# Service difficulty reports: N941SW

A list on [N941SW](https://openairdocs.org/aircraft/N941SW.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 · 202 reports

- [SDR SWIA2026051376012](https://openairdocs.org/sdr/SWIA2026051376012.md): Windshield · sparks · May 13, 2026 · N941SW · Cndair CL6002B19 · Windshield/Door Rain/Ice Removal
  > ON INITIAL DESCENT, RIGHT WINDSHIELD BEGAN SPARKING HEAVILY. IMMEDIATELY FOLLOWED BY R WSHLD HEAT CAUTION. COMPLIED WITH QRH, DEACTIVATED RIGHT WINDSHIELD HEAT. APPROX 1 FOOT LONG CRACK OBSERVED ON OUTER PANE OF WINDSHIELD. RETURNED TO KORD. (FLIGHT 5376N) R
- [SDR SWIA2026020875815](https://openairdocs.org/sdr/SWIA2026020875815.md): Hinge Fitting · corroded · Feb 8, 2026 · N941SW · Cndair CL6002B19 · Elevator Structure
  > DURING REMOVAL OF BEARING ON L/H ELEVATOR I/B HINGE FITTING PN 600-24043-1, FOUND BEARING BORES TO BE CORRODED AND PITTED. I/B HINGE FITTING REQUIRES REPLACEMENT. REMOVED CORRODED L/H ELEVATOR INBD L/E HINGE FITTING ASSY. AND INSTALLED 1 EA NEW L/H ELEVATOR I
- [SDR SWIA2026020675808](https://openairdocs.org/sdr/SWIA2026020675808.md): Hinge Fitting · corroded · Feb 6, 2026 · N941SW · Cndair CL6002B19 · Elevator Structure
  > UPON REMOVAL ON JOB HN00293246 CAMP #31662049, FOUND R/H ELEVATOR L/E HINGE FITTING ASSY P/N 600-24043-1 @ ES16.52 TO HAVE PITTING CORROSION AND A HEAVY SCRATCH IN BEARING BORES. REPLACE HINGE FITTING ASSY. (C-CHECK RO 04/17/2026)REMOVED CORRODED R/H ELEVATOR
- [SDR SWIA2026011975809](https://openairdocs.org/sdr/SWIA2026011975809.md): Intercostal · corroded · Jan 19, 2026 · N941SW · Cndair CL6002B19 · Passenger/Crew Doors
  > FOUND PAX DOOR MID DD3 INTERCOSTAL HAS CORROSION. INSTALLED NEW MID DD3 INTERCOSTAL TO PAX DOOR REF SRM 51-42-06 AND DWG 601R31902 REV BW. LEAK CHECK GOOD COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY AND M-337
- [SDR SWIA2026011875816](https://openairdocs.org/sdr/SWIA2026011875816.md): Intercostal · corroded · Jan 18, 2026 · N941SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT INTERCOSTAL DD5 HAS CORROSION. REMOVED AND INSTALLED PAX DOOR NEW DD5 AFT INTERCOSTAL PN 601R31902-317 PER CRJ 200 SRM 51-42-06 AND DWG 601R31902 REV BW. LEAK CHECK GOOD COMPLIED WITHSKYWEST TASK CARD 51-900-1003-SKY AND M-337
- [SDR SWIA2026011775820](https://openairdocs.org/sdr/SWIA2026011775820.md): Hinge Fitting · gouged · Jan 17, 2026 · N941SW · Cndair CL6002B19 · Wing Main, Frame Structure
  > RIGHT WING FWD HINGE BOX FITTING AT WS127.25 GOUGED. REPAIRED RT WING FWD HINGE BOX FITTING AT WS127 PER REO 601R-57-21-4040 REV -. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026010875793](https://openairdocs.org/sdr/SWIA2026010875793.md): Hinge Arm · gouged · Jan 8, 2026 · N941SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP HINGE ARM ASSY AT WS80.50 HAS GOUGE ON FWD HINGE FITTING. REPAIRED FWD HINGE FITTING FOR LT INBD FLAP HINGE ARM ASSY AT WS80.50 PER REO 601R-57-54-388, REV--, COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026010775795](https://openairdocs.org/sdr/SWIA2026010775795.md): Window Frame · cracked · Jan 7, 2026 · N941SW · Cndair CL6002B19 · Fuselage Main, Structure
  > WINDSHIELD CENTER POST PILOTS SIDE LWR CLIP CRACKED AS MARKED (C-CHECK RO 04/17/2026)REMOVED AND INSTALLED NEW WINDSHIELD CENTER POST PILOT SIDE LOWER CLIP PN: 601R33237-1S - FITTING IAW CRJ-200 SRM 51-42-21-00 & BOMBARDIER INC. DWG# 601R33007 REV. -U. COMPLI
- [SDR SWIA2026010575791](https://openairdocs.org/sdr/SWIA2026010575791.md): Cleat · cracked · Jan 5, 2026 · N941SW · Cndair CL6002B19 · Fuselage Main, Structure
  > SUSPECTED CRACK ON CLEAT AT APPROX FS484, LBL36. INSTALLED NEW REPAIR ANGLE AT APPROX FS484 LBL36 REF REO 601R-53-41-3388 REV--
- [SDR SWIA2026010575786](https://openairdocs.org/sdr/SWIA2026010575786.md): Floor Support · corroded · Jan 5, 2026 · N941SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESSURE FLOOR SILL HAS SCREW SHANK STUCK AND CORROSION SURROUNDING FASTENER HOLE AT APPROX FS499, LBL36. BLENDED CORROSION ON PRESSURE FLOOR SILL AT APPROX FS499 LBL36, AND EVALUATED AS 'WITHIN LIMITS'. REF. REO 601R-53-41-666 REV. -C.
- [SDR SWIA2026010475785](https://openairdocs.org/sdr/SWIA2026010475785.md): Fitting · corroded · Jan 4, 2026 · N941SW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > FORWARD JACK FITTING LH AND RH INTERCOSTALS CORRODED. REPAIRED FWD JACK FITTING INTERCOSTAL FLANGES PER REO 601R-53-11-4050 REV --
- [SDR SWIA2026010375821](https://openairdocs.org/sdr/SWIA2026010375821.md): Intercostal · corroded · Jan 3, 2026 · N941SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR DD6 INTERCOSTAL HAS CORROSION BETWEEN FORMER FS329.76 & FORMER FS338.963. REMOVED AND INSTALLED NEW PAX DOOR DD6 INTERCOSTAL PN 601R318057-1 PER CRJ 200 SRM 51-42-06 AND DWG 601R31902 REV BW. LEAK CHECK GOOD COMPLIED WITH SKYWEST SKY CARD 51-90
- [SDR SWIA2026010375811](https://openairdocs.org/sdr/SWIA2026010375811.md): Floor Support · corroded · Jan 3, 2026 · N941SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR BEAM AT LBL9 BETWEEN APPROX. FS559 - FS559+20 HAS MULTIPLE SPOTS OF CORROSION (C-CHECK RO 04/17/2026)REPAIRED FLOORBEAM AT LBL9 BETWEEN FS559 AND FS559+20 PER REO 601R-53-41-3389 REV -- DATED 2026-02-09 AND REO 601R-53-00-005 (REV B) DATED 2011-01-06.
- [SDR SWIA2026010375797](https://openairdocs.org/sdr/SWIA2026010375797.md): Former · corroded · Jan 3, 2026 · N941SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR FORMER FS329.41 HAS CORROSION AT MID DD4 INTERCOSTAL REMOVED AND INSTALLED NEW PAX DOOR FS329.41 FORMER PN 601R318088-3 PER SRM 51-42-06 AND DWG 601R31902 REV BW. LEAK CHECK GOOD
- [SDR SWIA2026010375796](https://openairdocs.org/sdr/SWIA2026010375796.md): Floor Support · corroded · Jan 3, 2026 · N941SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR BEAM AT RBL9 BETWEEN APPROX. FS559+80 - FS559+32 HAS MULTIPLE SPOTS OF CORROSION. REPAIRED FLOOR BEAM RBL9 BETWEEN APPROX. FS559.+32 - FS559+80 REF SRM 51-42-34 AND REO 601R-53-51-730 REV--
- [SDR SWIA2026010375792](https://openairdocs.org/sdr/SWIA2026010375792.md): Intercostal · corroded · Jan 3, 2026 · N941SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR MID DD4 INTERCOSTAL HAS CORROSION. REMOVED AND INSTALLED NEW MID DD4 INTERCOSTAL PN 601R318081-13 TO PAX DOOR REF SRM 51-42-06 AND SRM 51-42-21 AND DWG 601R31902 REV BW. LEAK CHECK GOOD.COMPLIED WITH SKY CARD 51-900-1003-SKY
- [SDR SWIA2025123075806](https://openairdocs.org/sdr/SWIA2025123075806.md): Frame · corroded · Dec 30, 2025 · N941SW · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION FS589.00 FRAME FWD & AFT WEB LOWER FLANGE STGR20L -23L. REMOVED AND INSTALLED NEW FRAME FS589 REF. DWG 601R36025 REV-P AND CRJ200 SRM 51-42-06. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY AND FORM M-337. SEE CONTINUE CARD FOR DETAILS.
- [SDR SWIA2025123075800](https://openairdocs.org/sdr/SWIA2025123075800.md): Frame · corroded · Dec 30, 2025 · N941SW · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION FS605.00 FRAME FWD & AFT WEB LOWER FLANGE STGR20L -22L. REPLACED FRAME FS605.00 BETWEEN STGR20R AND STGR20L REF. DWG 601R36026 REV-AF, DWG 601R35005 REV-AG AND CRJ200 SRM 51-42-06. REPAIRED FRAME FS605.00 BETWEEN STGR20L AND STGR18L PER REO 601R-53-
- [SDR SWIA2025122975825](https://openairdocs.org/sdr/SWIA2025122975825.md): Roller · frozen · Dec 29, 2025 · N941SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LH OUTBD FLAP INBD GUIDE ROLLER FROZEN. REMOVED AND REPLACED LH O/B FLAP I/B GUIDE ROLLER PER CRJ 200 SRM 51-41-02 TW TUC4606 DUE 30-JUN-2026
- [SDR SWIA2025122975824](https://openairdocs.org/sdr/SWIA2025122975824.md): Roller · frozen · Dec 29, 2025 · N941SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RH OUTBD FLAP INBD GUIDE ROLLER FROZEN CAMP # 31447488. REMOVED AND REPLACED RH O/B FLAP I/B GUIDE ROLLER PER SRM 51-41-02 TW TUC4606 DUE 30-JUN-2026
- [SDR SWIA2025122775812](https://openairdocs.org/sdr/SWIA2025122775812.md): Pressure Blkhd · cracked · Dec 27, 2025 · N941SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT SIDE OF FS621.00 REAR PRESSURE BULKHEAD LH INTERCOSTAL CRACKED REPLACED LH INTERCOSTAL ON AFT SIDE OF FS621.00 REAR PRESSURE BULKHEAD PER DWG 601-35012 REV. D, REO 601R-53-61-422 REV. NC 2001-08-23, CRJ200 SRM 51-42-21.COMPLETED SKYWEST TASK CARD 51-900
- [SDR SWIA2025122775790](https://openairdocs.org/sdr/SWIA2025122775790.md): Pressure Blkhd · cracked · Dec 27, 2025 · N941SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT SIDE OF FS 621.00 REAR PRESSURE BULKHEAD RT INTERCOSTAL CRACKED. REPLACED RH INTERCOSTAL ON AFT SIDE OF FS 621 REAR PRESSURE BULKHEAD PER DWG 601-35012 REV. D, REO 601R-53-61-422 REV. NC 2001-08-23, SRM 51-42-21.
- [SDR SWIA2025122775789](https://openairdocs.org/sdr/SWIA2025122775789.md): Window Frame · cracked · Dec 27, 2025 · N941SW · Cndair CL6002B19 · Fuselage Main, Structure
  > CO-PILOT WINDSHIELD OUTBOARD POST LOWER OUTBOARD CLIP IS VISIBLY CRACKED. REPLACED CRACKED CO-PILOT WINDSHIELD OUTBOARD POST LOWER OUTBOARD CLIP WITH NEW CLIP. IAW SRM 51-42-21-00 REV. 39 AND DWG 601R33007 REV -U.
- [SDR SWIA2025122775787](https://openairdocs.org/sdr/SWIA2025122775787.md): Window Frame · cracked · Dec 27, 2025 · N941SW · Cndair CL6002B19 · Fuselage Main, Structure
  > PILOT WINDSHIELD OUTBOARD POST LOWER OUTBOARD CLIP IS VISIBLY CRACKED. REMOVED AND REPLACED WITH 1 EA OF NEW PILOT WINDSHIELD OUTBOARD POST LOWER OUTBOARD CLIP REF. SRM 51-42-21 AND DWG 601R33007 REV -U.
- [SDR SWIA2025122375819](https://openairdocs.org/sdr/SWIA2025122375819.md): Floorbeam · corroded · Dec 23, 2025 · N941SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOOR BOARD SUPPORT STRAP AT APPROX. FS.559.00 BETWEEN LBL9 AND LBL36 HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED FLOORBOARD SUPPORT STRAP ON FS 559 BETWEEN LBL9 AND LBL36 PER CRJ200 SRM 51-42-06 AND DWG# 601R31025 REV N. LEAK CHECK GOOD.COMPLIES WI
- [SDR SWIA2025122375818](https://openairdocs.org/sdr/SWIA2025122375818.md): Floor Support · corroded · Dec 23, 2025 · N941SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESSURE FLOOR SILL HAS MULTIPLE SPOTS OF CORROSION FROM FS.409+128 TO FS.559.00 (MARKED). (C-CHECK RO 04/17/2026)REPAIRED MULTIPLE SPOTS OF CORROSION ON PRESSURE FLOOR LH SILL FROM FS.409+128 TO FS.559.00 REF. REO 601R-53-41-666REV C DATED 2012-11-06 & REO 6
- [SDR SWIA2025122375817](https://openairdocs.org/sdr/SWIA2025122375817.md): Floorbeam · corroded · Dec 23, 2025 · N941SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOOR BOARD SUPPORT STRAP AT APPROX. FS.559.00 BETWEEN RBL9 AND RBL36 HAS MULTIPLE SPOTS OF CORROSION (MARKED). REPLACED FLOORBOARD SUPPORT STRAP AT FS.559.00 BETWEEN RBL9 AND RBL36 REF. DWG 601R31025 REV. N, CRJ200 SRM 51-42-06-00, AND CRJ200 SRM 51-42-15-0
- [SDR SWIA2025122375807](https://openairdocs.org/sdr/SWIA2025122375807.md): Floor Support · corroded · Dec 23, 2025 · N941SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESSURE FLOOR RH SILL HAS MULTIPLE SPOTS OF CORROSION FROM FS.409+128 TO FS.559. COMPLIED WITH REO 601R-53-41-666 REV -C, DATE 2012-11-06 DISPOSITION 1.2 STEPS A-F. BLENDED OUT CORROSION. NO FASTENERS AFFECTED. NDT COMPLIED WITH, NO DEFECTS EXIST. RESTORED F
- [SDR SWIA2025121775805](https://openairdocs.org/sdr/SWIA2025121775805.md): Skin · gouged · Dec 17, 2025 · N941SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > EXTERIOR LOWER SKIN PANEL HAS NUMEROUS DEEP GOUGES ABOVE AND AFT OF PNL 172 BR, GROUND AIR CONDITIONING CONNECTION. REMOVED 14EA GOUGE DAMAGE ON EXTERIOR LOWER SKIN AREA FROM FS589 TO FS605 AND STGR 26R TO STGR 20R APROX. REF. SRM 51-12-00 AND REPAIRED DENTS
- [SDR SWIA2025121675822](https://openairdocs.org/sdr/SWIA2025121675822.md): Vane · chafed · Dec 16, 2025 · N941SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT I/B FLAP VANE SKIN CHAFFED AT APPROX FLS 103.00 (C-CHECK RO 04/17/2026)REPLACED RH INBD FLAP VANE LEADING EDGE SKIN AT APPROX FLS103 REF CRJ200SRM 51-42-13 AND DWG 601R14302 (REV E).COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.
- [SDR SWIA2025121675804](https://openairdocs.org/sdr/SWIA2025121675804.md): Vane · chafed · Dec 16, 2025 · N941SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT I/B FLAP VANE SKIN CHAFFED AT APPROX FLS 55.00 RECEIVED, LOCATED AND DRILLED NEW RH INBD FLAP VANE LEADING EDGE PANEL AT FLS 55.00 REF CRJ200 SRM 51-40-11, SRM 51-42-13 AND DWG 601R14302 REV E. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA2025121675799](https://openairdocs.org/sdr/SWIA2025121675799.md): Vane · chafed · Dec 16, 2025 · N941SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT I/B FLAP VANE SKIN CHAFFED AT APPROX FLS 55.00 (C-CHECK RO 04/17/2026)BLENDED REPORTED CHAFED AREA ON LH WING I/B FLAP VANE LE SKIN PER CRJ200 SRM 51-12-00. BLENDED AREA WAS FOUND OUT OF LIMITS PER REF GREO 601R57-52-004 REV -D, DATED 2012-12-19, DAMAGE
- [SDR SWIA2025121575814](https://openairdocs.org/sdr/SWIA2025121575814.md): Trunnion · chafed · Dec 15, 2025 · N941SW · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > LH MLG TRUNNION AFT SIDE FWD FACE HAS CHAFE DAMAGE. REMOVED CHAFFING FROM THE LEFT-HAND MAIN LANDING GEAR TRUNNION, AFT SIDE, FORWARD FACE. NO LIMITS GIVEN IN CRJ200 SRM 57-21-27-01. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 601R-57-21-4014 REV. -- DATE: 202
- [SDR SWIA2025121575810](https://openairdocs.org/sdr/SWIA2025121575810.md): Trunnion · chafed · Dec 15, 2025 · N941SW · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > RH MLG TRUNNION AFT SIDE FWD FACE HAS CHAFE DAMAGE. (MARKED) (C-CHECK RO 04/17/2026)BLENDED OUT DAMAGE ON RH MLG TRUNNION AFT SIDE FWD FACE PER CRJ200 SRM 51-12-00 AND COMPLIED WITH ALL STEPS (1-6) OF REO 601R-57-21-4008, REV --, 2026-01-14. COMPLIED WITH TAS
- [SDR SWIA2025121575803](https://openairdocs.org/sdr/SWIA2025121575803.md): Trunnion · chafed · Dec 15, 2025 · N941SW · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > RIGHT MLG TRUNNION FWD SIDE AFT FACE HAS CHAFE DAMAGE. REMOVED DAMAGE (CHAFE) ON R/H MLG TRUNION FWD SIDE AFT FACE, REF. CRJ200 SRM 51-12-00-00. REPAIRED PER REO 601R-57-21-4008, REV --, 2026-01-14. COMPLIED WITH ALL STEPS AND FOUND TO BE STRUCTURALLY ACCEPTAB
- [SDR SWIA2025121575802](https://openairdocs.org/sdr/SWIA2025121575802.md): Bracket · cracked · Dec 15, 2025 · N941SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RH BRAKE PRESSURE TRANSDUCER BRACKET IN THE RH WHEEL WELL HAS 2EA CRACKS. (MARKED) (C-CHECK RO 04/17/2026) REMOVED AND INSTALLED NEW BRAKE TRANSDUCER BRACKET IN RH WHEEL WELL REF. CRJ200 SRM 51-42-06 AND BOMBARDIER DWG 601R750004 REV -A. COMPLIED WITH SKYWES
- [SDR SWIA2025121575798](https://openairdocs.org/sdr/SWIA2025121575798.md): Rib · corroded · Dec 15, 2025 · N941SW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > RH BATT RIB AT APPROX WS 53.60 BEHIND LH MLG TIRE BURST PANEL HAS EVIDENCE OF CORROSION. (MARKED) (C-CHECK RO 04/17/2026)REMOVED CORROSION FROM THE RIGHT-HAND BATT RIB AT APPROX. WS 53.60, BEHIND THE LEFT-HAND MAIN LANDING GEAR TIRE BURST PANEL, AND EVALUATE
- [SDR SWIA2025121575788](https://openairdocs.org/sdr/SWIA2025121575788.md): Trunnion · chafed · Dec 15, 2025 · N941SW · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > LH MLG TRUNNION FWD SIDE AFT FACE HAS CHAFE DAMAGE. REMOVED CHAFFING FROM THE LEFT-HAND MAIN LANDING GEAR TRUNNION, FORWARD SIDE, AFT FACE. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 601R-57-21-4014 REV. -.
- [SDR SWIA2025120675801](https://openairdocs.org/sdr/SWIA2025120675801.md): Accumulator · cracked · Dec 6, 2025 · N941SW · Cndair CL6002B19 · Landing Gear Brake System
  > CRACK IN LEFT FWD EQUIPMENT COMPARTMENT OTBD OF BRAKE ACCUMULATOR CHARGING POINT. REPAIRED CRACK ON LH FWD EQUIPMENT COMPARTMENT OTBD OF BRAKE ACCUMULATOR IAW REO 601R-53-11-111 REV.NC DATED 98-03-18.COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.
- [SDR SWIA2025120575823](https://openairdocs.org/sdr/SWIA2025120575823.md): Windshield · cracked · Dec 5, 2025 · N941SW · Cndair CL6002B19 · Flight Compartment Windows
  > PILOT'S WINDSHILED CRACKED BEYOND LIMITS. REMOVED PILOT'S WINDSHIELD AND INSTALLED SERVICEABLE WINDSHIELD. REF. AMM 56-11-01-400-801. OPS CHECK GOOD. LEAK CHECK GOOD.
- [SDR SWIA2025120475813](https://openairdocs.org/sdr/SWIA2025120475813.md): Skin · damaged · Dec 4, 2025 · N941SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > ADM# N941SW-6379 BETWEEN FS193 AND 202.75, AND BETWEEN STRINGER 21L AND STRINGER 23L. LENGTH 32", WIDTH 2.4", DEPTH.100". PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. REPAIRED EXTE
- [SDR SWIA2019031245622](https://openairdocs.org/sdr/SWIA2019031245622.md): Landing Gear · failed · Mar 12, 2019 · N941SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE WARNING MESSAGE FOR NOSE GEAR STUCK IN THE DOWN AND LOCKED POSITION ON DEPARTURE. ASSOCIATED WOW INPUT CAUTION MESSAGE. RAN QRH FOR BOTH MADE NORMAL LANDING ALL GEAR CAME DOWN AND LOCKED. (FLT#5830) FO: 03/12/2019 CLOSED REMOVED AND REPLACED NLG
- [SDR SWIA2019030745614](https://openairdocs.org/sdr/SWIA2019030745614.md): O-Ring · failed · Mar 6, 2019 · N941SW · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > GEAR DISAGREE MESSAGE ON ROTATION (PUTTING GEAR UP).NOSE GEAR WAS DOWN AND MAIN WHEELS WERE UP. RAN QRH AND GOT GEAR TO COME DOWN. RETURNED TO FIELD FOR A SAFE LANDING. (FLT#5351) FO: 03/06/2019 CLOSED REMOVED NLG SLIDER MEMBER AND NLG FLOATING PISTON FROM THE
- [SDR SWIA2019030545594](https://openairdocs.org/sdr/SWIA2019030545594.md): Warning System · false activation · Mar 4, 2019 · N941SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE WARNING MESSAGE ON DEPARTURE. DUE TO NOSE GEAR INITIALLY NOT RETRACTING NORMALLY. MESSAGE CLEARED AND NOSE GEAR CAME UP NORMAL IN 30 SECONDS WITHOUT ANY ACTION FROM FLIGHT CREW. WE NEVER RAN ANY QRC OR QRH PROCEDURES. RETURNED TO FIELD. (FLT#5438
- [SDR SWIA2018072644906](https://openairdocs.org/sdr/SWIA2018072644906.md): Dcu · failed · Jul 26, 2018 · N941SW · Cndair CL6002B19 · Extinguishing System
  > CARGO LO BOTTLE MESSAGE IN CRUISE. NO BOTTLE DISCHARGE FOUND UPON INSPECTION. DECLARED EMERGENCY. LANDED SAFELY. (FLT#5561) CLOSED TROUBLESHOT CARGO LO BOTTLE MESSAGE IAW FIM. REMOVED AND REPLACED DCU 1 AND DCU 2 IAW AMM.
- [SDR SWIA2018072644905](https://openairdocs.org/sdr/SWIA2018072644905.md): Connector · dirty · Jul 26, 2018 · N941SW · Cndair CL6002B19 · Fire Protection System Wiring
  > CARGO BOTTLE LOW CAUTION ON DESCENT. STAYED ON FOR DURATION OF FLIGHT. DECLARED AN EMERGENCY. LANDED SAFELY. (FLT 5638) CLOSED CLEANED AND INSPECTED CARGO BOTTLE CONNECTOR IAW AMM. OPS CHECK GOOD.
- [SDR SWIA201804304612](https://openairdocs.org/sdr/SWIA201804304612.md): Stop Fitting · out of position · Apr 4, 2018 · N941SW · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR SURROUND, LOWER OUTER EDGE. HAS TWO GOUGES CAUSED BY SERVICE DOOR LOWER FITTINGS. REMOVED AND REPLACED THE LOWER SERVICE DOOR STOP FITTING IAW SRM.
- [SDR SWIA201804304611](https://openairdocs.org/sdr/SWIA201804304611.md): Floor Support · corroded · Apr 3, 2018 · N941SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 574 - 621 LT FLOOR SUPPORT CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW REO AND SRM.
- [SDR SWIA201804304610](https://openairdocs.org/sdr/SWIA201804304610.md): Seat Track · corroded · Apr 3, 2018 · N941SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT OUTBOARD SEAT TRACK, BS 559+112 - 621CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW REO.
- [SDR SWIA201804304609](https://openairdocs.org/sdr/SWIA201804304609.md): Floor Support · corroded · Apr 3, 2018 · N941SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SUPPORT BS 559+80 - 621 CORRODED. REMOVED THE CORROSION IAW SRM.

Next page: https://openairdocs.org/aircraft/N941SW/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 = 'N941SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N941SW/reports

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