# Service difficulty reports: N923SW

A list on [N923SW](https://openairdocs.org/aircraft/N923SW.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 · 175 reports

- [SDR SWIA2026092377231](https://openairdocs.org/sdr/SWIA2026092377231.md): Angle · cracked · Sep 23, 2026 · N923SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR SURROUND STRUCTURE FWD CLIP IAW SRM 53-61-23 ITEM 54A AT BS 574 CRACKED. REMOVED AND REPLACED CARGO DOOR SURROUND STRUCTURE FWD CLIP IAW SRM 53-61-23, ITEM 54A, AT BS 574 IAW SRM 51-42-21 COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR J6BA202408140009](https://openairdocs.org/sdr/J6BA202408140009.md): Skin · damaged · Jun 18, 2024 · N923SW · Cndair CL6002B19 · Wing, Plate/Skin
  > L/H WING DAMAGED NEAR JACK PAD; DUE TO A/C COMING OFF JACKS. (C-CHECK RO 8/12/2024) REPAIRED L/H WING EXTERNAL SKIN NEAR JACKPAD IAW MHI RJ REO # 601R-57-21-3852 REV -- DATED 7/29/2024
- [SDR J6BA2024081400008](https://openairdocs.org/sdr/J6BA2024081400008.md): Structure · damaged · Jun 18, 2024 · N923SW · Cndair CL6002B19 · Fuselage Main, Structure
  > AFT LOWER FUSELAGE DAMAGED FROM TAILSTAND; DUE TO A/C COMING OFF JACKS. (C-CHECK RO 8/12/2024) REMOVED AND REPLACED 2 (EA) STRINGERS 25L AND STR 27, 1 (EA) GUSSET AT STR 27 AND 1 (EA) LH LOWER AFT SKIN PANEL PART # 600-21032-5 THAT WERE ALL DAMAGED BET
- [SDR J6BA2024081400618](https://openairdocs.org/sdr/J6BA2024081400618.md): Pad · damaged · Jun 18, 2024 · N923SW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > R/H WING DAMAGED NEAR JACK PAD; DUE TO A/C COMING OFF JACKS. (C-CHECK RO 8/12/2024) REPAIRED R/H WING OUTER SKIN NEAR JACK PAD IAW MHIRJ REO # 601R-57-51-1048 REV -- DATED 7/25/2024
- [SDR J6BA2024081400605](https://openairdocs.org/sdr/J6BA2024081400605.md): Frame · corroded · Jun 5, 2024 · N923SW · Cndair CL6002B19 · Fuselage Main, Frame
  > AT FS589 BETWEEEN STR 25R AND 24R THERE IS CORROSION ON THE LOWER FRAME FLANGE. (C-CHECK RO 8/12/2024) REPLACED FRAME SEE CAMP NO:69743 FOR COMPLETED MAINTENANCE AND CPCP
- [SDR J6BA202408140013](https://openairdocs.org/sdr/J6BA202408140013.md): Frame · corroded · Jun 4, 2024 · N923SW · Cndair CL6002B19 · Fuselage Main, Frame
  > AT FS589 BETWEEEN STR 26L AND 25L THERE IS CORROSION ON THE AFT FACE OF THE FRAME. (C-CHECK RO 8/12/2024) REPLACED FRAME SEE CAMP NO:69743 FOR COMPLETED MAINTENANCE AND CPCP (DG281)
- [SDR J6BA202408140012](https://openairdocs.org/sdr/J6BA202408140012.md): Frame · corroded · Jun 4, 2024 · N923SW · Cndair CL6002B19 · Fuselage Main, Frame
  > AT FS5898 STR 24L THERE IS CORROSION ON THE AFT FACE OF THE FRAME. (C-CHECK RO 8/12/2024) REPLACED FRAME SE CAMP NO:69743 FOR COMPLETED MAINTENANCE ND CPCP
- [SDR J6BA202408140011](https://openairdocs.org/sdr/J6BA202408140011.md): Frame · corroded · Jun 4, 2024 · N923SW · Cndair CL6002B19 · Fuselage Main, Frame
  > AT FS605 BETWEEEN STR 26L AND 25L THERE IS CORROSION ON THE FRAME CAP. (C-CHECK RO 8/12/2024) REFER TO CAMP:69738 FOR FRAME REPLACEMENT (DB641)
- [SDR J6BA202408140010](https://openairdocs.org/sdr/J6BA202408140010.md): Frame · corroded · Jun 4, 2024 · N923SW · Cndair CL6002B19 · Fuselage Main, Frame
  > AT FS605 BETWEEEN STR 27 AND 26R THERE IS CORROSION ON AFT FACE OF THE FRAME. (C-CHECK RO 8/12/2024) REMOED AND REPLACED FRAME 605 IAW CRJ 200 SRM 51-42-06
- [SDR J6BA2024081400604](https://openairdocs.org/sdr/J6BA2024081400604.md): Frame · corroded · Jun 4, 2024 · N923SW · Cndair CL6002B19 · Fuselage Main, Frame
  > AT FS589 BETWEEEN STR 26R AND 25L THERE IS CORROSION ON FWD FACE OF THE FRAME AND LOWER FRAME FLANGE. (C-CHECK RO 8/12/2024) REMOVED AND REPLACED FRAM 589 IAW CRJ 200 SRM 51-43-06
- [SDR J6BA2024081400603](https://openairdocs.org/sdr/J6BA2024081400603.md): Riser · cracked · Jun 3, 2024 · N923SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FWD STAIR RISE HAS A CRACK. (C-CHECK RO 8/12/2024) REPAIRED PAX DOOR FWD STAIR RISER IAW BOMBARDIER REO# PL601R-52-11-702 REV E
- [SDR J6BA2020610000819](https://openairdocs.org/sdr/J6BA2020610000819.md): Smoke Detector · activated · Aug 19, 2023 · N923SW · Cndair CL6002B19 · Smoke Detection
  > WE OBSERVED A CARGO SMOKE WARNING MESSAGE PASSING THROUGH 16000 FEET 10 MINUTES AFTER DEPARTING KPSP. WE DECLARED THE EMERGENCY AND COMPLIED WITH THE SMOKE CARGO QRH PROCEDURE. AT THIS TIME, THE CARGO FAN FAIL MESSAGE APPEARED.AFTER DISCHARGING BOTH CARGO FIRE
- [SDR SWIA2024053000819](https://openairdocs.org/sdr/SWIA2024053000819.md): Smoke Warning · illuminated · Aug 19, 2023 · N923SW · Cndair CL6002B19 · Smoke Detection
  > WE OBSERVED A CARGO SMOKE WARNING MESSAGE PASSING THROUGH 16000 FEET 10 MINUTES AFTER DEPARTING KPSP. WE DECLARED THE EMERGENCY AND COMPLIED WITH THE SMOKE CARGO QRH PROCEDURE. AT THIS TIME, THE CARGO FAN FAIL MESSAGE APPEARED.AFTER DISCHARGING BOTH CARGO FIRE
- [SDR SWIA202163047](https://openairdocs.org/sdr/SWIA202163047.md): None · corroded · Nov 4, 2021 · N923SW · Cndair CL6002B19 · Fuselage Main, Frame
  > *CORROSION ON ANGLE AT FS621 AT APPROXIMATELY LBL32. (C-CHECK RO 12/04/2021) *CORROSION ON ANGLE AT FS621 AT APPROXIMATELY LBL32. REO 601R-53-61-117 REV. -E DATED 2018-01-15,CRJ-200-SRM 51-42-06, AND CRJ-200-SRM 51-42-21. COMPLIED WITH 51-900-1003-SKY
- [SDR SWIA202163046](https://openairdocs.org/sdr/SWIA202163046.md): None · defective · Nov 4, 2021 · N923SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS621 BULKHEAD HAS 2EA FASTENER HOLES WITH DEFECT MARKED HAS #1 AND #8 COMMON TO HORIZONTAL STIFFENER AT RBL27 AND LBL27. (C-CHECK RO 12/04/2021) REPAIRED FS621 BULKHEAD HAS 2EA FASTENER HOLES AT #1 AND #8 COMMON TO HORIZONTAL STIFFENER AT RBL27 AND LBL
- [SDR SWIA202163045](https://openairdocs.org/sdr/SWIA202163045.md): None · dented · Nov 2, 2021 · N923SW · Cndair CL6002B19 · Fuselage Structure (General)
  > PAX DOOR HAVE A DENT ON AFT CORNER OUTER SKIN BETWEEN FS338.00 AND FS347.25 (C-CHECK RO 12/04/2021) REPAIRED PAX DOOR DENT ON AFT CORNER OUTER SKIN BETWEEN FS338.00 AND FS347.25 PER REO601R-52-11-2902 DATED 2021-11-14. COMPLIED WITH 51-900-1003-SKY.
- [SDR SWIA202163044](https://openairdocs.org/sdr/SWIA202163044.md): None · cracked · Oct 31, 2021 · N923SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > INTERCOSTAL PN.601R350121-1 IS CRAKED ON THE AFT SIDE OF THE FS.621 BULKHEAD, OTBD ON STGR.16L (C-CHECK RO 12/04/2021) REMOVED, LOCATED, DRILLED AND REPLACED INTERCOSTAL PN.601R350121-1 CRAKED ON THE AFT SIDE OF THE FS.621 BULKHEAD, OTBD ON STGR.16L IAW
- [SDR SWIA202163043](https://openairdocs.org/sdr/SWIA202163043.md): None · cracked · Oct 29, 2021 · N923SW · Cndair CL6002B19 · Fuselage Main, Frame
  > R/H SIDE CLIP AT FS 625.0 STR 14 IS CRACKED. (C-CHECK RO 12/04/2021) REMOVED AND REPLACED R/H SIDE CLIP WITH NEW AT FS 625.0 STR 14 REF CRJ 200 SRM 51-42-21, CRJ 200 SRM 51-40-06, CRJ 200 51-21-16 AND DWG 601-35012 REV -D COMPLIED WITH TASK CARD 51-900
- [SDR SWIA202163042](https://openairdocs.org/sdr/SWIA202163042.md): None · damaged · Oct 27, 2021 · N923SW · Cndair CL6002B19 · Ailerons
  > REPLACE RH INBOARD FLAP OUTBOARD VANE CAP LEADING EDGE (C-CHECK RO 12/04/2021) REMOVED AND INSTALLED RH INBOARD FLAP OUTBOARD VANE CAP LEADING EDGE IAW CRJ 200 SRM 51-42-10 PG 4 AND DWG 601R14302 REV E. COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATIO
- [SDR SWIA202163041](https://openairdocs.org/sdr/SWIA202163041.md): None · damaged · Oct 27, 2021 · N923SW · Cndair CL6002B19 · Ailerons
  > REPLACE RH INBOARD FLAP CENTER VANE CAP LEADING EDGE (C-CHECK RO 12/04/2021) REMOVED AND INSTALLED NEW R/H INBOARD FLAP CENTER VANE CAP REF CRJ 200 SRM 51-42-10 PG 4. AND DWG 601R14302 REV E. COMPLIED WITH 51-900-1003-SKY
- [SDR SWIA202163040](https://openairdocs.org/sdr/SWIA202163040.md): None · damaged · Oct 27, 2021 · N923SW · Cndair CL6002B19 · Ailerons
  > REPLACE RH INBOARD FLAP INBOARD VANE CAP LEADING EDGE (C-CHECK RO 12/04/2021) REMOVED AND INSTALLED NEW RH INBOARD FLAP INBOARD VANE CAP LEADING EDGE REF CRJ-200-SRM 51-42-13 AND DRAWING 601R14302 REV E. COMPLIED WITH 51-900-1003-SKY AND SEE CONTIN
- [SDR SWIA202163039](https://openairdocs.org/sdr/SWIA202163039.md): None · corroded · Oct 25, 2021 · N923SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *RBL9 FLOOR BEAM CAP HAS CORROSION BETWEEN FS559+48 AND FS559+79. (C-CHECK RO 12/04/2021) REMOVED AND INSTALLED NEW FLOOR BEAM SECTION FOR FS 559+10 TO FS 570 REF REO 601R-53-51-608 REV -- DATED 2021-11-10 AND DRAWING 601R31119 REV H. COMPLIED WITH 51
- [SDR SWIA202163038](https://openairdocs.org/sdr/SWIA202163038.md): None · chafed · Oct 24, 2021 · N923SW · Cndair CL6002B19 · Wing Structure
  > RH AILERON HAS CHAFFING ON UPPER FWD LEADING EDGES. (C-CHECK RO 12/04/2021) REMOVED AND INSTALLED NEW R/H AILERON LEADING EDGE SKIN REF CRJ-200 SRM 51-42-06, SRM 51-42-21, SRM 51-42-22 AND DWG CC670-13000 REV -D. COMPLIED WITH 51-900-1003-SKY AND SEE
- [SDR SWIA202163037](https://openairdocs.org/sdr/SWIA202163037.md): None · corroded · Oct 23, 2021 · N923SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *CORROSION ON RH FLOOR SILL BETWEEN FS559 AND FS559+16. (C-CHECK RO 12/04/2021) REMOVED AND REPLACED RH FLOOR SILL BETWEEN FS.559-FS.559+16. REF CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-21 AND DWG 601R31003 REV.K. ALL CHECKS GOOD. COMPLIED WITH 51-900-10
- [SDR SWIA202163036](https://openairdocs.org/sdr/SWIA202163036.md): None · corroded · Oct 23, 2021 · N923SW · Cndair CL6002B19 · Fuselage Main, Frame
  > *CORROSION ON CROSSBEAM CAP STRIP AT FS589 BETWEEN LBL9 AND LBL27. (C-CHECK RO 12/04/2021) REMOVED AND REPLACED CAP STRIP P/N 601R35031-165 WITH A NEW UNIT IAW CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21 AND BOMBARDIER DRAWING 601R35031 REV. Y. COMPLIED WI
- [SDR SWIA202163035](https://openairdocs.org/sdr/SWIA202163035.md): None · corroded · Oct 23, 2021 · N923SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > *FLOOR BEAM UPPER CAP AT LBL9 BETWEEN FS569 AND FS610 HAS CORROSION. (C-CHECK RO 12/04/2021) REPLACED FLLOR BEAM LBL9 BETWEEN FS569 AND FS610 PER CRJ200 SRM 51-23-00, SRM 51-42-21, SRM 51-45-00, / SRM 51-42-22 & SRM 51-42-34 PER STEPS 1 THROUGH 5 OF
- [SDR SWIA202163034](https://openairdocs.org/sdr/SWIA202163034.md): None · corroded · Oct 23, 2021 · N923SW · Cndair CL6002B19 · Fuselage Main, Frame
  > *FLOOR BEAM UPPER CAP AT LBL27 BETWEEN FS569 AND FS610 HAS CORROSION AND CRACKS. (C-CHECK RO 12/04/2021) REPLACED FLOOR BEAM LBL9 BETWEEN FS569 AND FS610 PER CRJ200 SRM 51-23-00, SRM 51-42-21, SRM 51-45-00, SRM 51-42-22 & SRM 51-42-34 PER MHI RJ R.E.O
- [SDR SWIA202163033](https://openairdocs.org/sdr/SWIA202163033.md): None · gouged · Oct 22, 2021 · N923SW · Cndair CL6002B19 · Wing Structure
  > *RIGHT AILERON IS GOUGED ON THE FWD AREA OF THE RIB @STA 302.649 (C-CHECK RO 12/04/2021) REMOVED AND INSTALLED NEW RIB P/N CC670-13025-2, REF. MHIRJ 200 DWG. CC670-13000, REV. D, CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-13. SEE CONTINUATION CARD FOR DETAI
- [SDR SWIA202163032](https://openairdocs.org/sdr/SWIA202163032.md): None · cracked · Oct 18, 2021 · N923SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: AD 2019-08-04/02 40000 FC - COMPLY WITH PARAGRAPH (J) OF AD 2019-08-04 BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH
- [SDR SWIA202163031](https://openairdocs.org/sdr/SWIA202163031.md): None · gouged · Oct 17, 2021 · N923SW · Cndair CL6002B19 · Fuselage Structure (General)
  > *SERVICE DOOR HAS GOUGES ON EXTERNAL SKIN. AREAS MARKED (C-CHECK RO 12/04/2021) BLENDED GOUGE DAMAGE FROM SERVICE DOOR EXTERNAL SKIN REF CRJ 200 SRM 51-12-00. BLENDED AREA FOUND TO BE OUT OF LIMIT REF CRJ 200 SRM 52-00-31. REPAIRED SERVICE DOOR EXTERNAL
- [SDR SWIA202163030](https://openairdocs.org/sdr/SWIA202163030.md): None · dented · Sep 10, 2021 · N923SW · Cndair CL6002B19 · Fuselage Structure (General)
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA55795-601R-53-61-7268 REV 923SW MXCODEID50571-PR - LARGE DENT IN OUTSIDE FUSELAGE SKIN AT CARGO DOOR CUT OUT LOWER AFT CORNER FS605.00 - FS619.00 BELOW STR17L. COMPLIED WITH TEMPORARY REPAIR PER REO 601R-53-61-7268 REV
- [SDR SWIA202158128](https://openairdocs.org/sdr/SWIA202158128.md): Door Frame · cracked · May 3, 2021 · N923SW · Cndair CL6002B19 · Fuselage Main, Structure
  > PAX DOOR CUTOUT, UPPER/FWD STOP-FITTING IS CRACKED. (FILED CLOSED) REMOVED AND INSTALLED NEW PAX DOOR CUTOUT, UPPER/FWD STOP-FITTING WITH SERVICEABLE PART IAW CRJ 200 SRM 51-42-21. / REF CP 22736778 FOR OPS CHECKS DISCREPANCIES.
- [SDR SWIA2019102346606](https://openairdocs.org/sdr/SWIA2019102346606.md): Frame · corroded · Oct 23, 2019 · N923SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 513 APPROX STR17 R/H FRAME FWD LOWER INBOARD CORNER HAS CORROSION AS MARKED. (C-CHECK) RO: 10/22/19. PERFORMED BLEND OUT OF CORROSION AT FS 513.00 APPROX. STGR.17 FRAME FWD. LOWER I/B CORNER. IAW SRM. FOUND TO BE WITHIN LIMITS. IAW SRM. RESTORED FINISH.
- [SDR SWIA2019102346604](https://openairdocs.org/sdr/SWIA2019102346604.md): Frame · corroded · Oct 23, 2019 · N923SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FOUND CORROSION ON FS 333 FRAME BETWEEN STR 18R TO STR 23R. (C-CHECK) RO: 10/22/19. REMOVED CORROSION ON FS 333 FRAME AT STRINGER 23R AND 24R IAW SRM. FOUND OUT OF LIMIT IAW SRM 53-00-00.REMOVED AN INSTALLED FS 333 NEW FRAME SECTOR FROM STR 18R TO STR 23R
- [SDR SWIA2019102346603](https://openairdocs.org/sdr/SWIA2019102346603.md): Floor Support · corroded · Oct 23, 2019 · N923SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *PLATES ON FLOOR SUPPORT IN FWD CABIN WHERE THE WARDROBE MOUNTS HAVE CORROSION AROUND THE BOLT HOLES. LOCATIONS ARE OTBD AFT, INBD FWD, AND INBD AFT. (C-CHECK) RO: 10/22/19. BLENDED OUT CORROSION ON WARDROBE FLOOR SUPPORT MOUNT PLATES, FABRICATED NEW WARDROBE
- [SDR SWIA2019102346602](https://openairdocs.org/sdr/SWIA2019102346602.md): Floor Support · corroded · Oct 23, 2019 · N923SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * R/H FLOOR SUPPORT STRUCTURE FLOOR EDGE MEMBER ( SILL) / FS559.0+80 TO FS621.0, (C-CHECK) RO: 10/22/19. 559+80 TO 569 FOUND OUT OF LIMITS, REPLACED. SILL FOUND WITHIN LIMITS BOMBARDIER.
- [SDR SWIA2019102346601](https://openairdocs.org/sdr/SWIA2019102346601.md): Floor Support · corroded · Oct 23, 2019 · N923SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *FLOOR SUPPORT AT PAX DOOR OPEN HAS CORROSION ON THE CUPS FOR THE HAND RAIL SUPPORT STRUTS. (C-CHECK) RO: 10/22/19. PERFORMED BLEND OUT OF CORROSION ON PAX DOOR CUT OUT SURROUND FLOOR STRUCTURE IAW SRM. FOUND TO BE WITHIN LIMITS. RESTORED FINISH.
- [SDR SWIA2019102346600](https://openairdocs.org/sdr/SWIA2019102346600.md): Floor Support · corroded · Oct 23, 2019 · N923SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *L/H FLOOR SUPPORT AT FS310, APPROX LBL40 HAS CORROSION. LOCATED NEAR THE FWD END OF THE PAX DOOR. MARK WITH GREASE PENCIL. (C-CHECK) RO: 10/22/19. PERFORMED BLEND OUT OF CORROSION AT L/H FLOOR SUPPORT FS 310.00, LBL 40. IAW SRM. FOUND TO BE WITHIN LIMITS. RE
- [SDR SWIA2019102346599](https://openairdocs.org/sdr/SWIA2019102346599.md): Seat Track · corroded · Oct 23, 2019 · N923SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > *L/H FLOOR SEAT TRACK AT LBL9 HAS MULTIPLE AREA OF CORROSION FROM FS409 TO FS409+128. (C-CHECK) RO: 10/22/19. BLENDED FLOOR SEAT TRACKS AT LBL9 FS409.00 TO 409+128 IAW SRM, FOUND TO BE OUT OF LIMITS IAW SRM, REMOVED AND REPLACED SEAT TRACKS LBL9 FS409 TO FS
- [SDR SWIA2019102346598](https://openairdocs.org/sdr/SWIA2019102346598.md): Seat Track · corroded · Oct 23, 2019 · N923SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > *L/H FLOOR SEAT TRACK AT LBL9 HAS MULTIPLE AREA OF CORROSION FROM FS364 TO FS409. (C-CHECK) RO: 10/22/19. BLENDED FLOOR SEAT TRACKS AT LBL9 FS364.00 TO FS409.00 IAW SRM, FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED SEAT TRACKS LBL9 FS364.00 TO FS 409.00
- [SDR SWIA2019102346597](https://openairdocs.org/sdr/SWIA2019102346597.md): Frame · corroded · Oct 23, 2019 · N923SW · Cndair CL6002B19 · Fuselage Main, Frame
  > *CORROSION FOUND ON FRAME FS349.00, STGR27.FLAGGED. (C-CHECK) RO: 10/22/19. BLENDED OUT OF CORROSION ON FRAME AR FS349.00 STGR27 IAW SRM 51-21-06. FOUND TO BE WITHIN LIMITS IAW SRM. RESTORED TOPCOAT FINISH.
- [SDR SWIA2019102346596](https://openairdocs.org/sdr/SWIA2019102346596.md): Skin · chafed · Oct 23, 2019 · N923SW · Cndair CL6002B19 · Trailing Edge Flaps
  > *R/H INBD FLAP VANE LEADING EGDE IS CHAFED AT 3EA LOCATIONS. INBD,CNT, AND OTBD. (C-CHECK) RO: 10/22/19. BLENDED OUT CHAFFING AT 3 EACH LOCATIONS ON THE RH IB FLAP VANE TO A SMOOTH CONTOUR.FOUND THE O/B AND I/B WITH IN LIMITS AND MIDDLE OUT OF LIMITS. REMOVE
- [SDR SWIA2019102346595](https://openairdocs.org/sdr/SWIA2019102346595.md): Angle · cracked · Oct 23, 2019 · N923SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS280 RBL9 I/B ANGLE CRACKED IN RADIUS, TOP OF ANGLE. (C-CHECK) RO: 10/22/19. FABRICATED NEW ANGLE AND REPLACED IAW REO.
- [SDR SWIA2019102346593](https://openairdocs.org/sdr/SWIA2019102346593.md): Vertical Beam · cracked · Oct 23, 2019 · N923SW · Cndair CL6002B19 · Fuselage Main, Structure
  > FS 409.00 + 128 RBL 27.00 VERTICAL BEAM IS CRACKED LOWER INBOARD CORNER AS MARKED. (C-CHECK) RO: 10/22/19. REPLACED WITH NEW FS409.00+128 RBL27.00 VERTICAL BEAM IAW. LEAK CHECK AND OPS TEST GOOD.
- [SDR SWIA2018080744975](https://openairdocs.org/sdr/SWIA2018080744975.md): Bracket · damaged · Aug 7, 2018 · N923SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > AFTER TAKE OFF, PUT THE GEAR UP BUT NOSE GEAR WOULD NOT COME UP. WARNING ILLUMINATED, GEAR DISAGREE. PERFORMED QRH AND DIVERTED. REPLACED THE OLEO PROXIMITY SENSOR BRACKET AND ADJUSTED THE SENSOR IAW AMM.
- [SDR SWIA201743763](https://openairdocs.org/sdr/SWIA201743763.md): Floorbeam · corroded · Aug 19, 2017 · N923SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280 FWD FLOORBEAM ANGLE UPPER SURFACE HAS CORROSION. REMOVED AND REPLACED FWD FLOORBEAM ANGLE IAW SRM.
- [SDR SWIA201743762](https://openairdocs.org/sdr/SWIA201743762.md): Plate · chafed · Aug 18, 2017 · N923SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT WING AFT FLAP HINGE ARM UNDER PANEL 683BB CHAFED ON THE INBD & OTBD GUIDE PLATE. REPLACED THE GUIDE PLATES IAW SRM.
- [SDR SWIA201743761](https://openairdocs.org/sdr/SWIA201743761.md): Plate · gouged · Aug 18, 2017 · N923SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT WING AFT FLAP HINGE ARM LOCATED UNDER PANEL 686BB HAS GOUGE INBD GUIDE PLATE. REPLACED OUT OF LIMITS ATTACHMENT BRACKET IAW SRM.
- [SDR SWIA201743760](https://openairdocs.org/sdr/SWIA201743760.md): Hinge Arm · gouged · Aug 18, 2017 · N923SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT WING FLAP AFT HINGE ARM LOCATED UNDER PANEL 695BB HAS A GOUGE AND HAS A WORN INBD GUIDE PLATE. REMOVED AND REPLACED BRACKET WITH SERVICEABLE BRACKET IAW SRM.
- [SDR SWIA201743759](https://openairdocs.org/sdr/SWIA201743759.md): Lever · chafed · Aug 18, 2017 · N923SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FWD PULL IN LEVER CHAFED. REPLACED LEVER IAW REO. WARNING AND OPERATIONAL CHECKED GOOD

Next page: https://openairdocs.org/aircraft/N923SW/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 = 'N923SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N923SW/reports

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