# Service difficulty reports: N953SW

A list on [N953SW](https://openairdocs.org/aircraft/N953SW.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 · 177 reports

- [SDR SWIA2025031009](https://openairdocs.org/sdr/SWIA2025031009.md): Fuel Sys · malfunctioned · Mar 9, 2025 · N953SW · Cndair CL6002B19 · Aircraft Fuel System
  > TAKING OFF WELL ABOVE MINTO. AFTER REACHING TOC A 200LB LESS, GOT TO SECOND FIX AT PLANNED FUEL WEIGHT. DURING CRUISE AND ARRIVAL LANDING FUEL WEIGHT CONTINUED DEACREASING IN A RAPID TREND AND AFTER GETTING TO MINIMUM FUEL, HAD TO DIVERT TO ALTERNATE. FUEL BUR
- [SDR SWIA202503040002](https://openairdocs.org/sdr/SWIA202503040002.md): Warning Message · false activation · Mar 2, 2025 · N953SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > PROX SYS CHAN CAUTION. RAN QRH. LANDING GEAR CAME DOWN. (FLIGHT 5335 - FILED CLOSED) AFTER MAINTENANCE (REF: AML 1549668), MESSAGE CLEARED. PERFORMED AN OPS CHECK OF THE PSEU IN REF TO AMM 32-61-00. OPS CHECK GOOD. PERFORMED MLG EXTENSION AND RETRACTION
- [SDR SWI2025F00272](https://openairdocs.org/sdr/SWI2025F00272.md): Warning Message · activated · Mar 2, 2025 · N953SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > PROX SYS CHAN CAUTION. RAN QRH. LANDING GEAR CAME DOWN. (FLIGHT 5335 - FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA2024121001359](https://openairdocs.org/sdr/SWIA2024121001359.md): Window · broken · Dec 5, 2024 · N953SW · Cndair CL6002B19 · Flight Compartment Windows
  > L SIDE WINDOW BORKEN DURING CLIMB AT FL240. DIVERTED TO KLAS. (FLIGHT 5117 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 29276079 WITH THE FOLLOWING CORRECTIVE ACTION: "COMPLIED WITH TASK CARD 56-220-1000-SKY REMOVED AND REPLACED LH WINDO
- [SDR SWIA2024031209](https://openairdocs.org/sdr/SWIA2024031209.md): Warning Message · illuminated · Mar 9, 2024 · N953SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE WARNING AFTER SELECTING LANDING GEAR LEVER DOWN IN FLIGHT. RAN QRH TO PULL LANDING GEAR MANUAL RELEASE HANDLE. AFTER PULLING THE GEAR MANUAL RELEASE HANDLE GOT ALL 3 GEAR DN WITH NO MESSAGE. (FLIGHT 5624 FILED CLOSED)THIS DISCREPANCY WAS TRANSFER
- [SDR SWIA2024031100009](https://openairdocs.org/sdr/SWIA2024031100009.md): Warning Message · illuminated · Mar 9, 2024 · N953SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE WARNING AFTER SELECTING LANDING GEAR LEVER DOWN IN FLIGHT. RAN QRH TO PULL LANDING GEAR MANUAL RELEASE HANDLE. AFTER PULLING THE GEAR MANUAL RELEASE HANDLE GOT ALL 3 GEAR DN WITH NO MESSAGE. (FLIGHT 5624 FILED OPEN)THIS IS CURRENTLY A WORK IN PRO
- [SDR SWIA20240202122](https://openairdocs.org/sdr/SWIA20240202122.md): Duct · warning message · Jan 22, 2024 · N953SW · Cndair CL6002B19 · Engine Anti-Icing System
  > ANTI-ICE DUCT WARNING MESSAGE APPEARED WHILE IN CRUISE. QRH RESOLVED THE ISSUE. (FLIGHT 4797 FILED CLOSED)PERFORMED OPERATIONAL TEST OF THE ENGINE-COWL ANTI-ICE SYSTEM PER CRJ-200 AMM TASK 30-22-00-710-802, OPS CHECK GOOD.
- [SDR SWIA2024012300012](https://openairdocs.org/sdr/SWIA2024012300012.md): Anti-Ice System · warning message · Jan 22, 2024 · N953SW · Cndair CL6002B19 · Engine Anti-Icing System
  > ANTI-ICE DUCT WARNING MESSAGE APPEARED WHILE IN CRUISE. QRH RESOLVED THE ISSUE. (FLIGHT 4797 FILED OPEN)PERFORMED OPERATIONAL TEST OF THE ENGINE-COWL ANTI-ICE SYSTEM PER CRJ-200 AMM TASK 30-22-00-710-802, OPS CHECK GOOD.
- [SDR SWIA20231027901](https://openairdocs.org/sdr/SWIA20231027901.md): Unknown · chafed · Sep 1, 2023 · N953SW · Cndair CL6002B19 · Wing, Plate/Skin
  > LH LWR WING PLANK FWD OF THE MLG CUTOUT, W.S. 45.0 TO W.S. 47.61, HAS CHAFFING. (C-CHECK RO 10/29/2023) BLENDED OUT CHAFE ON LH LOWER WING PLANK FWD OF THE MLG CUTOUT, W.S 45.0 T0 47.61. REF CRJ 200 SRM 51-12-00RECEIVED ENGINEERING SUPPORT, FOR CHAFFING B
- [SDR SWIA2023102700831](https://openairdocs.org/sdr/SWIA2023102700831.md): Unknown · cracked · Aug 31, 2023 · N953SW · Cndair CL6002B19 · Fuselage Main, Frame
  > POSSIBLE CRACK AT F.S. 319 FRAME, FWD SIDE AT STGR 2R. (C-CHECK RO 10/29/2023) COMPLIED WITH PERMANENT REPAIR ON FRAME SECTOR FS319. BETWEEN STRG-1R -STGR -2R, ENSURED ALL REQUIREMENTS ARE MET IN REF REO 601R-53-21-3650 REV-- DATED 2023-09-06. COMPLIED WIT
- [SDR SWIA2023102700824](https://openairdocs.org/sdr/SWIA2023102700824.md): Unknown · damaged · Aug 24, 2023 · N953SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LBL 27 - APROX FS 621 - FLOOR BEAM ATTACHMENT TO REAR PRESSURE BULKHEAD HAS ERRANT HOLE ON INBD SIDE (27069818) (C-CHECK RO 10/29/2023) PLUGGED REDUNDANT HOLE PER REO 601R-53-61-8066 REV--, DATED 2023-08-17. COMPLIED WITH SKYCARD 51-900-1003-SKY. NO WEIGHT
- [SDR SWIA20231027822](https://openairdocs.org/sdr/SWIA20231027822.md): Unknown · damaged · Aug 22, 2023 · N953SW · Cndair CL6002B19 · Elevator, Spar/Rib
  > DURING AUDIT OF 40K TASK CARD 55-340-602(DETAILED INSPECTION OF THE RIGHT ELEVATOR FRONT SPAR ASSEMBLY) FOUND THAT THE RH ELEVATOR HAS DAMAGE ON INBOARD SIDE OF FRONT SPAR. (C-CHECK RO 10/29/2023) REPAIRED ELEVATOR IB LE DAMAGE TO THE FRONT SPAR PER MHIRJ
- [SDR SWI2023F00442](https://openairdocs.org/sdr/SWI2023F00442.md): Unknown · damaged · Aug 21, 2023 · N953SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > DURING AUDIT OF 1C TASK CARD 53-310-301(EXTERNAL ZONAL INSPECTION OF THE AFT FUSELAGE, FS621.00 TOFS755.00) FOUND AFT EQ BAY DOOR HAS DENTED CENTER INTERCOSTAL. (C-CHECK RO 10/29/2023) REMOVED DAMAGED INTERCOSTAL FROM AFT EQUIPMENT COMPARTMENT DOOR PER REF
- [SDR SWIA202310270821](https://openairdocs.org/sdr/SWIA202310270821.md): Unknown · corroded · Aug 21, 2023 · N953SW · Cndair CL6002B19 · Fuselage Main, Frame
  > ANGLE ON FRAME AT FS589 BETWEEN STR 23R - 23L IS CORRODED. (C-CHECK RO 10/29/2023) REPLACED ANGLE AT FRAME FS589 REF CRJ200 SRM 51-42-06 AND DWG#601R36025 REV-P. COMPLIED WITH SKY CARD 51-900-1003-SKY
- [SDR SWIA202310270818](https://openairdocs.org/sdr/SWIA202310270818.md): Unknown · damaged · Aug 18, 2023 · N953SW · Cndair CL6002B19 · Wing, Plate/Skin
  > RIVET COUNTER SINKS ARE DAMAGED AT LWR NUTPLATE HOLE UNDER 141AL (MARKED). (C-CHECK RO 10/29/2023) REPAIRED RIVET COUNTER SINKS UNDER ACCESS PANELS 141AL REF REO 601R-53-21-3648 REV-- DATED 2023-09-12. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOO
- [SDR SWIA20231027816](https://openairdocs.org/sdr/SWIA20231027816.md): Unknown · damaged · Aug 16, 2023 · N953SW · Cndair CL6002B19 · Wing, Plate/Skin
  > L/H ON WING PLANK FUEL ASSESS PANEL LOCATION 540BB HAS EVIDENCE OF FRETTING. (C-CHECK RO 10/29/2023) PERFORMED REPAIR ON LH WING PLANK ON FUEL PANEL 540BB. PER ALL STEPS OF REO 601R-57-21-030 REV -L DATED 2014-02-05. NO LEAKS NOTED. COMPLIED WITH ALL ST
- [SDR SWIA20231027814](https://openairdocs.org/sdr/SWIA20231027814.md): Unknown · cracked · Aug 14, 2023 · N953SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > COCKPIT FLOOR SUPPORT ANGLE IS CRACKED (C-CHECK RO 10/29/2023) REMOVED AND INSTALLED NEW COCKPIT FLOOR SUPPORT ANGLE. REF: REO 601R-53-11-926 REV -B DATE 2006/5/10.COMPLIED WITH 51-900-1003-SKY
- [SDR SWIA20231027812](https://openairdocs.org/sdr/SWIA20231027812.md): Unknown · failed · Aug 12, 2023 · N953SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > PASSENGER DOOR PIANO HINGE HALF ON FUSELAGE SIDE FAILED THE GO NO-GO CHECK OF THE DIAMETER OF THE HOLES. (C-CHECK RO 10/29/2023) REMOVED AND INSTALLED NEW PAX DOOR PIANO HINGE FUSELAGE SIDE IAW CRJ 200 SRM 53-21-23 AND DWG 601R31527 REV. AM, REO 601R-53-21
- [SDR SWI2023F00441](https://openairdocs.org/sdr/SWI2023F00441.md): Unknown · cracked · Aug 11, 2023 · N953SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING REMOVAL OF FLOOR SUPPORT CLIP, DISCOVERED CRACK IN FS280 BULKHEAD LOWER WEB AT RBL9. (C-CHECK RO 10/29/2023) REMOVED AND REPLACED EXISTING REPAIR PARTS @ FS280.00 BULKHEAD LOWER WEB. REF: REO 601R-53-11-926 REV -B DATE 2006/05/10COMPLIED WITH SKYWES
- [SDR SWI2023F00440](https://openairdocs.org/sdr/SWI2023F00440.md): Unknown · cracked · Aug 11, 2023 · N953SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RBL9 FLOORBEAM STRUCTURE AT FS280 OUTBOARD ANGLE CLIP CRACKED (C-CHECK RO 10/29/2023) REMOVED AND REPLACED FS280 FLOOR SUPPORT CLIP AT RBL9 OUTBOARD.. REF: REO 601R-53-11-926 REV -B DATE 2006/5/10COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19
- [SDR SWI2023F00439](https://openairdocs.org/sdr/SWI2023F00439.md): Unknown · cracked · Aug 11, 2023 · N953SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RBL9 FLOORBEAM STRUCTURE AT FS280 INBOARD ANGLE CLIP CRACKED (C-CHECK RO 10/29/2023) INSTALLED NEW FS280 FLOOR SUPPORT CLIP AT RBL9 INBOARD.. REF: PREVIOUSLY INCORPERATED REO 601R-53-11-926 REV -B DATE 2006/5/10.COMPLIED WITH 51-900-1003-SKY
- [SDR SWI2023F00438](https://openairdocs.org/sdr/SWI2023F00438.md): Unknown · elongated · Aug 11, 2023 · N953SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX DOOR HINGE, DOOR SIDE, ROLL PIN HOLE IS ELONGATED (C-CHECK RO 10/29/2023) REMOVED AND INSTALLED NEW PAX DOOR HINGE REF CRJ 200 SRM 52-10-31,DWG 601R31702 REV. N AND REO 601R-52-11-2987 REV. -- DATED 2023-08-21. COMPLIED WITH 51-900-1003-SKY AND PRESSU
- [SDR SWI2023F00437](https://openairdocs.org/sdr/SWI2023F00437.md): Unknown · cracked · Aug 11, 2023 · N953SW · Cndair CL6002B19 · Fuselage Main, Structure
  > BRACKET CRACKED BELOW LH WINDSHIELD SIDE POST (BELOW THE SILL MARKED) (C-CHECK RO 10/29/2023) REMOVED AND INSTALLED NEW BRACKET AT BELOW LH WINDSHIELD SIDE POST (BELOW THE SILL MARKED) REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21 AND DWG #601R34032 REV (V)
- [SDR SWIA20231027810](https://openairdocs.org/sdr/SWIA20231027810.md): Unknown · corroded · Aug 10, 2023 · N953SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME AT FS574 STGR25R- STRG26L HAS CORROSION (C-CHECK RO 10/29/2023) REMOVED CORROSION FROM FS574 TGR25R- STRG26L FRAME OUTER FLANGE AND REPAIRED REF. REO 601R-53-61-8078 REV. -- DATED 2023-09-06 STEPS 1-5. ALL STEPS COMPLIED WITH. COMPLIED WITH TASK CARD
- [SDR SWIA202310272229](https://openairdocs.org/sdr/SWIA202310272229.md): Unknown · corroded · Aug 9, 2023 · N953SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > L/H FLOOR BEAM AT FS559.00 BETWEEN LBL27 AND L/H FLOOR SILL HAS CORROSION (MARKED) (C-CHECK RO 10/29/2023) REMOVED AND REPLACED LH FLOOR STRAP/BEAM AT F.S. 559.00 BETWEEN LBL27 AND LH FLOOR SILL, REF CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-45-00 AND DWG 601R3
- [SDR SWIA202310270009](https://openairdocs.org/sdr/SWIA202310270009.md): Unknown · cracked · Aug 9, 2023 · N953SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FS280.00 SEAT RAIL STRUCTURE AT LBL9 OUTBOARD ANGLE CLIP CRACKED (MARKED) (C-CHECK RO 10/29/2023) FABRICATED, LOCATED, DRILLED AND INSTALLED THE FS280 FLOOR SUPPORT CLIP AT LBL9 OUTBOARD WITH 2024 T-42.050" P.O. # T70541. REF: PREVIOUSLY INCORPERATED REO
- [SDR SWIA202310270809](https://openairdocs.org/sdr/SWIA202310270809.md): Unknown · cracked · Aug 9, 2023 · N953SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FS280.00 SEAT RAIL STRUCTURE AT LBL9 INBOARD ANGLE CLIP CRACKED (MARKED) (C-CHECK RO 10/29/2023) REMOVED AND REPLACED FS280 FLOOR SUPPORT CLIP AT LBL9 INBOARD.. REF: REO 601R-53-11-926 REV -B DATE 2006/5/10COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY ST
- [SDR SWIA20231027809](https://openairdocs.org/sdr/SWIA20231027809.md): Unknown · corroded · Aug 9, 2023 · N953SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > R/H FLOOR SILL BETWEEN FS310.00 TO FS319.70 HAS CORROSION (MARKED) (C-CHECK RO 10/29/2023) REMOVED CORROSION ON RH FLOOR SILL BETWEEN FS310.00 TO FS319.70. REF CRJ-200 SRM 51-21-06. ORIGINAL THICKNESS OF 0.063". REMAINING THICKNESS OF 0.028" MATERIAL LOSS
- [SDR SWIA2023102700808](https://openairdocs.org/sdr/SWIA2023102700808.md): Unknown · corroded · Aug 8, 2023 · N953SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME @ FS 589.00 STR 25L- 25R HAS CORROSION AROUND LWR EDGE OF FRAME (C-CHECK RO 10/29/2023) REMOVED AND INSTALLED NEW LOWER SECTION FRAME AT FS 589.00 BETWEEN STRG 20L-20R CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21, AND DWG#601R36025 REV-P. NO LEAKS NOTE
- [SDR SWIA20231027008](https://openairdocs.org/sdr/SWIA20231027008.md): Unknown · corroded · Aug 8, 2023 · N953SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > R/H FLOOR BEAM AT FS559.00 BETWEEN RBL27 AND R/H FLOOR SILL HAS CORROSION (MARKED) (C-CHECK RO 10/29/2023) REMOVED AND INSTALLED NEW REPLACEMENT STRAP P/N 601R31025-29 AT FS.559.00 R/H PRESSURE FLOOR SUPPORT STRUCTURE BETWEEN RBL 27 & RBL 36 PER CRJ200 SR
- [SDR SWIA20231027808](https://openairdocs.org/sdr/SWIA20231027808.md): Unknown · corroded · Aug 8, 2023 · N953SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > L/H SEAT RAIL BEAM AT LBL27 BETWEEN FS605.00 TO FS621.00 HAS CORROSION (MARKED) (C-CHECK RO 10/29/2023) PERFORMED REPAIR TO LH SEAT RAIL FLOOR BEAM LOCATED AT LBL27 FS605 - FS621. PER ALL STEPS OF REO 601R-53-61-8066 REV -- DATED 2023-08-17. BLEND REPAIR O
- [SDR SWIA202310270807](https://openairdocs.org/sdr/SWIA202310270807.md): Unknown · corroded · Aug 7, 2023 · N953SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > L/H PRESSURE FLOOR SILL FROM FS 409+128 TO FS 559 HAS MULTIPLE SPOT OF CORROSION (C-CHECK RO 10/29/2023) REMOVED CORROSION ON LH PRESSURE FLOOR BETWEEN FS409+128 TO FS559 REF CRJ200 SRM 51-21-06. EVALUATED 23EA BLENDS ON LH PRESSURE FLOOR BETWEEN FS409+112
- [SDR SWIA2023102707](https://openairdocs.org/sdr/SWIA2023102707.md): Unknown · corroded · Aug 7, 2023 · N953SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > R/H PRESSURE FLOOR SILL FROM FS 409+128 TO FS 559 HAS MULTIPLE SPOT OF CORROSION (C-CHECK RO 10/29/2023) REPAIRED CORROSION AT 16EA LOCATIONS ALONG RH PRESSURE FLOOR SILL FROM F.S. 409+128 TO 559.0 PER MHIRJ REO 601R-53-41-3185REV -- DATED 2023-08-28 AND B
- [SDR SWIA2023102787](https://openairdocs.org/sdr/SWIA2023102787.md): Unknown · cracked · Aug 7, 2023 · N953SW · Cndair CL6002B19 · Doors
  > NLG - AFT DOOR CUTOUT - AFT L/H NLG DOOR CUTOUT RADIUS HAS SUSPECTED CRACK - APROX FS 235 (C-CHECK RO 10/29/2023) CUT AWAY DAMAGED / CRACKED AREA AND PERFORMED DOUBLER REPAIR AS PER REO 601R-53-11-048 REV. -D, DATED 06/10/15, SEE CONTINUE CARD FOR DETAILS.
- [SDR SWIA20231027807](https://openairdocs.org/sdr/SWIA20231027807.md): Unknown · cracked · Aug 7, 2023 · N953SW · Cndair CL6002B19 · Doors
  > NLG - AFT DOOR CUTOUT - AFT R/H NLG DOOR CUTOUT RADIUS HAS SUSPECTED CRACK - APROX FS 235 (C-CHECK RO 10/29/2023) PERFORMED REO 601R-53-11-048 REV. -D ISSUED 06/10/15 REPAIR TO AFT RH NLG CUTOUT RADIUS. COMPLIED WITH 51-900-1003-SKY
- [SDR SWIA20231027806](https://openairdocs.org/sdr/SWIA20231027806.md): Unknown · corroded · Aug 6, 2023 · N953SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > MULTIPLE AREAS OF CORROSION ON THE EXTERNAL LOWER SKIN WHERE FORWARD WING FAIRINGS ( 191BB AND 192BB) ATTACH AT FASTENER HOLES. (C-CHECK RO 10/29/2023) REMOVED MULTIPLES AREAS OF CORROSION ON THE EXTERNAL LOWER SKIN WHERE FORWARD WING FAIRINGS ( 191BB AND
- [SDR SWIA2023102700805](https://openairdocs.org/sdr/SWIA2023102700805.md): Unknown · cracked · Aug 5, 2023 · N953SW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > FWD RH BATT RIB WS53 IS CRACKED (MARKED) (C-CHECK RO 10/29/2023) INSTALLED NEW BAT RIB, FWD RH SIDE AT WS53.00. PER DWG 601R10203 REV-G AND CRJ 200 SRM 51-42-21. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY
- [SDR SWIA202310278005](https://openairdocs.org/sdr/SWIA202310278005.md): Unknown · cracked · Aug 5, 2023 · N953SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STGR3L CRACKED AT FS379.00. (C-CHECK RO 10/29/2023) REMOVED AND INSTALLED NEW ANGLE AT STGR3L AT FS 379.00 REF CRJ-200-SRM 53-00-03 AND CRJ-200-SRM 51-42-06. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOOD. SEE CONTINUATION CARD FOR DETAILS
- [SDR SWIA2023102705](https://openairdocs.org/sdr/SWIA2023102705.md): Unknown · cracked · Aug 5, 2023 · N953SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STGR3L ATTACHING STRUCTURE TO FS280.00 BULKHEAD IS CRACKED. (C-CHECK RO 10/29/2023) REMOVED AND INSTALLED NEW REPLACEMENT END ANGLE P/N 600-31057-19 ON STGR 3L AT FS.280 PER CRJ200 SRM 51-42-06 & SRM 51-42-21 REF. BOMBARDIER DWG. 600-31057 REV. P, NO LEAKS
- [SDR SWIA202310270805](https://openairdocs.org/sdr/SWIA202310270805.md): Unknown · cracked · Aug 5, 2023 · N953SW · Cndair CL6002B19 · Wing Structure
  > LEFT WING BATT RIB WS48.30 ANGLE ON THE FORWARD END OF THE CAP IS CRACKED. (C-CHECK RO 10/29/2023) REMOVED AND REPLACED LH WING BATT RIB ANGLE AT W.S. 48.30 WITH NEW, REF CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-21 AND DWG 600-10204 REV -L. COMPLIED WITH
- [SDR SWIA202310805](https://openairdocs.org/sdr/SWIA202310805.md): Unknown · corroded · Aug 5, 2023 · N953SW · Cndair CL6002B19 · Wing Structure
  > LEFT WING BATT RIB WS53.60 ANGLE ON THE FORWARD END INBOARD SIDE IS CORRODED. (C-CHECK RO 10/29/2023) WET INSTALLED NEW LH BATT RIB ASSY AT WS53.60 REF CRJ-200 SRM 51-42-21, CRJ-200 SRM 51-42-06 AND DRAWING NO: 601R10203 REV-G. COMPLIED WITH SKYWEST T
- [SDR SWIA202310270803](https://openairdocs.org/sdr/SWIA202310270803.md): Unknown · corroded · Aug 3, 2023 · N953SW · Cndair CL6002B19 · Galley Doors
  > SERVICE DOOR FORWARD FORMER IS CORRODED EXTERNALY ALONG THE BOTTOM OF THE FORMER, (MARKED) (C-CHECK RO 10/29/2023) REPLACED FWD FORMER (LOWER FWD PAN) P/N 601R38437-2 ON SERVICE DOOR, REF. CRJ200 SRM 51-42-06 & STRUCTURE ASSEMBLY, SERVICE DOOR DWG. 601R38
- [SDR SWIA2023102700803](https://openairdocs.org/sdr/SWIA2023102700803.md): Unknown · chafed · Aug 3, 2023 · N953SW · Cndair CL6002B19 · Fuselage Structure (General)
  > CLUSTER OF CHAFES BETWEEN FS589-FS605 STGR22R-STGR25R (MARKED) (C-CHECK RO 10/29/2023) REPAIRED CLUSTER OF CHAFES BETWEEN FS589-FS605 STGR22R-STGR25R REF CRJ200 SRM 51-42-06, REO 601R-53-61-8077 REV -- DATE 2023-09-06 AND REO 601R-51-00-309 REV -A DATE
- [SDR SWIA20231027802](https://openairdocs.org/sdr/SWIA20231027802.md): Unknown · cracked · Aug 2, 2023 · N953SW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > RH WING TRAILING EDGE RIB AT WS130.0 HAS A CRACK (C-CHECK RO 10/29/2023) REPAIRED CRACKED RH TRAILING EDGE RIB AT W.S. 130.0 PER MHIRJ REO 601R-57-51-1022 REV -- DATED 2023-08-07COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19) STRUCTURAL MAJOR
- [SDR SWIA20231027028](https://openairdocs.org/sdr/SWIA20231027028.md): Unknown · chafed · Jul 28, 2023 · N953SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBOARD FLAP VANE LEADING EDGE IS CHAFED AT WS97. S/N 111 (C-CHECK RO 10/29/2023) REMOVED AND INSTALLED NEW L/H INBOARD FLAP VANE LEADING EDGE CRJ 200 SRM 51-42-13 AND DRAWING 601R14302 REV E. COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATION CARD
- [SDR SWIA2019062746005](https://openairdocs.org/sdr/SWIA2019062746005.md): Proximity Sensor · failed · Jun 27, 2019 · N953SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > WHILE IN CRUISE GEAR DISAGREE WARNING MESSAGE CAME ON, THE GEAR FUNCTIONED NORMALLY ON LANDING. R&R DOWNLOCK PROXIMITY SENSOR HARNESS IAW AMM. SWUNG ALL 3 GEAR MULTIPLE TIMES WITHOUT ANY DEFECTS IAW AMM. OPS CHECKS GOOD.
- [SDR SWIA2019050345823](https://openairdocs.org/sdr/SWIA2019050345823.md): Skin · damaged · Apr 21, 2019 · N953SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DAMAGE AT FS 640-654 AND STR'S 23L-24L. (C-CHECK) RO: 05/02/2019 REPAIRED FUSELAGE SKIN DAMAGE AT FS 640-654 AND STR'S 23L-24L. BY EXTERNAL DOUBLER IAW REO.
- [SDR SWIA2019050345821](https://openairdocs.org/sdr/SWIA2019050345821.md): Skin · damaged · Apr 18, 2019 · N953SW · Cndair CL6002B19 · Wing, Plate/Skin
  > RT WING PLANK MOST AFT FASTENER HOLE ON END OF STRAP OVERSIZED. (C-CHECK) RO: 05/02/2019 COMPLIED WITH REPAIR OF RT WING PLANK MOST AFT FASTENER HOLE ON END OF STRAP OVERSIZED IAW REO.
- [SDR SWIA2019050345824](https://openairdocs.org/sdr/SWIA2019050345824.md): Elevator · damaged · Apr 16, 2019 · N953SW · Cndair CL6002B19 · Elevator Structure
  > LT ELEVATOR TRAILING EDGE HAS DAMAGE NOTED APPROXIAMTELY 3 INCHES AND 6 INCHES FROM IB EDGE. (C-CHECK) RO: 05/02/2019 REPAIRED LT ELEVATOR IAW SRM AND REO.
- [SDR SWIA2019050345820](https://openairdocs.org/sdr/SWIA2019050345820.md): Cleat · corroded · Apr 12, 2019 · N953SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR FWD AND AFT CLEATS CORRODED AROUND NUTPLATES. (C-CHECK) RO: 05/02/2019 REMOVED AND INSTALLED NEW CLEATS P/N 601R31527-137 AND 601R31527-217, IAW SRM.

Next page: https://openairdocs.org/aircraft/N953SW/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 = 'N953SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N953SW/reports

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