# Service difficulty reports: N947SW

A list on [N947SW](https://openairdocs.org/aircraft/N947SW.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 · 209 reports

- [SDR SWI2025F01792](https://openairdocs.org/sdr/SWI2025F01792.md): Pdu · faulted · Dec 2, 2025 · N947SW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL CAUTION MESSAGE ON APPROACH WHEN SELECTING FLAPS 20 TO 30. RAN QRH & FLAPS STAYED IN FLAPS 20 DETENT AFTER RESELECTING FLAPS 20 FROM FLAPS 30 DETENT IAW PROCEDURE. (FLIGHT 4808) REF CP 31297248 & CP 31297331 FOR TROUBLESHOOTING. REF CP 31297272 FO
- [SDR SWI2025F01711](https://openairdocs.org/sdr/SWI2025F01711.md): Warning Message · illuminated · Dec 2, 2025 · N947SW · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLAPS FAIL CAUTION MESSAGE ON APPROACH WHEN SELECTING FLAPS 20 TO 30. RAN QRH AND FLAPS STAYED IN THE FLAPS 20 DETENT AFTER RESELECTING FLAPS 20 FROM THE FLAPS 30 DETENT PER PROCEDURE. (FLIGHT 4808)
- [SDR SWIA202508110010](https://openairdocs.org/sdr/SWIA202508110010.md): Bracket · cracked · Aug 10, 2025 · N947SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > FWD CARGO DOOR TRACK LOWER BRACKET CRACKED. (FILED CLOSED)REMOVED AND REPLACED CARGO DOOR FWD TRACK LOWER MOUNT BRACKET IN REFERENCE TO SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337.
- [SDR SWIA2025011000001](https://openairdocs.org/sdr/SWIA2025011000001.md): Smoke Warning · activated · Jan 1, 2025 · N947SW · Cndair CL6002B19 · Detection System
  > CLIMBING PAST 14000€™ SMOKE TOILET CAUTION MESSAGE ALONG WITH SMOKE DETECTOR IN LAV. BOTH CA AND FO VERIFIED LIGHT WHITE SMOKE IN CABIN. UPON LANDING NO EVIDENCE OF FIRE BY GROUND PERSONNEL. (FLIGHT 5199 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED
- [SDR SWIA20250102002](https://openairdocs.org/sdr/SWIA20250102002.md): Lavatory · smoke · Jan 1, 2025 · N947SW · Cndair CL6002B19 · Smoke Detection
  > CLIMBING PAST 14000€™ SMOKE TOILET CAUTION MESSAGE ALONG WITH SMOKE DETECTOR IN LAV. BOTH CA AND FO VERIFIED LIGHT WHITE SMOKE IN CABIN. UPON LANDING NO EVIDENCE OF FIRE BY GROUND PERSONNEL. CURRENTLY A WORK IN PROGRESS
- [SDR SWIA2024010301230](https://openairdocs.org/sdr/SWIA2024010301230.md): Acm · smoke · Dec 30, 2024 · N947SW · Cndair CL6002B19 · Cabin Cooling System
  > SMOKE TOILET AT FL310 ON DECENT GOT OXY PRESS LOW?. PACK 1 WAS SHOWING 120 DEGREES C. WAS EXCESSIVELY HOT AND SMOKE IN PLANE / CABIN. (FLIGHT 4644 - FILED CLOSED) REFER TO AML1503487 FOR THE SERVICING OF THE CREW O2 SYSTEM ( MASKS WERE DAWNED DURING SMOKE
- [SDR SWIA2024123101](https://openairdocs.org/sdr/SWIA2024123101.md): A/C Pack · smoke · Dec 30, 2024 · N947SW · Cndair CL6002B19 · Detection System
  > €ŒSMOKE TOILET€? AT FL310 ON DECENT GOT €ŒOXY PRESS LOW€?. PACK 1 WAS SHOWING 120 DEGREES C. WAS EXCESSIVELY HOT AND SMOKE IN PLANE / CABIN. (FLIGHT 4644 - FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA2024080700003](https://openairdocs.org/sdr/SWIA2024080700003.md): Carbon Seal · leaking · Aug 3, 2024 · N947SW · Cndair CL6002B19 · Turbine Engine Oil System
  > L ENG OIL PRESS WARNING IN FLIGHT. INTERMITTENT AT CLIMB OUT AND CRUISE. COMPLIED WITH QRH. PRESSURE INDICATED BETWEEN 28-35PSI INITIALLY. BEGAN TO DECREASE ON DESCENT AND WARNING BECAME PERSISTENT. FOLLOWED QRH AND SHUT L ENG DOWN. (FLIGHT 5801 - FILED CLOSED
- [SDR SWIA2024080500003](https://openairdocs.org/sdr/SWIA2024080500003.md): Oil System · warning message · Aug 3, 2024 · N947SW · Cndair CL6002B19 · Engine Oil Pressure
  > L ENG OIL PRESS WARNING IN FLIGHT. INTERMITTENT AT CLIMB OUT AND CRUISE. COMPLIED WITH QRH. PRESSURE INDICATED BETWEEN 28-35PSI INITIALLY. BEGAN TO DECREASE ON DESCENT AND WARNING BECAME PERSISTENT. FOLLOWED QRH AND SHUT L ENG DOWN. (FLIGHT 5801 - FILE OPEN)
- [SDR SWIA202403190005](https://openairdocs.org/sdr/SWIA202403190005.md): Door Frame · corroded · Mar 5, 2024 · N947SW · Cndair CL6002B19 · Fuselage Main, Structure
  > PASSENGER DOOR CUT OUT FRAME AT APPROXIMATELY FS 310 BETWEEN STGR 11L AND 12L CORRODED AS MARKED (C-CHECK RO 3/19/2024) REMOVED NOTED CORROSION FROM PASSENGER DOOR CUT OUT FRAME AT APPROXIMATELY FS 310.00 BETWEEN STGR 11L AND 12L, NDT INSPECTED NO DEFECTS
- [SDR SWIA20240319219](https://openairdocs.org/sdr/SWIA20240319219.md): Floorbeam · cracked · Feb 19, 2024 · N947SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280.00 OUTBD RBL9 FLOOR BEAM CLIP CRACKED (C-CHECK RO 3/19/2024) REMOVED NOTED FS 280.00 OUTBD RBL9 FLOOR BEAM CRACKED CLIP AND INSTALLED REPAIR CLIP REF CRJ 200 SRM 51-42-21 REF BOMBARDIER DWG# 601R31113 REV-AD W/OUT JOGGLE PER BOMBARDIER REO 601R-53-1
- [SDR SWI202403190240](https://openairdocs.org/sdr/SWI202403190240.md): Angle · cracked · Feb 9, 2024 · N947SW · Cndair CL6002B19 · Fuselage Main, Structure
  > RIGHT COCKPIT WINDOW POST LOWER AFT ANGLE IS CRACKED. (MARKED) (C-CHECK RO 3/19/2024) REMOVED CRACKED RIGHT COCKPIT WINDOW POST LOWER AFT ANGLE AND INSTALLED NEW RIGHT COCKPIT WINDOW POST LOWER AFT ANGLE P/N: 601R33235-4S WITH NEW 4EA HI-LOK AND NUT. REF.
- [SDR SWIA20240319209](https://openairdocs.org/sdr/SWIA20240319209.md): Angle · cracked · Feb 9, 2024 · N947SW · Cndair CL6002B19 · Fuselage Main, Structure
  > LEFT COCKPIT WINDOW POST LOWER AFT ANGLE IS CRACKED. (MARKED) (C-CHECK RO 3/19/2024) REMOVED AND REPLACED L/H COCKPIT WINDOW POST LOWER AFT ANGLE P/N 601R33235-3 REF. CRJ-200 SRM 51-42-21 AND BOMBARDIER DWG# 601R33007 REV -U
- [SDR SWIA20240319205](https://openairdocs.org/sdr/SWIA20240319205.md): Hinge · worn · Feb 5, 2024 · N947SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > PASSENGER DOOR PIANO HINGE HALF ON FUSELAGE HAS WARE BETWEEN LUGS (C-CHECK RO 3/19/2024) REMOVED AND REPLACED HINGE WITH NEW ONE P/N-600-35129-15. REF:CRJ-200 S.R.M.53-21-23. C/W 51-900-1003-SKY. LEAK CHECK GOOD.
- [SDR SWI202403190239](https://openairdocs.org/sdr/SWI202403190239.md): Intercostal · cracked · Feb 3, 2024 · N947SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACK IN INTERCOSTAL 601-35012-51 IN AFT EQUIPMENT BAY BETWEEN FS 621.00 - 625.00, STGR 15L (C-CHECK RO 3/19/2024) REMOVED AND REPLACED INTERCOSTAL CLIP P/N: 601-35012-51 IN AFT EQUIPMENT BAY BETWEEN FS 621.00 - 625.00, STGR 14L. REF. CRJ 200 SRM 51-42-21
- [SDR SWI202403190238](https://openairdocs.org/sdr/SWI202403190238.md): Intercostal · cracked · Feb 3, 2024 · N947SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACK IN INTERCOSTAL 601-35012-52 IN AFT EQUIPMENT BAY BETWEEN FS 621.00 - 625.00, STGR 15R (C-CHECK RO 3/19/2024) REMOVED AND REPLACED INTERCOSTAL CLIP P/N: 601-35012-52 IN AFT EQUIPMENT BAY BETWEEN FS 621.00 - 625.00, STGR 14R. REF. CRJ 200 SRM 51-42-21
- [SDR SWI202403190237](https://openairdocs.org/sdr/SWI202403190237.md): Window Frame · cracked · Feb 3, 2024 · N947SW · Cndair CL6002B19 · Fuselage Main, Structure
  > RIGHT WINDSHIELD SIDE POST SUPPORT STRUCTURE HAS A CRACK, BELOW THE POST. (MARKED & FLAGGED) (C-CHECK RO 3/19/2024) REPLACED SUPPORT BRACKET PER BOMBARDIER DRAWING 601R34032 (REV P) -AND- CRJ200SRM 51-40-06 & SRM 51-42-06.COMPLETED SKYWEST TASK CARD 51-90
- [SDR SWI202403190236](https://openairdocs.org/sdr/SWI202403190236.md): Window Frame · cracked · Feb 3, 2024 · N947SW · Cndair CL6002B19 · Fuselage Main, Structure
  > LEFT WINDSHIELD SIDE POST SUPPORT STRUCTURE HAS A CRACK, BELOW THE POST. (MARKED & FLAGGED) (C-CHECK RO 3/19/2024) REMOVED CRACKED LEFT WINDSHIELD POST SUPPORT STRUCTURE AND INSTALLED NEW. REF. CRJ200 SRM 51-40-06, DWG NO. 601R34032 REV. P, & DWG NO. 601R
- [SDR SWIA20240319203](https://openairdocs.org/sdr/SWIA20240319203.md): Cam · gouged · Feb 3, 2024 · N947SW · Cndair CL6002B19 · Fuselage Main, Structure
  > PASSENGER DOOR FRAME FORWARD CAM GOUGED (C-CHECK RO 3/19/2024) REPLACED CAM FITTING & SHIM AT PAX DOOR FWD FS310 FRAME PER CRJ200 SRM 51-23-00 & SRM 51-42-21 & BOMBARDIER DWG 600-31900 REV K. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY AND SKYWEST FORM M-
- [SDR SWI2024031900235](https://openairdocs.org/sdr/SWI2024031900235.md): Floorbeam · cracked · Feb 2, 2024 · N947SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > SUSPECTED CRACK AT FS 280.00 LBL9 FLOOR BEAM CLIP AS MARKED MX TRANS 27765703 (C-CHECK RO 3/19/2024) REMOVED CRACKED FLOOR BEAM CLIP REF CRJ200 SRM 51-42-21.INSTALLED NEW REPLACEMENT AT FS280.00, I/B LBL9.00 REO 601R-53-11-171, REV -D, 13-FEB-08.COMPLIED
- [SDR SWIA2024031900202](https://openairdocs.org/sdr/SWIA2024031900202.md): Floor Support · corroded · Feb 2, 2024 · N947SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > EVIDENCE OF CORROSION FOUND ON L/H FLOOR SILL AT AFT CARGO DOOR CUT-OUT MULTIPLE LOCATIONS (C-CHECK RO 3/19/2024) REPLACED CARGO DOOR FLOOR SILL PER BOMBARDIER DRAWING 601R35011 (REV R) -AND- CRJ200SRM 51-42-06 (REVISION 39 DATED MAR 10/2021) -AND- CRJ200
- [SDR SWI202403190234](https://openairdocs.org/sdr/SWI202403190234.md): Skin · scratched · Feb 1, 2024 · N947SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > MULTIPLE AREAS OF SCRATCHES/GOUGING ON AFT CARGO DOOR EXTERNAL SKIN (C-CHECK RO 3/19/2024) REPAIRED / BLENDED MULTIPLE SCRATCHES / GOUGES ON AFT CARGO DOOR EXTERNAL SKIN REF REO REO-601R-52-31-416 REV -- DATE 2024-02-06. SEE CONTINUE FOR WORK PERFORMED C/W
- [SDR SWIA20240619201](https://openairdocs.org/sdr/SWIA20240619201.md): Rivet · loose · Feb 1, 2024 · N947SW · Cndair CL6002B19 · Trailing Edge Flaps
  > TWO AREAS OF SMOKING RIVETS ON LH OB FLAP UPPER SURFACE, APPRX 30 FASTNERS.( MARKED) (C-CHECK RO 3/19/2024) REPLACED NOTED SMOKING RIVETS ON LH OB FLAP UPPER SURFACE, APPROX. 30 FASTENERS REF MHIRJ REO--601R-57-53-1290 REV -- DATE 2024-02-03.COMPLIED WITH
- [SDR SWIA20240319204](https://openairdocs.org/sdr/SWIA20240319204.md): Skin · dented · Dec 4, 2023 · N947SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA82364-REO 601R-57-21-2702 MXCODEID65934-PR - DENT FOUND ON LT WING FWD LOWER PLANK BETWEEN WS65.75-WS85.50 AND BETWEEN STR 19-STR 20. PERMENANT REPAIR DUE WITHIN 2100 HOUR PER REO 601R-57-21-3702., PART NUMBER: -, S
- [SDR SWIA2023071400009](https://openairdocs.org/sdr/SWIA2023071400009.md): Unknown · unknown · Jul 9, 2023 · N947SW · Cndair CL6002B19 · Landing Gear Door Actuator
  > NOSE GEAR DIDN€™T COME UP DURING RETRACTION FOLLOWED BY A GEAR DISAGREE WARNING. FOLLOWED QRH AND LANDED. (FLT 5280 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 26868711 WITH THE FOLLOWING CORRECTIVE ACTION: "REF CP 26873100, REPLACEMENT OF NLG
- [SDR SWIA202307100009](https://openairdocs.org/sdr/SWIA202307100009.md): Unknown · unknown · Jul 9, 2023 · N947SW · Cndair CL6002B19 · Landing Gear Door Actuator
  > NOSE GEAR DIDN€™T COME UP DURING RETRACTION FOLLOWED BY A GEAR DISAGREE WARNING. FOLLOWED QRH AND LANDED. (FLT 5280 FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA2023013028001](https://openairdocs.org/sdr/SWIA2023013028001.md): Skin · dented · Jan 28, 2023 · N947SW · Cndair CL6002B19 · Wing, Plate/Skin
  > FOUND DENT DAMAGE TO WING FWD LOWER PLANK BTW WS65.75 €“ WS85.50 & BTW STR19 €“ STR20, LHS TO BE OUT OF LIMITS. COMPLIED WIH REO 601R-57-21-3702 DATED 2023-02-01 REV-. THIS IS A TEMPORARY DISPOSITION VALID FOR 2100 FLIGHT HOURS COMPLY WITH VISUAL REINSP
- [SDR SWIA202053761](https://openairdocs.org/sdr/SWIA202053761.md): Windshield · failed · Nov 3, 2020 · N947SW · Cndair CL6002B19 · Flight Compartment Windows
  > CAPT`S WINDSHIELD SHATTERED IN FLIGHT, RETURNED TO DEN, NO OVERWEIGHT LANDING. FLIGHT 5086-FILED CLOSED. REMOVED AND REPLACED CAPT`S WINDSHIELD, REFERENCE TASK CARD AND AMM. OPERATIONAL AND LEAK/PRESSURIZATION CHECKS GOOD. TORQUE WRENCH S/N 0711501055 CAL
- [SDR SWIA2020082151927](https://openairdocs.org/sdr/SWIA2020082151927.md): Bearing · worn · Jul 22, 2020 · N947SW · Cndair CL6002B19 · Elevator Structure
  > RH ELEVATOR #1, #2, & #3 HINGE POINT BEARINGS APPEAR WORN. (C-CHECK) RO 8/18/2020 REMOVED WORN BEARING & INSTALLED 1 EA. NEW BEARING P/N MS14102-6 IN HINGE FITTING ASSY. P/N 600-24043-1, REF. BOMBARDIER DWG, MPS & BAPS. SEE CONTINUE CARD FOR DETAILS.
- [SDR SWIA2020082151926](https://openairdocs.org/sdr/SWIA2020082151926.md): Rib · cracked · Jul 13, 2020 · N947SW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > RH WING RIB CAP AT WS 48.70 HAS 2EA CRACKS. INSTALLED NEW R/H WING RIB CAP AT WS 48.70 P/N 600-10389-2S. P/O T000055653/5 REF CRJ 200 SRM AND DWG, COMPLIED WITH TASK CARD AND M-337
- [SDR SWIA2020082151925](https://openairdocs.org/sdr/SWIA2020082151925.md): Attach Angle · cracked · Jul 12, 2020 · N947SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > POSSIBLE CRACK ON ATTACH ANGLE AT FS 625.30, APPROX. STGR 14R, RBL 45. INSTALLED INTERCOSTAL ANGLE PART # 601-35012-52 USING NEW ANGLE, NEW LOCK FASTENERS, & NEW LOCK FASTENER COLLARS. IAW SRM AND REO.
- [SDR SWIA2020082151924](https://openairdocs.org/sdr/SWIA2020082151924.md): Attach Angle · cracked · Jul 12, 2020 · N947SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > POSSIBLE CRACK ON ATTACH ANGLE AT FS 625.30, APPROX. STGR 14L, LBL 45 (MARKED) (C-CHECK) RO 8/18/2020 INSTALLED INTERCOSTAL ANGLE PART # 601-35012-51 USING NEW ANGLE, NEW HI-LITE FASTENERS, & NEW HI-LITE COLLARS. REF. CRJ200 SRM AND BOMBARDIER REO. COMP
- [SDR SWIA2020082151923](https://openairdocs.org/sdr/SWIA2020082151923.md): Door Frame · corroded · Jul 10, 2020 · N947SW · Cndair CL6002B19 · Fuselage Main, Structure
  > PAX DOOR FRAME - FS 349 - STGR 15L - DOUBLER BRACKET CORRODED 2X AS MARKED (C-CHECK) RO 8/18/2020 INSTALLED NEW GUSSET P/N 601R38312-41 REF. DWG NO. AND CRJ 200 SRM. COMPLETED SKYWEST TASK CARD.
- [SDR SWIA2020082151940](https://openairdocs.org/sdr/SWIA2020082151940.md): Attach Bracket · corroded · Jul 9, 2020 · N947SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > THE DRAIN ATTACHING BRACKET UNDER THE SERVICE DOOR SURROUND JUST FWD OF FS349.00 HAS CORROSION. RERMOVED AND REPLACED DRAIN ATTACHING BRACKET UNDER THE SERVICE DOOR SURROUND JUST FWD OF FS349.00 IAW SRM
- [SDR SWIA2020082151939](https://openairdocs.org/sdr/SWIA2020082151939.md): Seat Track · corroded · Jul 9, 2020 · N947SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > THE SEAT TRACK AT RBL9.00 HAS CORROSION FROM FS409.00 TO APPROX. FS409.00+128. REMOVED AND REPLACED SEAT TRACK AT FS409 TO 409+128 RBL9 REF AMM.
- [SDR SWIA2020082151938](https://openairdocs.org/sdr/SWIA2020082151938.md): Seat Track · corroded · Jul 9, 2020 · N947SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > THE SEAT TRACK AT LBL9.00 HAS CORROSION FROM FS409.00 TO APPROX. FS409.00+128. REMOVED AND REPLACED SEAT TRACK AT FS409 TO 409+128 LBL9 REF AMM.
- [SDR SWIA2020082151937](https://openairdocs.org/sdr/SWIA2020082151937.md): Seat Track · corroded · Jul 9, 2020 · N947SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > THE SEAT TRACK AT LBL9.00 HAS CORROSION FROM FS364.00 TO FS394.00. 0 INSTALLED NEW SEAT TRACK AT LBL 9.00 FROM F.S. 364.00 TO F.S. 394.00. IAW AMM.
- [SDR SWIA2020082151936](https://openairdocs.org/sdr/SWIA2020082151936.md): Seat Track · corroded · Jul 9, 2020 · N947SW · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > THE SEAT TRACK AT RBL9.00 HAS CORROSION FROM FS349.00 TO FS379.00. INSTALLED NEW SEAT TRACK P/N 601R31032-15 FROM F.S 349.00 TO F.S 379.00 IAW AMM.
- [SDR SWIA2020082151935](https://openairdocs.org/sdr/SWIA2020082151935.md): Fitting · corroded · Jul 9, 2020 · N947SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > THE GALLEY FITTING BETWEEN FS280.00 AND FS295.00 AT RH FLOOR SILL HAS CORROSION. REPLACED GALLEY FTG PLATE BTWN FS.280 & FS. 295.00 AT RH FLOOR SILL. REF. SRM. INSTALLATION COMPLETED USING NEW BLIND RIVETS AND NUTPLATE.
- [SDR SWIA2020082151934](https://openairdocs.org/sdr/SWIA2020082151934.md): Fitting · corroded · Jul 9, 2020 · N947SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > THE GALLEY FITTING BETWEEN FS310.00 AND FS319.00 BETWEEN LBL9.00 AND RBL9.00 HAS CORROSION. REMOVED CORROSION FROM GALLEY FTG BTWN FS310.00 AND FS319.00 BTWN LBL9 AND RBL9 REF SRM. FOUND TO BE OUT OF ALLOWABLE LIMITS REF SRM. FABRICATED AND INSTALLED THE GA
- [SDR SWIA2020082151933](https://openairdocs.org/sdr/SWIA2020082151933.md): Fitting · corroded · Jul 9, 2020 · N947SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > THE GALLEY FITTING AT FS295.00 BETWEEN LBL9.00 AND RBL9.00 HAS CORROSION. REMOVED CORROSION FROM GALLEY FTG AT FS295.0 BTWN LBL9 AND RBL9 REF SRM 51-21-06. FOUND TO BE OUT OF LIMITS PER REF SRM. FABRICATED AND INSTALLED FITTING PLATE FS295.0 BTWN LBL9 AND RB
- [SDR SWIA2020082151932](https://openairdocs.org/sdr/SWIA2020082151932.md): Fitting · corroded · Jul 9, 2020 · N947SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > THE WARDROBE FITTING BETWEEN LBL27.00 AND LBL9.00 AT FS310.00 HAS CORROSION. (MARKED) (C-CHECK) RO 8/18/2020 INSTALLED NEW WARDROBE FITTING REF. CRJ200 SRM. INSTALLATION COMPLETED USING NEW BLIND RIVETS.
- [SDR SWIA2020082151931](https://openairdocs.org/sdr/SWIA2020082151931.md): Fitting · corroded · Jul 9, 2020 · N947SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > THE WARDROBE FITTING BETWEEN LH SILL AT FS310.00 HAS CORROSION. (MARKED) (C-CHECK) RO 8/18/2020 REPLACED WARDROBE FITTING REF. CRJ200 SRM. NEW NUTPLATE AND BLIND RIVETS USED FOR INSTALLATION.
- [SDR SWIA2020082151930](https://openairdocs.org/sdr/SWIA2020082151930.md): Fitting · corroded · Jul 9, 2020 · N947SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > THE WARDROBE FITTING BETWEEN LBL27.00 AND LBL9.00 BETWEEN FS280.00 AND FS295.00 HAS CORROSION. INSTALLED NEW WARDROBE FITTING REF. CRJ200 SRM. INSTALLATION COMPLETED USING NEW BLINDE RIVETS AND NUTPLATE.
- [SDR SWIA2020082151929](https://openairdocs.org/sdr/SWIA2020082151929.md): Fitting · corroded · Jul 9, 2020 · N947SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > THE WARDROBE FITTING ON THE LH FLOOR SILL BETWEEN FS280.00 AND FS295.00 HAS CORROSION. (MARKED) (C-CHECK) RO 8/18/2020 INSTALLED NEW WARDROBE FITTING REF. CRJ200 SRM. INSTALLATION COMPLETED USING NEW CHERRYMAX RIVETS AND NUTPLATE.
- [SDR SWIA2020082151922](https://openairdocs.org/sdr/SWIA2020082151922.md): Door Frame · corroded · Jul 8, 2020 · N947SW · Cndair CL6002B19 · Fuselage Main, Structure
  > A BAY DOOR CUTOUT - FS 394 - STGR 26R - DOOR SEAL LIP CORRODED BELOW R/H AFT DOOR STOP BRKT AS MARKED (C-CHECK) RO 8/18/2020 REMOVED CORROSION ON FRAME ANGLE FS394.00 AND STGR 26R REF CRJ 200 SRM. FOUND TO BE OUT OF LIMITS. PERFORMED REPAIR REF REO. COMPL
- [SDR SWIA2020082151921](https://openairdocs.org/sdr/SWIA2020082151921.md): Intercostal · corroded · Jul 8, 2020 · N947SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > A BAY DOOR CUTOUT - INTERCOSTAL - BETWEEN FS'S 394 / 409 - JUST R OF STGR 27 - CORRODED 2X AS MARKED (C-CHECK) RO 8/18/2020 REMOVED AND REPLACED ABAY DOOR CUTOUT INTERCOSTAL BETWEEN FS394 AND FS409 BETWEEN STR 27 AND STR 26R REF BOMBARDIER DWG AND CRJ200
- [SDR SWIA2020082151920](https://openairdocs.org/sdr/SWIA2020082151920.md): Angle · cracked · Jul 8, 2020 · N947SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS484 CABLE FEED THROUGH INBOARD CLIP CRACKED AT LBL27 (MARKED). (C-CHECK) RO 8/18/2020 REMOVED AND REPLACED CLIP AT FS484 LBL27 IAW CRJ200 SRM, TECHNICAL DATA SOURCE BOMBARDIER ENG. DWG.
- [SDR SWIA2020082151919](https://openairdocs.org/sdr/SWIA2020082151919.md): Angle · cracked · Jul 8, 2020 · N947SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS484 CABLE FEED THROUGH INBOARD CLIP CRACKED AT RBL27 (MARKED). (C-CHECK) RO 8/18/2020 REMOVED AND REPLACED CLIP AT FS484 RBL27 IAW CRJ200 SRM, TECHNICAL DATA SOURCE BOMBARDIER ENG. DWG.
- [SDR SWIA2020082151918](https://openairdocs.org/sdr/SWIA2020082151918.md): Pressure Deck · cracked · Jul 8, 2020 · N947SW · Cndair CL6002B19 · Fuselage Main, Structure
  > PRESSURE FLOOR CRACKED BETWEEN BL0 AND RBL9 AT FS461 AND SUSPECTED CRACK BETWEEN BL0 AND LBL9 AT FS461 (MARKED). (C-CHECK) RO 8/18/2020 REPAIRED PRESSURE FLOOR WEB AT FS461 BETWEEN LBL9 AND RBL9 REF REO. COMPLIED WITH TASK CARD.

Next page: https://openairdocs.org/aircraft/N947SW/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 = 'N947SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N947SW/reports

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