA2026040376202.md): Floor Support · corroded · Apr 3, 2026 · N973SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND MULTIPLE SPOTS OF SURFACE CORROSION ON RT PRESSURE FLOOR SILL FROM FS 409.00+128 AND FS 559.00 FROM RBL 36.00 TO RBL 45.00. BLENDED CORROSION ON THE RT PRESSURE FLOOR SILL ASSY APPROX RBL 36.00 - RBL 45.00 AND BETWEEN FS409.00 +128 AND FS559.00 IAW SRM
- [SDR SWIA2026060876201](https://openairdocs.org/sdr/SWIA2026060876201.md): Floor Support · corroded · Apr 3, 2026 · N973SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND MULTIPLE SPOTS OF SURFACE CORROSION ON LH PRESSURE FLOOR SILL FROM FS 409.00+128 AND FS 559.00 FROM LBL 36.00 TO LBL 45.00. BLENDED CORROSION ON THE LH PRESSURE FLOOR SILL ASSY APPROX LBL 36.00 - LBL 45.00 AND BETWEEN FS409.00 +128 AND FS559.00 IAW SRM
- [SDR SWIA2026040375666](https://openairdocs.org/sdr/SWIA2026040375666.md): Channel · cracked · Apr 3, 2026 · N973SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR FWD TRACK ON FS 574.00, BOTTOM CHANNEL NEAR DOOR SURROUND IS CRACKED. REMOVED AND REPLACED CARGO DOOR FWD TRACK ON FS 574.00 BOTTOM CHANNEL NEAR DOOR SURROUND IAW SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026040176209](https://openairdocs.org/sdr/SWIA2026040176209.md): Structure · cracked · Apr 1, 2026 · N973SW · Cndair CL6002B19 · Fuselage Main, Structure
  > FOUND CRACKED EXTRUSION ON THE CEILING OF THE RT MLG BAY. LOCATED BETWEEN BS 522 AND 533 ON RBL 47. REMOVED AND REPLACED EXTRUSION ON THE CEILING OF THE RT MLG BAY LOCATED BETWEEN BS 522 AND 533, RBL 47.00 IAW SRM 51-42-21.
- [SDR SWIA2026040176205](https://openairdocs.org/sdr/SWIA2026040176205.md): Fitting · cracked · Apr 1, 2026 · N973SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR AFT BALANCE SPRING MOUNT (FITTING) IS CRACKED ON THE UPPER INBD CORNER. REMOVED AND REPLACED THE CARGO DOOR AFT BALANCE SPRING MOUNT (FITTING) IN REFRERENCE WITH THE SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY. REF CP 322099324 FOR LEAK C
- [SDR SWIA2026040176204](https://openairdocs.org/sdr/SWIA2026040176204.md): Structure · cracked · Apr 1, 2026 · N973SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND CRACKED EXTRUSION ON THE CEILING OF THE LT MLG BAY. LOCATED BETWEEN FS 522.00 AND FS 533.00 ON LBL 47. REMOVED AND REPLACED EXTRUSION ON THE CEILING OF THE LT MLG BAY LOCATED BETWEEN FS 522.00 AND FS 533.00 ON LBL 47.00 IAW SRM 51-42-21. COMPLETED TASK
- [SDR SWI2026F00078](https://openairdocs.org/sdr/SWI2026F00078.md): Acm · fumes · Jan 16, 2026 · N973SW · Cndair CL6002B19 · Cabin Cooling System
  > FUMES DURING FLIGHT AFTER SWAPPING BLEEDS FROM APU TO ENGINES. FUMES RESOLVED WHEN LEFT PACK WAS SHUT OFF. (FLIGHT 5117)PERFORMED FIM TASK 21-21-0 PERFORMED OPERATION CHECK OF BOTH LEFT AND RIGHT PACKS PER 21-51-00, ISOLATED BLEED SOURCE AND PERFORMED OPERAT
- [SDR SWIA2025102700017](https://openairdocs.org/sdr/SWIA2025102700017.md): Door Frame · dented · Oct 17, 2025 · N973SW · Cndair CL6002B19 · Fuselage Main, Structure
  > DURING REPLACEMENT OF APU INLET DOOR FRAME SUPPORT 5-OFF OVERSIZED HOLES AND DENT DAMAGE WERE FOUND BETWEEN BS 654.5 - 672.2 AT S4L AFFECTING THE STACK UP OF S4L, BS 654.5 FRAME SECTOR, MTG FITTING AND CLIP. COMPLIED WITH REO 601R-53-61-8400 REV-, DATED 2025-1
- [SDR SWI2025F01434](https://openairdocs.org/sdr/SWI2025F01434.md): Skin · dented · Oct 17, 2025 · N973SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DURING REPLACEMENT OF APU INLET DOOR FRAME SUPPORT 5-OFF OVERSIZED HOLES AND DENT DAMAGE WERE FOUND BETWEEN FS654.50 - FS672.20 AT STR4L AFFECTING THE STACK UP OF STR4L, FS654.50 FRAME SECTOR, MTG FITTING AND CLIP (FILED OPEN)
- [SDR SWIA202510270012](https://openairdocs.org/sdr/SWIA202510270012.md): Frame Splice · cracked · Oct 12, 2025 · N973SW · Cndair CL6002B19 · Fuselage Main, Frame
  > BS 654.50 FRAME SPLICE AT STGR 6L IS CRACKED/CORRODED. PERFORMED TEMPORARY REPAIR TO BS 654.5 FRAME SPLICE AT S6L IN REFERENCE TO REO 601R-53-61-8397. PERFORMED EDDY CURRENT IN REFERENCE TO NDTM 53-00-097, PART 6 AND FOUND AREA TO BE CRACK FREE. COMPLIED WITH
- [SDR SWIA202502060005](https://openairdocs.org/sdr/SWIA202502060005.md): Pin · installed · Feb 5, 2025 · N973SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE WHEN RETRACTING GEAR. GEAR PIN STILL FOUND IN RIGHT MAIN LANDING GEAR (FLIGHT 5016 - FILED CLOSED) REMOVED RH MLG LOCKPIN IN REF TO CRJ 200 AMM 10-11-00. PERFORMED VISUAL INSPECTION OF MLGS AND DOORS IN REF TO CRJ 200 AMM 32-10-00, NO DEFE
- [SDR SWIA20240615](https://openairdocs.org/sdr/SWIA20240615.md): A/C Pack · odor · Jun 15, 2024 · N973SW · Cndair CL6002B19 · Cabin Cooling System
  > D: L PACK HI TEMP ON THE GROUND IN LAR AFTER REARMING THE PACKS AFTER LEFT ENGINE START AFTER SINGLE ENGINE TAXI. QRH RESOLVED ISSUE. ONCE ON THE GROUND IN DEN, LEFT PACK STARTED TO RISE IN TEMPERATURE AGAIN WITH A SMOKY SMELL. TURNED OFF LEFT PACK BEFORE IT O
- [SDR SWIA2024060500003](https://openairdocs.org/sdr/SWIA2024060500003.md): Warning Message · false activation · Jun 3, 2024 · N973SW · Cndair CL6002B19 · Central Warning
  > ANTI ICE DUCT WARNING MESSAGE THROUGH 23000FT. IN ICING CONDITIONS. WINGS AND COWLS SELECTED ON. RAN QRH, MESSAGE CLEARED AFTER 5MIN. DID NOT COME BACK ON. HAD TO SELECT WING STANDBY AND COWLS FOR DESCENT. (FLIGHT 4705 FILED CLOSED)THIS DISCREPANCY WAS TRANSFE
- [SDR SWIA202311130002](https://openairdocs.org/sdr/SWIA202311130002.md): Unknown · warning message · Nov 12, 2023 · N973SW · Cndair CL6002B19 · Central Warning
  > ANTI-ICE DUCT EMERGENCY MESSAGE POPPED UP IN FLIGHT IN ICING CONDITIONS.RAN QRH MESSAGE WENT AWAY AND NEVER RETURNED. (FLIGHT 5422 FILED CLOSED)
- [SDR SWI2023F00035](https://openairdocs.org/sdr/SWI2023F00035.md): Unknown · gouged · Feb 9, 2023 · N973SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > RH SIDE SEAT RAIL HAS MULTIPLE GOUGES FROM FS 409.00+16 THRU FS 409.00+112 (C-CHECK RO 3/11/2023) REMOVED AND NSTALLED NEW RH SIDE SEAT RAIL FS 409.00+16 THRU FS 409.00+112 REF CRJ200 AMM 53-01-11-400-802
- [SDR SWIA202300315020](https://openairdocs.org/sdr/SWIA202300315020.md): Unknown · gouged · Feb 9, 2023 · N973SW · Cndair CL6002B19 · Fuselage Structure (General)
  > RH SIDE SEAT RAIL HAS MULTIPLE GOUGES FROM FS 409.00+16 THRU FS 409.00+112 (C-CHECK RO 3/11/2023) REMOVED AND NSTALLED NEW RH SIDE SEAT RAIL FS 409.00+16 THRU FS 409.00+112 REF CRJ200 AMM 53-01-11-400-802
- [SDR SWI2023F00025](https://openairdocs.org/sdr/SWI2023F00025.md): Unknown · cracked · Feb 6, 2023 · N973SW · Cndair CL6002B19 · Fuselage Floor Panel
  > AT R/H FS280 AFT FLOOR ANGLE FOUND RBL 9.0 INBD AND OUTBD CLIPS CRACKED (C-CHECK RO 3/11/2023) REMOVED AND INSTALLED NEW INBOARD AND OUTBOARD CLIPS AT RBL9 / FS280 BEAM. REF: REO 601R-53-11-171, REV: D, 13 FEB 07 FOR FASTENER TYPE AND LOCATION.C/W 51-90
- [SDR SWI2023F00024](https://openairdocs.org/sdr/SWI2023F00024.md): Unknown · unknown · Feb 6, 2023 · N973SW · Cndair CL6002B19 · Fuselage Floor Panel
  > AT R/H FS280 AFT FLOOR ANGLE FOUND RBL 9.0 SPLICE ANGLE 601R-53-11-136-4 CRACKED (C-CHECK RO 3/11/2023) REPAIRED R/H FS280 AFT FLOOR ANGLE RBL 9.0 SPLICE ANGLE 601R-53-11-136-4 REF REO 601R-53-11-136, REV: A 2007-11-01.C/W 51-900-1003-SKY
- [SDR SWI2023F00023](https://openairdocs.org/sdr/SWI2023F00023.md): Unknown · unknown · Feb 6, 2023 · N973SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > PERFORM SPLICE REPAIR TO L/H INBD FLAP LWR INBD SKIN (C-CHECK RO 3/11/2023) PERMEANANTLY REPAIRED L/H INBD FLAP LWR SKIN DENT BUY PERFORMING AND COMPLYING WITH LWR SKIN SPLICE REPAIR REF BOMBARDIER REO 601R-57-52-1544 REV -- 2010-01-07. COMPLIED WITTH
- [SDR SWI2023F00022](https://openairdocs.org/sdr/SWI2023F00022.md): Unknown · cracked · Feb 6, 2023 · N973SW · Cndair CL6002B19 · Fuselage Floor Panel
  > AT R/H FS280 AFT FLOOR ANGLE FOUND RBL 9.0 INBD AND OUTBD CLIPS CRACKED (C-CHECK RO 3/11/2023) REMOVED AND INSTALLED NEW INBOARD AND OUTBOARD CLIPS AT RBL9 / FS280 BEAM. REF: REO 601R-53-11-171, REV: D, 13 FEB 07 FOR FASTENER TYPE AND LOCATION.C/W 51-90
- [SDR SWI2023F00021](https://openairdocs.org/sdr/SWI2023F00021.md): Unknown · unknown · Feb 6, 2023 · N973SW · Cndair CL6002B19 · Fuselage Floor Panel
  > AT R/H FS280 AFT FLOOR ANGLE FOUND RBL 9.0 SPLICE ANGLE 601R-53-11-136-4 CRACKED (C-CHECK RO 3/11/2023) REPAIRED R/H FS280 AFT FLOOR ANGLE RBL 9.0 SPLICE ANGLE 601R-53-11-136-4 REF REO 601R-53-11-136, REV: A 2007-11-01.C/W 51-900-1003-SKY
- [SDR SWIA20230315012](https://openairdocs.org/sdr/SWIA20230315012.md): Unknown · unknown · Feb 6, 2023 · N973SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > PERFORM SPLICE REPAIR TO L/H INBD FLAP LWR INBD SKIN (C-CHECK RO 3/11/2023) PERMEANANTLY REPAIRED L/H INBD FLAP LWR SKIN DENT BUY PERFORMING AND COMPLYING WITH LWR SKIN SPLICE REPAIR REF BOMBARDIER REO 601R-57-52-1544 REV -- 2010-01-07. COMPLIED WITTH
- [SDR SWI2023F00020](https://openairdocs.org/sdr/SWI2023F00020.md): Unknown · cracked · Feb 5, 2023 · N973SW · Cndair CL6002B19 · Fuselage Floor Panel
  > PILOT'S SIDE POST CRACKED AT UPPER BARREL NUT AS MARKED (C-CHECK RO 3/11/2023) REMOVED AND REPLACED PILOT SIDE POST. REF. CRJ200 SRM 51-42-21, SRM 51-41-02 AND DWG# 601R33007 REV. UCOMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19) STRUCTURA
- [SDR SWI2023F00019](https://openairdocs.org/sdr/SWI2023F00019.md): Unknown · cracked · Feb 5, 2023 · N973SW · Cndair CL6002B19 · Fuselage Floor Panel
  > FS280 AFT CENTER COCKPIT FLOOR SUPPORT IS CRACKED (C-CHECK RO 3/11/2023) REPAIRED FS280 AFT CENTER COCKPIT FLOOR SUPPORT REF DWG 600-34017, REV: AD, CRJ200 SRM 51-42-06, REVISION 39: MAR 10/2021.C/W 51-900-1003-SKY
- [SDR SWI2023F00018](https://openairdocs.org/sdr/SWI2023F00018.md): Unknown · cracked · Feb 5, 2023 · N973SW · Cndair CL6002B19 · Fuselage Floor Panel
  > PILOT'S SIDE POST CRACKED AT UPPER BARREL NUT AS MARKED (C-CHECK RO 3/11/2023) REMOVED AND REPLACED PILOT SIDE POST. REF. CRJ200 SRM 51-42-21, SRM 51-41-02 AND DWG# 601R33007 REV. UCOMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19) STRUCTURA
- [SDR SWIA2023003150011](https://openairdocs.org/sdr/SWIA2023003150011.md): Unknown · cracked · Feb 5, 2023 · N973SW · Cndair CL6002B19 · Fuselage Floor Panel
  > FS280 AFT CENTER COCKPIT FLOOR SUPPORT IS CRACKED (C-CHECK RO 3/11/2023) REPAIRED FS280 AFT CENTER COCKPIT FLOOR SUPPORT REF DWG 600-34017, REV: AD, CRJ200 SRM 51-42-06, REVISION 39: MAR 10/2021.C/W 51-900-1003-SKY
- [SDR SWI2023F00034](https://openairdocs.org/sdr/SWI2023F00034.md): Unknown · gouged · Jan 31, 2023 · N973SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > LH SIDE SEAT RAIL APPROX. FS409.0+112 THRU FS449.0+85.00 HAS GOUGES AND SCRATCHES. FLAGGED (C-CHECK RO 3/11/2023) COMPLETED INSTALL OF SEAT RAIL. REF: REO-601R-53-00-055 REV-C DATE 2017-03-21 REPAIR "B", TUC-8615 CAL DUE 31-OCT-2023.
- [SDR SWI2023F00033](https://openairdocs.org/sdr/SWI2023F00033.md): Unknown · gouged · Jan 31, 2023 · N973SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > LH SIDE SEAT RAIL APPROX. FS449.85 THRU FS499.00 HAS GOUGES AND SCRATCHES. FLAGGED (C-CHECK RO 3/11/2023) INSTALLED NEW SIDE SEAT RAIL. REF: REO-601R-53-00-055 REV-C DATE 2017-03-21 REPAIR "B", TUC-8615 CAL DUE 31-OCT-2023.
- [SDR SWI2023F00032](https://openairdocs.org/sdr/SWI2023F00032.md): Unknown · gouged · Jan 31, 2023 · N973SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > LH SIDE SEAT RAIL APPROX. FS499.00 THRU FS544.00 HAS GOUGES AND SCRATCHES. FLAGGED (C-CHECK RO 3/11/2023) REMOVED OLD SIDE SEAT RAIL AND INSTALLED NEW SIDE SEAT RAIL.REF: REO-601R-53-00-055 REV-C DATE 2017-03-21 REPAIR "B".
- [SDR SWI2023F00031](https://openairdocs.org/sdr/SWI2023F00031.md): Unknown · gouged · Jan 31, 2023 · N973SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > LH SIDE SEAT RAIL APPROX. FS544.00 THRU FS559.+96 HAS GOUGES AND SCRATCHES. FLAGGED (C-CHECK RO 3/11/2023) REMOVED OLD SIDE SEAT RAIL AND REPLACED OLD SIDE SEAT RAIL WITH NEW SIDE SEAT RAIL. REF: REO-601R-53-00-055 REV-C DATE 2017-03-21 REPAIR "B", TUC-
- [SDR SWI2023F00030](https://openairdocs.org/sdr/SWI2023F00030.md): Unknown · gouged · Jan 31, 2023 · N973SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > RH SIDE SEAT RAIL APPROX. FS544.00 THRU FS559.0+96 HAS GOUGES AND SCRATCHES. FLAGGED (C-CHECK RO 3/11/2023) REPLACED OLD SIDE SEAT RAIL WITH NEW SIDE SEAT RAIL. REF: REO-601R-53-00-055 REV-C DATE 2017-03-21 REPAIR "B", TUC-8615 CAL DUE 31-OCT-2023.
- [SDR SWIA2023003150444](https://openairdocs.org/sdr/SWIA2023003150444.md): Unknown · gouged · Jan 31, 2023 · N973SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > RH SIDE SEAT RAIL APPROX. FS499.00 THRU FS544.0 HAS GOUGES AND SCRATCHES. FLAGGED (C-CHECK RO 3/11/2023) RERMOVED OLD SIDE SEAT RAIL AND INSTALLED NEW SIDE SEAT RAIL.REF: REO-601R-53-00-055 REV-C DATE 2017-03-21 REPAIR "B".
- [SDR SWIA202300315018](https://openairdocs.org/sdr/SWIA202300315018.md): Unknown · gouged · Jan 31, 2023 · N973SW · Cndair CL6002B19 · Fuselage Structure (General)
  > LH SIDE SEAT RAIL APPROX. FS409.0+112 THRU FS449.0+85.00 HAS GOUGES AND SCRATCHES. FLAGGED (C-CHECK RO 3/11/2023) COMPLETED INSTALL OF SEAT RAIL. REF: REO-601R-53-00-055 REV-C DATE 2017-03-21 REPAIR "B", TUC-8615 CAL DUE 31-OCT-2023.
- [SDR SWI2023F00029](https://openairdocs.org/sdr/SWI2023F00029.md): Unknown · gouged · Jan 31, 2023 · N973SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > LH SIDE SEAT RAIL APPROX. FS449.85 THRU FS499.00 HAS GOUGES AND SCRATCHES. FLAGGED (C-CHECK RO 3/11/2023) INSTALLED NEW SIDE SEAT RAIL. REF: REO-601R-53-00-055 REV-C DATE 2017-03-21 REPAIR "B", TUC-8615 CAL DUE 31-OCT-2023.
- [SDR SWI2023F00028](https://openairdocs.org/sdr/SWI2023F00028.md): Unknown · gouged · Jan 31, 2023 · N973SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > LH SIDE SEAT RAIL APPROX. FS499.00 THRU FS544.00 HAS GOUGES AND SCRATCHES. FLAGGED (C-CHECK RO 3/11/2023) REMOVED OLD SIDE SEAT RAIL AND INSTALLED NEW SIDE SEAT RAIL.REF: REO-601R-53-00-055 REV-C DATE 2017-03-21 REPAIR "B".
- [SDR SWI2023F00027](https://openairdocs.org/sdr/SWI2023F00027.md): Unknown · gouged · Jan 31, 2023 · N973SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > LH SIDE SEAT RAIL APPROX. FS544.00 THRU FS559.+96 HAS GOUGES AND SCRATCHES. FLAGGED (C-CHECK RO 3/11/2023) REMOVED OLD SIDE SEAT RAIL AND REPLACED OLD SIDE SEAT RAIL WITH NEW SIDE SEAT RAIL. REF: REO-601R-53-00-055 REV-C DATE 2017-03-21 REPAIR "B", TUC-
- [SDR SWI2023F00026](https://openairdocs.org/sdr/SWI2023F00026.md): Unknown · gouged · Jan 31, 2023 · N973SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > RH SIDE SEAT RAIL APPROX. FS544.00 THRU FS559.0+96 HAS GOUGES AND SCRATCHES. FLAGGED (C-CHECK RO 3/11/2023) REPLACED OLD SIDE SEAT RAIL WITH NEW SIDE SEAT RAIL. REF: REO-601R-53-00-055 REV-C DATE 2017-03-21 REPAIR "B", TUC-8615 CAL DUE 31-OCT-2023.
- [SDR SWIA202300315015](https://openairdocs.org/sdr/SWIA202300315015.md): Unknown · gouged · Jan 31, 2023 · N973SW · Cndair CL6002B19 · Fuselage Structure (General)
  > RH SIDE SEAT RAIL APPROX. FS499.00 THRU FS544.0 HAS GOUGES AND SCRATCHES. FLAGGED (C-CHECK RO 3/11/2023) RERMOVED OLD SIDE SEAT RAIL AND INSTALLED NEW SIDE SEAT RAIL.REF: REO-601R-53-00-055 REV-C DATE 2017-03-21 REPAIR "B".
- [SDR SWI2023F00040](https://openairdocs.org/sdr/SWI2023F00040.md): Unknown · gouged · Jan 30, 2023 · N973SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > RH SIDE SEAT RAIL HAT CHANNEL HAS MULTIPLE GOUGES FROM FS409.112 THRU FS439.0. FLAGGED (C-CHECK RO 3/11/2023) REMOVED OLD HAT CHANNEL AND INSTALLED NEW HAT CHANNEL. REF: CRJ-200 S.R.M.51-41-00.
- [SDR SWI2023F00039](https://openairdocs.org/sdr/SWI2023F00039.md): Unknown · gouged · Jan 30, 2023 · N973SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > RH SIDE SEAT RAIL HAS MULTIPLE GOUGES FROM FS409.112 THRU FS449.0. FLAGGED (C-CHECK RO 3/11/2023) REMOVED AND INSTALLED NEW RH SIDE SEAT RAIL FS409.112 THRU FS449.0 REF CRJ200 AMM 53-01-11-400-802
- [SDR SWI2023F00038](https://openairdocs.org/sdr/SWI2023F00038.md): Unknown · cracked · Jan 30, 2023 · N973SW · Cndair CL6002B19 · Fuselage Main, Frame
  > *CRACK ON INTERNAL STRG3L SPLICE ANGLE ON AFT SIDE OF CIRCUMFERENTIAL FUSELAGE SPLICE AT FS280.00 (MARKED) (C-CHECK RO 3/11/2023) REPLACED INBD & OUTBD STRG3L SPLICE ANGLES ON AFT SIDE OF CIRCUMFERENTIAL FUSELAGE SPLICE AT FS280.00 REF DWG 600-31057 REV
- [SDR SWIA20230315233](https://openairdocs.org/sdr/SWIA20230315233.md): Unknown · corroded · Jan 30, 2023 · N973SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FORMER BETWEEN MID DD5 AND MID DD6 INTERCOSTAL IS CORRODED (C-CHECK RO 3/11/2023) REMOVED AND REPLACED PAX DOOR FORMER BETWEEN MID DD5 AND MID DD6 REF CRJ 200 SRM 51-42-06 AND DWG 601R31702 REV. N.COMPLIED WITH 51-900-1003-SKY (CL600-2B19) STR

Next page: https://openairdocs.org/aircraft/N973SW/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 = 'N973SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N973SW/reports

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