# Service difficulty reports: N945SW

A list on [N945SW](https://openairdocs.org/aircraft/N945SW.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 7 · 305 reports

- [SDR SWIA2026100977593](https://openairdocs.org/sdr/SWIA2026100977593.md): Manifold · leaking · Oct 9, 2026 · N945SW · Cndair CL6002B19 · Hydraulic System, Main
  > HYDRAULIC SYSTEM TWO WENT FROM 50 TO 5 IN 30 MINUTES NO MESSAGE ASSOCIATED UPON LANDING OBSERVED HYDRAULIC FLUID LEAKING DOWN AC FROM THE AFT COMPARTMENT BAY FLIGHT 5100. UPON ARRIVAL TO AC FOUND HYD SYS 2 AT 10 FOUND LEAK COMING FROM HYD SYS 2 PRESSURE MAN
- [SDR SWIA2026031775521](https://openairdocs.org/sdr/SWIA2026031775521.md): Lamp · burned out · Mar 17, 2026 · N945SW · Cndair CL6002B19 · Flight Compartment Lighting
  > HEARD A POP AND FAINT SMELL OF SMOKE (PLASTIC) ON CLIMBOUT FOR A COUPLE SECONDS. APPEARS TO BE THE OBSERVER OXYGEN MASK HOUSING LIGHT. TOP RIGHT CORNER OF MASK HOUSING LIGHT STRIP IS MELTED. (FLIGHT 4761) UPON ARRIVAL FOUND OBSERVERS CREW MEMBER O2 MASK FL
- [SDR SWIA2026031875521](https://openairdocs.org/sdr/SWIA2026031875521.md): Light · smoke · Mar 17, 2026 · N945SW · Cndair CL6002B19 · Crew Oxygen System
  > HEARD A POP AND FAINT SMELL OF SMOKE (PLASTIC) ON CLIMBOUT FOR A COUPLE SECONDS. APPEARS TO BE THE OBSERVER OXYGEN MASK HOUSING LIGHT. TOP RIGHT CORNER OF MASK HOUSING LIGHT STRIP IS MELTED. OPEN
- [SDR SWIA2025081800011](https://openairdocs.org/sdr/SWIA2025081800011.md): Skin · corroded · Aug 11, 2025 · N945SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > CORROSION ON THE EXTERIOR BELLY SKIN BETWEEN FS 559.00+80 AND FS 559.00+112 AND STR 26L - 26R. (C-CHECK RO 08/16/2025)COMPLIED WITH REO 601R-53-51-716 DATED: 2025-08-14 PERMANENT DISPOSITION FOR BLENDED CORROSION DAMAGE ON FUSELAGE SKIN PANEL BETWEEN FS559.
- [SDR SWI2025F01089](https://openairdocs.org/sdr/SWI2025F01089.md): Bushing · damaged · Jul 31, 2025 · N945SW · Cndair CL6002B19 · Wing, Control Surface Attach Fittings
  > REMOVED THE RH AILERON #3 HINGE ASSEMBLY TO F.O.M. (C-CHECK RO 08/16/2025)COMPLIED WITH REO 601R-57-51-015 REV: NC DATED: AUG-09-1995 AND REO 601R-27-15-001 REV: A DATED: 09-08-95 BY REAMING AND INSTALLING OVERSIZED BUSHINGS AT THE WING TRAILING EDGE RH AILER
- [SDR SWIA2025081800731](https://openairdocs.org/sdr/SWIA2025081800731.md): Hinge Fitting · damaged · Jul 31, 2025 · N945SW · Cndair CL6002B19 · Wing, Control Surface Attach Fittings
  > REMOVED THE RH AILERON #2 HINGE ASSEMBLY TO F.O.M. (C-CHECK RO 08/16/2025)COMPLIED WITH REO 601R-57-51-015 REV: NC DATED: AUG-09-1995 AND REO 601R-27-15-001 REV: A DATED: 09-08-95 BY REAMING AND INSTALLING OVERSIZED BUSHINGS AT THE WING TRAILING EDGE RH AI
- [SDR SWIA2025081800703](https://openairdocs.org/sdr/SWIA2025081800703.md): Angle · damaged · Jul 3, 2025 · N945SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > REMOVED TWO FASTENERS ON RH PRESSURE FLOOR SILL ANGLE AT FS513.00 AND BETWEEN RBL42.4 - RBL36.0 TO FOM (C-CHECK RO 08/16/2025)COMPLIED WITH REO 601R-53-41-3333 REV-A DATED 2025-07-16 DISPOSITION FOR ALTERNATE FASTENER INSTALLATION TO RH PRESSURE SILL FLOOR A
- [SDR SWI2025F00854](https://openairdocs.org/sdr/SWI2025F00854.md): Floor Support · damaged · Jul 3, 2025 · N945SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > REMOVED TWO FASTENERS ON RH PRESSURE FLOOR SILL ANGLE AT FS513.00 AND BETWEEN RBL42.4 - RBL36.0 TO FOM (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA2025081800612](https://openairdocs.org/sdr/SWIA2025081800612.md): Skin · damaged · Jun 12, 2025 · N945SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > OVERSIZED HOLE TO FUSELAGE LOWER SKIN PANEL AT FS589.00 AT STR27 (C-CHECK RO 08/16/2025)COMPLIED WITH REO 601R-53-61-8343 REV--A DATED 2025-06-13 FOR OVERSIZED HOLE TO FUSELAGE LOWER SKIN PANEL AT FS589.00 AT STR27. PERFORMED EDDY CURRENT INSPECTION WITH REFE
- [SDR SWIA2025081800060](https://openairdocs.org/sdr/SWIA2025081800060.md): Structure · corroded · Jun 11, 2025 · N945SW · Cndair CL6002B19 · Fuselage Structure (General)
  > 1 AREA OF CORROSION BEYOND ALLOWABLE LIMITS AS PER GREO 601R-53-41-666 REV -C DATED 2012-11-06 JUST FWD OF FS 559.00 AT LBL 42.5 APPROXIMATELY (C-CHECK RO 08/16/2025)COMPLIED WITH REO 601R-53-41-3325 REV- DATED 2025-06-21 REPAIR TO PRESSURE FLOOR SILL BETWEE
- [SDR SWIA2025081800611](https://openairdocs.org/sdr/SWIA2025081800611.md): Structure · corroded · Jun 11, 2025 · N945SW · Cndair CL6002B19 · Fuselage Structure (General)
  > 4 AREAS OF CORROSION BEYOND ALLOWABLE LIMITS AS PER GREO 601R-53-41-666 REV -C DATED 2012-11-06 BETWEEN FS449.85 AND FS529.00 AT APPROXIMATLY RBL 43.0 (C-CHECK RO 08/16/2025)COMPLIED WITH REO 601R-53-41-3322 REV "--" DATED 2025-07-04 FOR 4 AREAS OF CORROSIO
- [SDR SWIA2025081800605](https://openairdocs.org/sdr/SWIA2025081800605.md): Frame · cracked · Jun 5, 2025 · N945SW · Cndair CL6002B19 · Fuselage Main, Frame
  > DURING CORROSION REMOVAL ON FRAME FS 605.00, FOUND A.200€? CRACK ON THE FWD ANGLE ON STR 19R EMANATING FROM A RIVET HOLE TO THE END OF THE ANGLE. (C-CHECK RO 08/16/2025)COMPLIED WITH REO 601R-53-61-8339 DATED: 2025-06-12 REV -- REPAIR FOR CRACK DAMAGE TO FRA
- [SDR SWIA2025060600005](https://openairdocs.org/sdr/SWIA2025060600005.md): Frame · cracked · Jun 5, 2025 · N945SW · Cndair CL6002B19 · Fuselage Main, Frame
  > DURING CORROSION REMOVAL ON FRAME FS 605.00, FOUND A.200€? CRACK ON THE FWD ANGLE ON STR 19R EMANATING FROM A RIVET HOLE TO THE END OF THE ANGLE. (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA2025081800604](https://openairdocs.org/sdr/SWIA2025081800604.md): Tie Down · cracked · Jun 4, 2025 · N945SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO NET CENTER TIE DOWN RING PLATE (REF SRM 53-61-43 ITEM 77) CRACKED. (C-CHECK RO 08/16/2025)REMOVED AND REPLACED THE CARGO NET CENTER TIE DOWN RING PLATE IN REFERENCE WITH THE CRJ-200 SRM 51-42-21, SRM 51-42-06 AND SRM 53-61-43. COMPLIED WITH TASK CARD 5
- [SDR SWIA202506500004](https://openairdocs.org/sdr/SWIA202506500004.md): Plate · cracked · Jun 4, 2025 · N945SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CARGO NET CENTER TIE DOWN RING PLATE (REF SRM 53-61-43 ITEM 77) CRACKED. (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA2025081800530](https://openairdocs.org/sdr/SWIA2025081800530.md): Floorbeam · cracked · May 30, 2025 · N945SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CRACKED CLIP IN FLOOR BEAM WEB AT PILOT'S BULKHEAD FS 280.00, LBL 9.0, WL 73.10 (C-CHECK RO 08/16/2025)REMOVED AND REPLACED THE CLIP IN FLOOR BEAM WEB AT PILOT'S BULKHEAD FS 280.00, LBL 9.0, WL 73.10 IN REFERENCE WITH THE CRJ-200 SRM 51-42-21, REO 601R-53-11-
- [SDR SWIA2025081800529](https://openairdocs.org/sdr/SWIA2025081800529.md): Strap · corroded · May 29, 2025 · N945SW · Cndair CL6002B19 · Fuselage Main, Structure
  > PRESSURE FLOOR AFT STRAP BETWEEN RBL27.50 AND RBL36.20 AT FS559.00 HAS SURFACE CORROSION. (C-CHECK RO 08/16/2025)PRESSURE FLOOR AFT STRAP BETWEEN RBL27.50 AND RBL36.20 AT FS559.00 REPLACED IN REFERENCE TO SRM 51-42-06. COMPETED CORROSION FINDINGS REPORT. C
- [SDR SWI2025F01088](https://openairdocs.org/sdr/SWI2025F01088.md): Pressure Deck · corroded · May 29, 2025 · N945SW · Cndair CL6002B19 · Fuselage Main, Structure
  > MULTIPLE AREAS OF CORROSION ON LH PRESSURE FLOOR SILL BETWEEN FS409.00+128 AND 559.00. (C-CHECK RO 08/16/2025)REFERENCE CP 30297365 FOR REPAIR OF AREA BEYOND LIMITS JUST FWD OF FS 559.00 AT LBL 42.5 APPROXIMATELY. BLENDED ALL OTHER AREAS OF CORROSION ON LH
- [SDR SWI2025F01087](https://openairdocs.org/sdr/SWI2025F01087.md): Pressure Deck · corroded · May 29, 2025 · N945SW · Cndair CL6002B19 · Fuselage Main, Structure
  > MULTIPLE AREAS OF CORROSION ON RH PRESSURE FLOOR SILL BETWEEN FS409.00+128 AND 559.00. (C-CHECK RO 08/16/2025)REFERENCE CP 30297321 FOR REPAIRS OF AREAS BEYOND LIMITS BETWEEN FS449.85 AND FS529.00 AT APPROXIMATLY RBL 43.0. BLENDED ALL OTHER AREAS OF CORROS
- [SDR SWIA2025081800521](https://openairdocs.org/sdr/SWIA2025081800521.md): Angle · cracked · May 21, 2025 · N945SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH INTERCOSTAL CLIP, AFT OF REAR PRESSURE BULKHEAD AT STGR 14R CRACKED (C-CHECK RO 08/16/2025)REMOVED AND REPLACED RH INTERCOSTAL CLIP, AFT OF REAR PRESSURE BULKHEAD AT STGR 14R WITH REFERENCE TO SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPL
- [SDR SWIA2025052200021](https://openairdocs.org/sdr/SWIA2025052200021.md): Angle · cracked · May 21, 2025 · N945SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH INTERCOSTAL CLIP, AFT OF REAR PRESSURE BULKHEAD AT STGR 14R CRACKED (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA2025081800513](https://openairdocs.org/sdr/SWIA2025081800513.md): A/C Pack · cracked · May 13, 2025 · N945SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR CAM TRACK SUPPORT ASSY LOWER CHANNEL AT FS574.00 AND STR 16L HAS CRACK AROUND SECOND MOST OUTBOARD LOWER RIVET HEAD (C-CHECK RO 08/16/2025)REPLACED CARGO DOOR CAM TRACK SUPPORT ASSY LOWER CHANNEL AT FS574.00 AND STR 16L IN REFERENCE TO SRM 51-42-21
- [SDR SWIA202505140013](https://openairdocs.org/sdr/SWIA202505140013.md): Track · cracked · May 13, 2025 · N945SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR CAM TRACK SUPPORT ASSY LOWER CHANNEL AT FS574.00 AND STR 16L HAS CRACK AROUND SECOND MOST OUTBOARD LOWER RIVET HEAD (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA2025081800210](https://openairdocs.org/sdr/SWIA2025081800210.md): Angle · cracked · Feb 10, 2025 · N945SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA67693-601R-53-61-1550 945SW MXCODEID55290-PR - LH INTERCOSTAL CLIP, AFT OF REAR PRESSURE BULKHEAD AT STGR 14L, CRACKED. COMPLIED WITH TEMPORARY REPAIR PER REO 601R-53-61-1550 REV -B DATED 2010-11-01. PERMANENT REPAIR
- [SDR SWIA202405020001](https://openairdocs.org/sdr/SWIA202405020001.md): Warning Message · illuminated · May 1, 2024 · N945SW · Cndair CL6002B19 · Windshield/Door Rain/Ice Removal
  > L WSHLD HEAT MESSAGE (FILED CLOSED)REMOVED AND REPLACED LH WINDSHIELD IAW AMM 56-11-01 AND TASK CARD 56-220-1000-SKY COCKPIT WINDSHIELD AND SIDE WINDOW INSTALLATION. VERIFIED NO SMOKE PRESENT FROM LH WINDSHIELD POWER TERMINALS WITH AIRCRAFT PRESSURIZED AT 2.4
- [SDR SWIA202264773](https://openairdocs.org/sdr/SWIA202264773.md): None · overheated · Mar 5, 2022 · N945SW · Cndair CL6002B19 · Ice/Rain Protection System
  > WING OVHT WARNING ON DESCENT IN DRO (FLIGHT 5301 - FILED CLOSED) PERFORMED OPS CHECK OF WING ANTI ICE PER CRJ-200 AMM 30-12-00-710-803. DURING OPS CHECK NOTED THAT LH WING OVHT MESSAGE ON A/ICE PAGE WOULD INTERMITTENTLY COME ON. PERFORMED CROSS BLEED FROM
- [SDR SWIA202263753](https://openairdocs.org/sdr/SWIA202263753.md): None · leaking · Jan 10, 2022 · N945SW · Cndair CL6002B19 · Hydraulic Pressure Sensor
  > ON CLIMB OUT FROM FAR, GOT 'HYD 3 LO PRESS' CAUTION MESSAGE & HYD SYS 3 INDICATED '0' PSI. CREW C/W QRH PROCEDURE, DIVERTED TO MSP, PERFORMED MANUAL GEAR EXTENSION, DECLARED EMERGENCY & LANDED WITHOUT INCIDENT & NOT OVERWEIGHT. CREW NOTED HYD SYS 3 QTY INDIC
- [SDR SWIA202161779](https://openairdocs.org/sdr/SWIA202161779.md): None · cracked · Oct 15, 2021 · N945SW · Cndair CL6002B19 · Window/Windshield System
  > CRACK IN UPPER LEFT CORNER OF CAPTAINS FORWARD WINDSHIELD. (FLIGHT 5045 - FILED CLOSED) REMOVED AND REPLACED CAPTAIN SIDE FORWARD WINDSHIELD REF TO AMM 56-11-01. OPS CHECKED NORMAL AT THIS TIME / CW TASK CARD FOR WINDSHIELD REPLACEMENT 56-220-1000-SKY
- [SDR SWIA2021080560053](https://openairdocs.org/sdr/SWIA2021080560053.md): Hinge Fitting · damaged · Jul 7, 2021 · N945SW · Cndair CL6002B19 · Ailerons
  > LH AILERON WING TRAILING CENTER HINGE FITTING LUGS AT WS319.604 AND 323.038 REQUIRE REAMING FOR OVER SIZED BUSHING INSTALLATION (C-CHECK RO 8/1/2021) REAMED AND INSTALLED OVERSIZED BUSHING AT LH AILERON WING TRAILING CENTER HINGE FITTING LUGS AT WS319.
- [SDR SWIA2021080560104](https://openairdocs.org/sdr/SWIA2021080560104.md): Bolt · corroded · Jun 19, 2021 · N945SW · Cndair CL6002B19 · Aerodynamic Fairings
  > *CORRODED HARDWARE FOR AFT FAIRING BRKT ASSY AT APPROX. FS890.00 (MARKED) AFT OF ANTI-ROTATION FITTING FOR H-STAB (C-CHECK RO 8/1/2021) REMOVED AND REPLACE WITH NEW QTY3 BOLTS WITH HARDWARE APPROX FS890.00 AFT OF ANTI-ROTATION FITTING H-STAB. REF. CRJ2
- [SDR SWIA2021080560103](https://openairdocs.org/sdr/SWIA2021080560103.md): Bolt · corroded · Jun 19, 2021 · N945SW · Cndair CL6002B19 · Trailing Edge Flaps
  > *L/H OTBD FLAP INBD SEAL HARDWARE IS CORRODED (MARKED) (C-CHECK RO 8/1/2021) REMOVED AND REPLACED L/H OTBD FLAP INBD SEAL HARDWARE WITH NEW REF CRJ 200 AMM 57-53-10-400- 801. SEE CONTINUE CARD FOR DETAILS
- [SDR SWIA2021080560102](https://openairdocs.org/sdr/SWIA2021080560102.md): Bolt · corroded · Jun 19, 2021 · N945SW · Cndair CL6002B19 · Trailing Edge Flaps
  > *L/H OTBD FLAP OTBD SEAL HARDWARE IS CORRODED (MARKED) (C-CHECK RO 8/1/2021) REMOVED AND REPLACED WITH NEW 7EA BOLTS ON L/H OTBD FLAP OTBD SEAL REF CRJ 200 SRM 51-41-02
- [SDR SWIA2021080560052](https://openairdocs.org/sdr/SWIA2021080560052.md): Doubler · corroded · Jun 12, 2021 · N945SW · Cndair CL6002B19 · Passenger/Crew Doors
  > *PASSENGER DOOR INTERNAL STRUCTURE €“ FRAME DOUBLER AT APPROXIMATELY FS320 BETWEEN DD7 AND HINGE END OF DOOR HAS CORROSION. (C-CHECK RO 8/1/2021) REMOVED AND REPLACED WITH NEW FORMER P/N 601R318038-3 AT FS320.00 BETWEEN DD5 AND HINGE ON LOWER PAX DOOR.
- [SDR SWIA2021080560051](https://openairdocs.org/sdr/SWIA2021080560051.md): Angle · corroded · Jun 12, 2021 · N945SW · Cndair CL6002B19 · Passenger/Crew Doors
  > *PASSENGER DOOR INTERNAL STRUCTURE €“ CLIP ON AT FS320 ON HINGE END OF DOOR HAS CORROSION (C-CHECK RO 8/1/2021) INSTALLED NEW CLIPS ON FS 320.00 OF PAX DOOR P/N 601R319034-2-01 REF CRJ 200 SRM 51-42-06 AND DWG 601R31702 REV -N. COMPLIED WITH 51-900-10
- [SDR SWIA2021080560050](https://openairdocs.org/sdr/SWIA2021080560050.md): Nut Plate · corroded · Jun 11, 2021 · N945SW · Cndair CL6002B19 · Emergency Exits
  > *LH EMERGENCY EXIT DOOR €“ FORWARD FITTING ON BOTTOM OF DOOR HAS 4 EACH RUSTY NUTPLATES. (C-CHECK RO 8/1/2021) REMOVED AND INSTALLED FWD ATTACH BRACKET COMMON TO STOP FITTING ON LH EMERGENCY DOOR. REF CRJ 200 SRM 51-42-06 AND DWG 601R31123 REV H. COMP
- [SDR SWIA2021080560049](https://openairdocs.org/sdr/SWIA2021080560049.md): Nut Plate · corroded · Jun 11, 2021 · N945SW · Cndair CL6002B19 · Fuselage Main, Structure
  > *LH EMERGENCY EXIT DOOR €“ CORROSION AT NUTPLATE LOCATION FOR AFT FITTING ON BOTTOM OF DOOR AND 4 EACH RUSTY NUTPLATES. (C-CHECK RO 8/1/2021) REMOVED CORRODED AFT ATTACH BRACKET ON INNER SURFACE OF LH EMERGENCY DOOR COMMON TO FITTING NUTPLATES. REF CRJ
- [SDR SWIA2021080560048](https://openairdocs.org/sdr/SWIA2021080560048.md): Window Post · cracked · Jun 8, 2021 · N945SW · Cndair CL6002B19 · Fuselage Main, Structure
  > * THE COCKPIT WINDSHIELD CENTER POST'S LOWER LH FITTING HAS A SUSPECTED CRACK BETWEEN THE 2 AFT BOTTOM FASTENERS. (MARKED WITH BLACK ARROW) (C-CHECK RO 8/1/2021) REPLACED CRACKED COCKPIT WINDSHIELD CENTER POST LOWER LH FITTING WITH A NEW PART (P/N 601R3
- [SDR SWIA2021080560047](https://openairdocs.org/sdr/SWIA2021080560047.md): Window Post · cracked · Jun 8, 2021 · N945SW · Cndair CL6002B19 · Fuselage Main, Structure
  > * THE COCKPIT WINDSHIELD CENTER POST'S LOWER RH FITTING IS CRACKED. (C-CHECK RO 8/1/2021) REPLACED CRACKED COCKPIT WINDSHIELD CENTER POST LOWER RH FITTING WITH A NEW PART (P/N 601R33237-2), DRILLED, LOCATED AND INSTALLED REF CRJ-200 SRM 51-42-21, 51-40-
- [SDR SWIA2021080560101](https://openairdocs.org/sdr/SWIA2021080560101.md): Drag Angle · corroded · Jun 7, 2021 · N945SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FWD DRAG ANGLE HAS MULITPLE SPOTS OF CORROSION ON BOTTOM SIDE (C-CHECK RO 8/1/2021) REMOVED AN REPLACED WITH NEW DRAG ANGLE REF CRJ200 SRM 51-42-10
- [SDR SWIA2021080560100](https://openairdocs.org/sdr/SWIA2021080560100.md): Web · corroded · Jun 7, 2021 · N945SW · Cndair CL6002B19 · Passenger/Crew Doors
  > MULTIPLE SPOTS OF CORROSION FOUND ON FWD PAX DOOR WEB (C-CHECK RO 8/1/2021) REMOVED AND REPLACED WITH NEW PAX DOOR WEB P/N 601R317071-12S REF CRJ200 SRM 51-42-06. SEE CONTINUE CARD FOR DETAILS.
- [SDR SWIA2021080560099](https://openairdocs.org/sdr/SWIA2021080560099.md): Web · corroded · Jun 7, 2021 · N945SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT WEB HAS SURFACE CORROSION ON UPPER STEP (C-CHECK RO 8/1/2021) REMOVED AND REPLACED NEW PAX DOOR AFT WEB P/N 601R317071-11S REF CRJ200 SRM 51-42-06. SEE CONTINUE CARD FOR DETAILS.
- [SDR SWIA2021080560083](https://openairdocs.org/sdr/SWIA2021080560083.md): Intercostal · corroded · Jun 7, 2021 · N945SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON DD3 INTERCOSTAL BETWEEN FS 320.10 AND FS 338.00 (C-CHECK RO 8/1/2021) REPLACED DD3 INTERCOSTAL BETWEEN FS 320.10 AND FS 338.00 DWG 601R31702 REV N, CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21. COMPLIED WITH 51-900-1003-SKY AND PRE
- [SDR SWIA2021080560046](https://openairdocs.org/sdr/SWIA2021080560046.md): Fitting · chafed · Jun 7, 2021 · N945SW · Cndair CL6002B19 · Trailing Edge Flaps
  > * THE RH WING, OUTBOARD FLAP'S NOSE RIB FITTING AT APPROX. FLS 235, HAS CHAFING ON ITS INTERNAL INBOARD SURFACE IN MULTIPLE SPOTS. (MARKED WITH RED GREASE PENCIL) (C-CHECK RO 8/1/2021) REPAIRED R/H WING OUTBOARD FLAP NOSE RIB FITTING AT APPROX FLS 235
- [SDR SWIA2021080560045](https://openairdocs.org/sdr/SWIA2021080560045.md): Attach Fitting · galled · Jun 7, 2021 · N945SW · Cndair CL6002B19 · Trailing Edge Flaps
  > * THE LH WING, OUTBOARD FLAP'S VANE ATTACH FITTINGS HAVE GALLING AND CHAFING PRESENT ON THEIR LOWER SURFACES AT THE FOLLOWING APPROX. LOCATIONS: FLS 171, FLS 189, FLS 235, FLS 280, AND FLS 296. (C-CHECK RO 8/1/2021) REMOVED GALLING REF REO 601R-57-53-19
- [SDR SWIA2021080560044](https://openairdocs.org/sdr/SWIA2021080560044.md): Attach Fitting · chafed · Jun 7, 2021 · N945SW · Cndair CL6002B19 · Trailing Edge Flaps
  > * THE LH WING OUTBOARD FLAP, INBOARD HINGE BOX'S AFT ATTACH FITTING IS CHAFED ON THE CENTER 2 LUGS. (C-CHECK RO 8/1/2021) REPAIRED L/H WING OUTBOARD FLAP INBOARD HINGE BOX AFT ATTACH FITTINGS REF REO 601R-57-21-3497 REV.-- DATED 2021-06-29. COMPLIED
- [SDR SWIA2021080560043](https://openairdocs.org/sdr/SWIA2021080560043.md): Attach Fitting · chafed · Jun 7, 2021 · N945SW · Cndair CL6002B19 · Trailing Edge Flaps
  > * THE LH WING OUTBOARD FLAP, CENTER HINGE BOX'S AFT ATTACH FITTING IS CHAFED ON THE CENTER 2 LUGS. (C-CHECK RO 8/1/2021) REPAIRED L/H WING OUTBOARD FLAP CENTER HINGE BOX AFT ATTACH FITTING REO 601R-57-21-3497 REV.-- DATED 2021-06-29. COMPLIED WITH 51-9
- [SDR SWIA2021080560042](https://openairdocs.org/sdr/SWIA2021080560042.md): Attach Fitting · chafed · Jun 7, 2021 · N945SW · Cndair CL6002B19 · Trailing Edge Flaps
  > * THE LH WING OUTBOARD FLAP, OUTBOARD HINGE BOX'S AFT ATTACH FITTING IS CHAFED ON THE CENTER 2 LUGS. (C-CHECK RO 8/1/2021) REPAIRED L/H WING OUTBOARD FLAP OUTBOARD HINGE BOX AFT ATTACH FITTING REF REO 601R-57-21-3497 REV.-- DATED 2021-06-29. COMPLIED W
- [SDR SWIA2021080560106](https://openairdocs.org/sdr/SWIA2021080560106.md): Cotter Pin · missing · Jun 6, 2021 · N945SW · Cndair CL6002B19 · Horizontal Stabilizer Structure
  > AFTER PERFORMING A GVI OF THE HORIZONTAL STABILIZER STEADY FITTING FOR THE PRESENCE OF LOOSE/DAMAGED ATTACHING HARDWARE. FOUND THE FOUR UPPER BOLTS ARE MISSING COTTER PINS. (C-CHECK RO 8/1/2021) INSTALLED 4 NEW COTTOR PINS HORIZONTAL STABILIZER STEADY
- [SDR SWIA2021080560082](https://openairdocs.org/sdr/SWIA2021080560082.md): Hinge Fitting · chafed · Jun 6, 2021 · N945SW · Cndair CL6002B19 · Horizontal Stabilizer Structure
  > * THE HORIZONTAL STABILIZER'S RH OUTBOARD HINGE FITTING, FOR THE RH ELEVATOR, IS CHAFED ON ITS BOTTOM SIDE. (C-CHECK RO 8/1/2021) REPAIRED R/H HORIZONTAL STABILIZER OUTBOARD HINGE FITTING REF REO 601R-55-11-689 REV -- DATED 2021-06-21. SEE CONTINUATIO
- [SDR SWIA2021080560081](https://openairdocs.org/sdr/SWIA2021080560081.md): Hinge Fitting · chafed · Jun 6, 2021 · N945SW · Cndair CL6002B19 · Horizontal Stabilizer Structure
  > * THE HORIZONTAL STABILIZER'S RH CENTER HINGE FITTING, FOR THE RH ELEVATOR, IS CHAFED ON ITS INBOARD PLATE. (C-CHECK RO 8/1/2021) REPIARED HORIZONTAL STABILIZER R/H CENTER HINGE FITTING FOR THE R/H ELEVATOR REF REO 601R-55-11-061 REV D DATED 2020-10-

Next page: https://openairdocs.org/aircraft/N945SW/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 = 'N945SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N945SW/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.