# Service difficulty reports: N943SW

A list on [N943SW](https://openairdocs.org/aircraft/N943SW.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 6 · 280 reports

- [SDR SWIA2026070777753](https://openairdocs.org/sdr/SWIA2026070777753.md): Skin · damaged · Jul 7, 2026 · N943SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT & TOOL DAMAGE ON SKIN SURFACE BTWN BS 654 - 672, S26R. THE DAMAGED SKIN WAS REPAIRED IAW REO 601R-53-61-8613, REV -. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026060177752](https://openairdocs.org/sdr/SWIA2026060177752.md): Floor Support · corroded · Jun 1, 2026 · N943SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON FLOOR SUPPORT RBL 9 BTW BS 409.48 - 409.80. REMOVED CORROSION FROM THE FLOOR SUPPORT, BS 409.48 - 409.80, RBL 9, MEASURED, EVALUATED, FOUND OUT OF LIMITS, RECEIVED NEW FLOOR SUPPORT, LOCATED AND DRILLED AND INSTALLED THE NEW FLOOR SUPPORT I
- [SDR SWIA2026052177754](https://openairdocs.org/sdr/SWIA2026052177754.md): Stringer · corroded · May 21, 2026 · N943SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STRINGER 19L, AFT NUT PLATES REMOVED STRINGER 19L, & STR 20L, STR 24R, BTW BS 409.80 - 409.96, & STR 25R - 25L BS 409. 96. PERFORMED A STRINGER SPLICE REPAIR ON STR 19L BTWN BS 402.98 - 409.112 IAW SRM 53-00-03. COMPLIED WITH TASK CARD 51
- [SDR SWIA2026041577756](https://openairdocs.org/sdr/SWIA2026041577756.md): Seat Track · corroded · Apr 15, 2026 · N943SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > AFT PAX CABIN SEAT TRACK FROM BS 559 -559.096 HAD CORROSION AROUND THE FASTENERS. REMOVED THE DAMAGED SEAT TRACK AND INSTALLED A NEW SEAT TRACK IAW SRM 51-41-02, REV 30. AND REO 601R-53-00-764, REV-.
- [SDR SWIA2026032777755](https://openairdocs.org/sdr/SWIA2026032777755.md): Skin · corroded · Mar 27, 2026 · N943SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > NUMEROUS SPOTS OF CORROSION ON FUSELAGE SKIN AT ATTACHMENT HOLES FOR FAIRING PANEL 195BB. BLENDED AND EVALUATED, FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW REO 601R-53-00-943, REV -, & SRM 53-00-31 PAR 4 B, FIG 101, & FIG 102. COMPLIED WITH TASK CARD 51-900-10
- [SDR SWIA2026032777751](https://openairdocs.org/sdr/SWIA2026032777751.md): Skin · corroded · Mar 27, 2026 · N943SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > NUMEROUS SPOTS OF CORROSION ON FUSELAGE SKIN AT ATTACHMENT HOLES FOR FAIRING PANEL 192BB. EVALUATED AND REPAIRED THE AREAS IAW REO 601R-53-31-1372, REV --, & REF CONTINUATION CARD FOR PROCEDURE DETAILS, LEAK CHECKED GOOD IAW AMM 21-50-00-863-801, PRESSURIZAT
- [SDR SWIA2026032777750](https://openairdocs.org/sdr/SWIA2026032777750.md): Floor Panel · cracked · Mar 27, 2026 · N943SW · Cndair CL6002B19 · Fuselage Floor Panel
  > LEFT TRU BAY FLOOR PANEL WAS CRACKED AT BS 193, LBL 30. PERFORMED A REPAIR ON THE TRU BAY FLOOR PANEL IAW REO 601R-53-11-4067, REV-, TASK CARD 51-900-1003-SKY COMPLIED WITH.
- [SDR SWIA2026032777749](https://openairdocs.org/sdr/SWIA2026032777749.md): Skin · corroded · Mar 27, 2026 · N943SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > NUMEROUS SPOTS OF CORROSION ON FUSELAGE SKIN AT ATTACHMENT HOLES FOR FAIRING PANEL 191BB. EVALUATED & REPAIRED AREAS AS REQUIRED IAW REO 601R-53-31-1372, REV --, REF CONTINUATION CARD FOR PROCEDURE DETAILS, LEAK CHECKED GOOD IAW AMM 21-50-00-863-801, NO WEIG
- [SDR SWIA2026032777748](https://openairdocs.org/sdr/SWIA2026032777748.md): Floor Panel · cracked · Mar 27, 2026 · N943SW · Cndair CL6002B19 · Fuselage Floor Panel
  > RIGHT TRU BAY FLOOR PANEL WAS CRACKED AT BS 193, RBL 30. PERFORMED A REPAIR ON THE ELECTRICAL BAY FLOOR PANEL IAW REO 601R-53-11-245, REV C, REPAIR TYPE II, VIEW II, SHEET 6.
- [SDR SWIA202508110009](https://openairdocs.org/sdr/SWIA202508110009.md): Landing Gear · warning message · Aug 9, 2025 · N943SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE MESSAGE AFTER GEAR SELECTOR HANDLE SELECTED IN UP POSITION ON TAKEOFF. RAN QRH. QRH DIRECTED US TO USE THE MANUAL GEAR EXTENSION. WE ULTIMATELY GOT THEN 3 GREEN DOWN AND LOCKED INDICATIONS ON ED-1. HAD A NORMAL, UNEVENTFUL LANDING AT ORD. (FLIGH
- [SDR SWIA20240718](https://openairdocs.org/sdr/SWIA20240718.md): Frame · cracked · Jul 18, 2024 · N943SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME 682.00 HAS 1 CRACK ON THE CAP ANGLE AT THE LOWER (6 O'CLOCK POSITION) JUST FOWARD OF THE AFT EQUIPMENT BAY DOOR OPENING. (FILED CLOSED) REPAIRED CRACK IN FRAME 682.00 ON THE CAP ANGLE AT THE LOWER (6 O'CLOCK POSITION) JUST FOWARD OF THE AFT EQUIPMEN
- [SDR SWIA20240809718](https://openairdocs.org/sdr/SWIA20240809718.md): Frame · cracked · Jul 18, 2024 · N943SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME 682.00 HAS 1 CRACK ON THE CAP ANGLE AT THE LOWER (6 O'CLOCK POSITION) JUST FOWARD OF THE AFT EQUIPMENT BAY DOOR OPENING. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWI2024F01096](https://openairdocs.org/sdr/SWI2024F01096.md): Floor Support · corroded · Jul 6, 2024 · N943SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH PRESSURE FLOOR SILL HAS 7 SPOTS OF CORROSION ON THE TOP SURFACE. CORROSION FOUND RANGING FROM FS 449.85 TO FS 513.00 (FILED CLOSED) DURING REPAIR PROCESS EVALUATION DISCOVERED 25 TOTAL AREAS OF CORROSION DAMAGE BETWEEN FS424.00-FS559.00 AND RBL36.00-R
- [SDR SWIA20240706](https://openairdocs.org/sdr/SWIA20240706.md): Floor Support · corroded · Jul 6, 2024 · N943SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LH PRESSURE FLOOR SILL HAS 4 SPOTS OF CORROSION ON THE TOP SURFACE. CORROSION FOUND RANGING FROM FS 513.00 TO FS 554.00 (FILED CLOSED) DURING REPAIR PROCESS EVALUATION DISCOVERED 19 AREAS OF CORROSION DAMAGE BETWEEN FS424.00-FS559.00 AND LBL36.00-LBL45.00
- [SDR SWIA202408090661](https://openairdocs.org/sdr/SWIA202408090661.md): Floor Support · corroded · Jul 6, 2024 · N943SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > RH PRESSURE FLOOR SILL HAS 7 SPOTS OF CORROSION ON THE TOP SURFACE. CORROSION FOUND RANGING FROM FS 449.85 TO FS 513.00 (FILED OPEN)
- [SDR SWIA20240809706](https://openairdocs.org/sdr/SWIA20240809706.md): Floor Support · corroded · Jul 6, 2024 · N943SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LH PRESSURE FLOOR SILL HAS 4 SPOTS OF CORROSION ON THE TOP SURFACE. CORROSION FOUND RANGING FROM FS 513.00 TO FS 554.00 (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWI2024F01094](https://openairdocs.org/sdr/SWI2024F01094.md): Skin · chafed · Jul 3, 2024 · N943SW · Cndair CL6002B19 · Ailerons
  > FOUND CHAFE DAMAGE ON LH AILERON OB LOWER LEADING EDGE SKIN. (FILED CLOSED)REMOVED AND REPLACED LH AILERON OB LOWER LEADING EDGE SKIN IN REF TO SRM 51-42-21. PAINTED SKIN IN REF TO SRM 51-25-01. COMPLETED TASK CARD 51-900-1003-SKY AND M-337.
- [SDR SWIA20240703](https://openairdocs.org/sdr/SWIA20240703.md): Pressure Blkhd · cracked · Jul 3, 2024 · N943SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT SIDE OF PRESSURE BULKHEAD @ FS621.00 JUST OUTBOARD OF RBL 36.20 AND INLINE WITH STRINGER 14R, CLIP/ANGLE CRACKED. (FILED CLOSED) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWI2024F00658](https://openairdocs.org/sdr/SWI2024F00658.md): Skin · chafed · Jul 3, 2024 · N943SW · Cndair CL6002B19 · Ailerons
  > FOUND CHAFE DAMAGE ON LH AILERON OB LOWER LEADING EDGE SKIN. (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA2024070500003](https://openairdocs.org/sdr/SWIA2024070500003.md): Pressure Blkhd · cracked · Jul 3, 2024 · N943SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT SIDE OF PRESSURE BULKHEAD @ FS621.00 JUST OUTBOARD OF RBL 36.20 AND INLINE WITH STRINGER 14R, CLIP/ANGLE CRACKED. (OPEN)
- [SDR SWIA20240819701](https://openairdocs.org/sdr/SWIA20240819701.md): Strap · corroded · Jul 1, 2024 · N943SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > CORROSION ON LH STRAP AT FS 559.00. RUNS LATERALLY BETWEEN LBL 36.00 AND LBL 27.00 (FILED CLOSED)REMOVED AND REPLACED LH STRAP AT FS 559.00.THAT RUNS LATERALLY BETWEEN LBL 36.00 AND LBL 27.00 IN REF TO SRM 51-42-06.
- [SDR SWIA20240809659](https://openairdocs.org/sdr/SWIA20240809659.md): Strap · corroded · Jul 1, 2024 · N943SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON RH STRAP AT FS 559.00. RUNS LATERALLY BETWEEN RBL 36.00 AND RBL 27.00 (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA20240809701](https://openairdocs.org/sdr/SWIA20240809701.md): Strap · corroded · Jul 1, 2024 · N943SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON LH STRAP AT FS 559.00. RUNS LATERALLY BETWEEN LBL 36.00 AND LBL 27.00 (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWI2024F01095](https://openairdocs.org/sdr/SWI2024F01095.md): Pressure Blkhd · gouged · Jun 29, 2024 · N943SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > 7 GOUGED RIVET HEADS AND 12 GOUGE MARKS ON THE FWD FACE OF THE AFT PRESSURE BULKHEAD AT FS 621.00 (FILED CLOSED) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA20240629](https://openairdocs.org/sdr/SWIA20240629.md): Floorbeam · corroded · Jun 29, 2024 · N943SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION AND CRACK ON FLOOR SUPPORT BEAM IN THE CARGO BAY THAT RUNS LATERALLY FROM STGR 17L AND STGR 17R AT FS 589.00 AND LBL 38.40. (FILED CLOSED) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWI2024F00660](https://openairdocs.org/sdr/SWI2024F00660.md): Rivet · gouged · Jun 29, 2024 · N943SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > 7 GOUGED RIVET HEADS AND 12 GOUGE MARKS ON THE FWD FACE OF THE AFT PRESSURE BULKHEAD AT FS 621.00 (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA20240809629](https://openairdocs.org/sdr/SWIA20240809629.md): Floorbeam · corroded · Jun 29, 2024 · N943SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION AND CRACK ON FLOOR SUPPORT BEAM IN THE CARGO BAY THAT RUNS LATERALLY FROM STGR 17L AND STGR 17R AT FS 589.00 AND LBL 38.40. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA202310030002](https://openairdocs.org/sdr/SWIA202310030002.md): Not Reported · warning message · Oct 2, 2023 · N943SW · Cndair CL6002B19 · Landing Gear System
  > D; ON DEPARTURE WHEN GEAR LEVER SELECTED UP, WARNING MESSAGES NOSE DOOR AND GEAR DISAGREE. QRH PROCEDURE RESULTED IN DOWN 3 GREEN. RETURNED TO LAND AT DENVER TAXIIED BACK WITHOUT ISSUE.C; DEFERRED LANDING GEAR RETRACTION SYSTEM REF CRJ200 MEL 32-30-1. MX ACTIO
- [SDR SWIA202159277](https://openairdocs.org/sdr/SWIA202159277.md): Pin · out of adjust · Jul 2, 2021 · N943SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREEE WARNING MESSAGE ON TAKEOFF. GEAR POSTED SIX SECONDS AFTER POSITIONING GEAR HANDLE UP. COMPLETED QRH PROCEDURE. COMPLETED EMER 13-3. GEAR DISAGREE WARNING MESSAGE CLEARED. LANDED AT 47,000 LBS. NO FURTHER ISSUES. (FLIGHT 5325 - FILED CLOSED)
- [SDR SWIA202157281](https://openairdocs.org/sdr/SWIA202157281.md): Access Panel · damaged · Mar 30, 2021 · N943SW · Cndair CL6002B19 · Elevator, Plate/Skin
  > ELEVATOR ACESS PANEL 334BB HAS OVERSIZED SCREW HOLE (C-CHECK RO 4/2/2021) PERFORMED REPAIR TO PANEL 334BB IAW REO 601R-55-21-544 REV: -- DATE: 2021-3-31 SEE CONTINUATION CARD FOR DETAILS
- [SDR SWIA202157249](https://openairdocs.org/sdr/SWIA202157249.md): Bonding Plate · corroded · Mar 18, 2021 · N943SW · Cndair CL6002B19 · Nacelle/Pylon, Main Frame
  > LH PYLON TRAILING EDGE LOWER IB AND OB BONDING PLATES HAVE CORROSION (C-CHECK RO 4/2/2021) (C-CHECK RO 4/2/2021) REMOVED DAMAGED BONDING PLATES AND INSTALLED SERVICEABLE PLATES ON LH PYLON IAW CRJ 200 AMM 51-80-00-400-808 AND CRJ 200 SRM 51-42-13. R
- [SDR SWIA202157327](https://openairdocs.org/sdr/SWIA202157327.md): Stop Fitting · gouged · Mar 17, 2021 · N943SW · Cndair CL6002B19 · Emergency Exits
  > WHILE REMOVING L/H OVERWING EMERGENCY EXIT DOOR STOP FITTINGS P/N 600-31381-1 FOUND 5 EACH GOUGED BEYOND LIMITS (C-CHECK RO 4/2/2021) REMOVED AND REPLACED 5 EACH STOP FITTINGS 600-31381-1 FROM L/H OVERWING EMERGENCY EXIT DOOR IAW CRJ 200 AMM 52-21-00-000
- [SDR SWIA202157280](https://openairdocs.org/sdr/SWIA202157280.md): Frame · damaged · Mar 4, 2021 · N943SW · Cndair CL6002B19 · Fuselage Main, Frame
  > F.S. 3.19 FRAME HAS 1 EA ELONGATED HOLE IN LOWER FLANGE AT STR 26R (C-CHECK RO 4/2/2021) REPAIRED FS 319 FRAME 1 EA ELONGATED HOLE IN LOWER FLANGE AT STR 26R IAW MHIRJ REO 601R-53-21-3410 REV -- DATED 2021-03-17 COMPLETED SKYCARD 51-900-1003-SKY ATTACHED
- [SDR SWIA202157255](https://openairdocs.org/sdr/SWIA202157255.md): Stiffener · cracked · Feb 24, 2021 · N943SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > WHILE COMPLYING WITH REO 601R-53-61-1240 REV -D DATED 2016-10-31 FOUND LEFT HAND LOWER STIFFNER AT FS 621 AFT SIDE OF BULKHEAD CRACKED (C-CHECK RO 4/2/2021) REMOVED AND REPLACED WITH NEW SERVICABLE STIFFNER PN- 601R36008-51 IAW CRJ 200 SRM 51-42-06, 51-2
- [SDR SWIA202157323](https://openairdocs.org/sdr/SWIA202157323.md): Intercostal · corroded · Feb 21, 2021 · N943SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON INTERCOSTAL F.S. 310 STR 16L-15L AFT INBD SIDE OF FLANGE ( 3RD INTERCOSTAL FROM FLOOR) JUST FWD OF PX DOOR (C-CHECK RO 4/2/2021) REPAIRED CORROSION FOUND ON INTERCOSTAL F.S. 310 STR 16L-15L AFT INBD SIDE OF FLANGE ( 3RD INTERCOSTAL FRO
- [SDR SWIA202157322](https://openairdocs.org/sdr/SWIA202157322.md): Shear Tie · corroded · Feb 21, 2021 · N943SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > CORROSION FOUND ON SHEAR TIE STRAP AT PX DOOR FWD LOWER DOOR CUT OUT F.S. 310 STRINGERS 17L-15L (C-CHECK RO 4/2/2021) CORROSION FOUND ON SHEAR TIE STRAP AT PX DOOR FWD LOWER DOOR CUT OUT F.S. 310 STRINGERS 17L-15L FOUND TO BE OUT OF LIMITS PER SRM 51-21
- [SDR SWIA202157247](https://openairdocs.org/sdr/SWIA202157247.md): Shear Tie · cracked · Feb 17, 2021 · N943SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > CRACKED FRAME CLEAT FOUND AT F.S. 280 STRINGER 3L (C-CHECK RO 4/2/2021) REMOVED CRACKED CLEAT AND INSTALLED NEW CLEAT AT F.S. 280 STRINGER 3L IAW CRJ200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21
- [SDR SWIA202157278](https://openairdocs.org/sdr/SWIA202157278.md): Bracket · cracked · Feb 13, 2021 · N943SW · Cndair CL6002B19 · Passenger/Crew Doors
  > BRACKET ON INTERCOSTAL, DOOR DATUM 1 1ST FROM FWD UPPER END OF PAX DOOR P/N 601R318084-2 IS CRACK AROUND RIVET HOLE (C-CHECK RO 4/2/2021) REMOVED AND REPLACE BRACKET ON INTERCOSTAL DOOR DATUM 1 1ST FROM FWD UPPER END OF THE PAX DOOR IAW CRJ 200 SRM 51-40-
- [SDR SWIA202157260](https://openairdocs.org/sdr/SWIA202157260.md): Bulkhead · cracked · Feb 13, 2021 · N943SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > INDICATONS NOTED AT FS 621 REAR PRESSURE BULKHEAD LBL9.5/ WL131,1.9" LONG AND 95% FULL SCREEN HEIGHT, LBL18/ WL 131, 3" L0NG AND 100% FULL SCREEN HEIGHT, BL0.00/ WL126, 9.5" LONG AND 97% FULL SCREEN HEIGHT AND RBL18 /WL131, 4.25" LONG AND 100% FULL SCREEN HEIG
- [SDR SWIA202157321](https://openairdocs.org/sdr/SWIA202157321.md): Washer · corroded · Feb 12, 2021 · N943SW · Cndair CL6002B19 · Spoilers
  > RH IN BOARD GROUND SPOILER, HINGES ATTACHING (NUTS AND WASHERS) HARDWARE CORRODED AT APPROX WS 97, WS75 AND WS56 (C-CHECK RO 4/2/2021) REMOVED CORRODED HARDWARE ON RH INBD GROUND SPOILER AND INSTALLED SEVICEABLE HARDWARE IAW CRJ 200 AMM 27-65-01-000/400-8
- [SDR SWIA202157320](https://openairdocs.org/sdr/SWIA202157320.md): Washer · corroded · Feb 12, 2021 · N943SW · Cndair CL6002B19 · Spoilers
  > RH OUTBOARD GROUND SPOILER HINGES, ALL ATTACHING HARDWARE (NUTS AND WASHER) CORRODED AT APPROX WS 139, WS120, AND WS104. (C-CHECK RO 4/2/2021) REMOVED AND INSTALLED SERVICABLE RH OB GROUND SPOILER ATTACHING HARDWARE(NUTS AND WASHERS) AT WS 139, WS 120 AND
- [SDR SWIA202157319](https://openairdocs.org/sdr/SWIA202157319.md): Nut · corroded · Feb 12, 2021 · N943SW · Cndair CL6002B19 · Spoilers
  > RH FLIGHT SPOILER HINGES, ALL ATTACHING HARDWARE (NUTS AND WASHER) CORRODED AT APPROX WS 213, WS191, WS183 AND WS162. (C-CHECK RO 4/2/2021) REMOVED AND REPLACED RH FLIGHT SPOILER ATTACHING HARDWARE (NUTS AND WASHERS) IAW CRJ200 AMM 27-64-05-400-801
- [SDR SWIA202157318](https://openairdocs.org/sdr/SWIA202157318.md): Washer · corroded · Feb 12, 2021 · N943SW · Cndair CL6002B19 · Spoilers
  > RH SPOILERON, ALL HINGES ATTACHING HARDWARE (NUTS AND WASHERS) CORRODED AT APPROX WS 274, WS255, WS246 AND WS 226. (C-CHECK RO 4/2/2021) REMOVED CORRODED HARDWARE ON RH SPOILERON AND REPLACED WITH SERVICEABLE HARDWARE IAW CRJ 200 AMM27-64-05-000/400-801.
- [SDR SWIA202157277](https://openairdocs.org/sdr/SWIA202157277.md): Support Angle · corroded · Feb 12, 2021 · N943SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT FORMER ANGLE CORRODED P/N 601R318732-3 (C-CHECK RO 4/2/2021) REMOVED AND REPLACED PAX DOOR AFT FORMER ANGLE IAW CRJ 200 SRM 51-40-11, 51-42-06, 51-42-21, & SKY CARD 51-900-1003-SKY NO WEIGHT CHANGE, FORM 337 IS ATTACHED REF ATTACHED CONTINUA
- [SDR SWIA202157294](https://openairdocs.org/sdr/SWIA202157294.md): Drag Angle · cracked · Feb 11, 2021 · N943SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT DRAG ANGLE IS CRACK REQUIRES REPLACEMENT P/N 601R31772-5 (C-CHECK RO 4/2/2021) REMOVED AND REPLACED PAX DOOR AFT DRAG ANGLE IAW CRJ 200 SRM 51-40-11 SRM 51-42 -06 REV 38 7-10-19
- [SDR SWIA202157317](https://openairdocs.org/sdr/SWIA202157317.md): Bracket · corroded · Feb 10, 2021 · N943SW · Cndair CL6002B19 · Passenger/Crew Doors
  > BRACKET ON INTERCOSTAL DD6 AFT SIDE OF PAX DOOR 2ND FROM HINGE CORRODED P/N 601R318084-2 (C-CHECK RO 4/2/2021) REMOVED AND REPLACED BRACKET ON INTERCOSTAL DD6 ON PAX DOOR IAW CRJ 200 SRM 51-40-11, 51-42-06, & SKYCARD 51-900-1003-SKY NO WEIGHT CHANGE FORM
- [SDR SWIA202157276](https://openairdocs.org/sdr/SWIA202157276.md): Intercostal · corroded · Feb 10, 2021 · N943SW · Cndair CL6002B19 · Passenger/Crew Doors
  > CLIP, INTERCOSTAL DD7 AFT SIDE OF PAX DOOR 1ST FROM HINGE CORRODED P/N 601R318824-2 (C-CHECK RO 4/2/2021) REMOVED AND REPLACED THE CLIP, INTERCOSTAL DD7 ON AFT SIDE OF THE PAX DOOR IAW CRJ 200 SRM 51-40-11,, 51-42-06, & SKY CARD 51-900-1003-SKY FORM 337
- [SDR SWIA202157275](https://openairdocs.org/sdr/SWIA202157275.md): Intercostal · corroded · Feb 10, 2021 · N943SW · Cndair CL6002B19 · Passenger/Crew Doors
  > INTERCOSTAL DD7 AFT SIDE OF PAX DOOR 1ST FROM HINGE CORRODED P/N 601R318825-1 (C-CHECK RO 4/2/2021) REMOVED AND REPLACED INTERCOSTAL DD7 AFT SIDE OF PAX DOOR IAW CRJ 200 SRM 51-40-11, 51-42-06, AND SKYCARD 51-900-1003-SKY NO WEIGHT CHANGE 337 FORM IS ATTA
- [SDR SWIA202157274](https://openairdocs.org/sdr/SWIA202157274.md): Intercostal · corroded · Feb 10, 2021 · N943SW · Cndair CL6002B19 · Passenger/Crew Doors
  > INTERCOSTAL DD6 AFT SIDE OF PAX DOOR 2ND FROM HINGE CORRODED P/N 601R31902-323 (C-CHECK RO 4/2/2021) REMOVED AND REPLACED INTERCOSTAL DD6 ON PAX DOOR IAW CRJ 200 SRM 51-40-11, 51-42-06, & SKY CARD 51-900-1003-SKY NO WEIGHT CHANGE, FORM 337 IS ATTACHED, RE
- [SDR SWIA202157273](https://openairdocs.org/sdr/SWIA202157273.md): Intercostal · corroded · Feb 10, 2021 · N943SW · Cndair CL6002B19 · Passenger/Crew Doors
  > INTERCOSTAL AFT SIDE OF PAX DOOR 3ND FROM HINGE CORRODED P/N 601R31902-317 (C-CHECK RO 4/2/2021) REMOVED AND REPLACED INTERCOSTAL AFT SIDE OF PAX DOOR IAW CRJ 200 SRM 51-40-11, 51-42-06, & SKYCARD 51-900-1003-SKY, NO WEIGHT CHANGE FORM 337 IS ATTACHED REF

Next page: https://openairdocs.org/aircraft/N943SW/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 = 'N943SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N943SW/reports

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