# Service difficulty reports: N956SW

A list on [N956SW](https://openairdocs.org/aircraft/N956SW.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 · 216 reports

- [SDR SWIA2026071976657](https://openairdocs.org/sdr/SWIA2026071976657.md): A/C Pack · warning message · Jul 19, 2026 · N956SW · Cndair CL6002B19 · Cabin Cooling System
  > RIGHT PACK HIGH PRESSURE ON CLIMB OUT AT 11000, MESSAGE DISAPPEARED, CABIN ALT WARNING MESSAGE APPEARED THEN BECAME A CABIN ALT CAUTION AS WE DESCENDED BACK THOUGH 11000. RAN THE QRH FOR CABIN ALT AND DIVERTED BACK TO DENVER. (FLIGHT 5224) OPEN.
- [SDR SWIA2026020275110](https://openairdocs.org/sdr/SWIA2026020275110.md): Seal · damaged · Jan 19, 2026 · N956SW · Cndair CL6002B19 · Fuselage Main, Structure
  > LEFT MLG WHEEL WELL UPPER STRUCTURE DAMAGED. REPAIRED THE WHEEL WELL UPPER STRUCTURE IAW REO 601R-53-41-3383, REV P3. ON TASK CARD 27-900-1008-SKY.
- [SDR SWIA2025120375109](https://openairdocs.org/sdr/SWIA2025120375109.md): Window Frame · cracked · Dec 3, 2025 · N956SW · Cndair CL6002B19 · Fuselage Main, Structure
  > AFTER EDDY CURRENT INSPECTION OF THE WINDWSHIELD CENTER POST, NR 8 ATTACH STRUCTURE CRACKS WERE FOUND IN LOWER PART. R & R WINDWSHIELD CENTER POST NR 8 ATTACH STRUCTURE IAW 00 SRM 51-24-16, SRM 51-42-21, IPC 53-11-19, PAGE 6.
- [SDR SWIA2025120375108](https://openairdocs.org/sdr/SWIA2025120375108.md): Floor Support · corroded · Dec 3, 2025 · N956SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT FLOOR SUPPORT, RBL 9, BTWN BS 559 +64 - 559 + 80 CORRODED. R & R THE FLOOR SUPPORT IAW SRM 51-42-21, NO FURTHER ACTION IS REQUIRED, JOB COMPLETED
- [SDR SWIA2026020270111](https://openairdocs.org/sdr/SWIA2026020270111.md): Floorbeam · corroded · Nov 19, 2025 · N956SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FWD CABIN- UNDER FLOOR FRAME FS 333.00 HAS CORROSION BETWEEN STRG 23L TO 23R. REMOVED AND REPLACED FWD CABIN- UNDER FLOOR FRAME FS 333.00 BETWEEN STRG 18LH TO 23RH IAW SRM 51-42-06, SRM 51-42-21.
- [SDR SWIA20250430027](https://openairdocs.org/sdr/SWIA20250430027.md): Pump · faulted · Apr 27, 2025 · N956SW · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), Main
  > HYD 3 LO PRESS AND GEAR DISAGREE. DID MANUAL GEAR EXTENSION AND HYD 3 QRH (FLIGHT 5539 - FILED CLOSED)FOUND HYDRAULIC PUMP 3A CRACKED, REMOVED AND REPLACED HYDRAULIC PUMP 3A WITH A SERVICEABLE UNIT IN REFERENCE TO AMM 29-12-03, NO LEAKS NOTED. PLEASE REFERENC
- [SDR SWIA202504280007](https://openairdocs.org/sdr/SWIA202504280007.md): Hydraulic System · low pressure · Apr 27, 2025 · N956SW · Cndair CL6002B19 · Hydraulic System, Main
  > HYD 3 LO PRESS AND GEAR DISAGREE. DID MANUAL GEAR EXTENSION AND HYD 3 QRH (FLIGHT 5539 - FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA202504070005](https://openairdocs.org/sdr/SWIA202504070005.md): Uplock Hook · fod · Apr 5, 2025 · N956SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE WARNING ON GEAR RETRACTION AFTER TAKEOFF, LEFT MAIN INDICATING RED. WENT AWAY WITH QRH PROCEDURE, GEAR REMAINED DOWN AND LOCKED ON LANDING AT SFO. (FLIGHT 5951 - FILED CLOSED)REFERENCED FAULT ISOLATION MANUAL 32-60-07, UPON TROUBLESHOOTING FOUND
- [SDR SWIA202412301406](https://openairdocs.org/sdr/SWIA202412301406.md): Steering Sys · inoperative · Dec 29, 2024 · N956SW · Cndair CL6002B19 · Landing Gear Steering System
  > CAUTION STEERING INOP ON TAKE OFF CREW REPORTED GEAR UP AT APPROX 50 FT AFTER T/O. INTERROGATED MDC FAULT HISTORY. BITS 20, 25, AND 26 SET TO 1. PER CRJ 200 FIM 32-50-01 FIGURE 103 NOTE 3: "STEERING INOP (C) NUISANCE MESSAGE ON TAKE-OFF: WHEN THE AIRCRAFT T
- [SDR SWIA202410110006](https://openairdocs.org/sdr/SWIA202410110006.md): Windshield · cracked · Oct 6, 2024 · N956SW · Cndair CL6002B19 · Flight Compartment Windows
  > FO SIDE WINDSHIELD HAS VERTICAL CRACK ALONG CENTER POST. (FLIGHT 4752 - FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 28954710 WITH THE FOLLOWING CORRECTIVE ACTION: "REFERENCE CAMP CP28955885 FOR THE REMOVAL OF THE FO'S WINDSHIELD.INSTALLED FO SI
- [SDR SWI2024F00905](https://openairdocs.org/sdr/SWI2024F00905.md): Windshield · cracked · Oct 6, 2024 · N956SW · Cndair CL6002B19 · Flight Compartment Windows
  > FO SIDE WINDSHIELD HAS VERTICAL CRACK ALONG CENTER POST. (FLIGHT 4752 - FILED OPEN) PLEASE REFERENCE AML 1445552
- [SDR SWIA2024090900005](https://openairdocs.org/sdr/SWIA2024090900005.md): Pressure Deck · out of limits · Sep 5, 2024 · N956SW · Cndair CL6002B19 · Fuselage Main, Structure
  > RH PRESSURE FLOOR SILL FS449.85 BLEND OUT IS BEYOND LIMITS OF GENERIC REO 601R-53-41-666 REV "C". (FILED CLOSED) PERFORMED REPAIR OF RH PRESSURE FLOOR SILL FS449.85 WITH REFERENCE TO REO 601R-53-41-3258 REV "--" DATED 2024-09-11. COMPLIED WITH TASK CARD
- [SDR SWIA2024090600005](https://openairdocs.org/sdr/SWIA2024090600005.md): Floor Support · out of limits · Sep 5, 2024 · N956SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH PRESSURE FLOOR SILL FS449.85 BLEND OUT IS BEYOND LIMITS OF GENERIC REO 601R-53-41-666 REV "C". (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWI2024F00900](https://openairdocs.org/sdr/SWI2024F00900.md): Hinge Pin · corroded · Aug 19, 2024 · N956SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > CORROSION FOUND UNDER PANEL 141AL ON THE UPPER SURFACE UNDER THE HINGE PIN, VISIBLE WITH THE DOOR CLOSED. (FILED CLOSED) BLENDED DAMAGED AREA UNDER PANEL 141AL ON THE UPPER SURFACE UNDER THE HINGE PIN ON FUSELAGE SKIN WITH REFERENCE TO SRM 51-21-06. PER
- [SDR SWIA20240819](https://openairdocs.org/sdr/SWIA20240819.md): Hinge Pin · corroded · Aug 19, 2024 · N956SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > CORROSION FOUND UNDER PANEL 141BL ON THE UPPER SURFACE UNDER THE HINGE PIN, VISIBLE WITH THE DOOR CLOSED. (FILED CLOSED) BLENDED DAMAGED AREA UNDER PANEL 141BL ON THE UPPER SURFACE UNDER THE HINGE PIN ON FUSELAGE SKIN WITH REFERENCE TO SRM 51-21-06. PER
- [SDR SWIA20241030810](https://openairdocs.org/sdr/SWIA20241030810.md): Track · damaged · Aug 10, 2024 · N956SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > FORWARD AND AFT CARGO DOOR TRACKS DAMAGED ON THE OUTSIDE OF TRACK AT THE BOTTOM WHERE CARGO DOOR PINS HAVE COME INTO CONTACT (FILED CLOSED) REMOVED AND REPLACED AFT CARGO DOOR TRACK WITH REFERENCE TO SRM 51-42-06 AND SRM 51-42-13. COMPLIED WITH TASK CAR
- [SDR SWI2024F00899](https://openairdocs.org/sdr/SWI2024F00899.md): Pressure Blkhd · damaged · Aug 8, 2024 · N956SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD FORWARD FACE HAS 5 DAMAGED FASTENERS, 11 GOUGES AND ONE SCRATCH ABOUT 4 INCHES LONG (FILED CLOSED) COMPLIED WITH REO 601R-53-61-8215 DATED: 2024-08-22 REV €“ FOR THE BLENDED GOUGES ON FS 621.00 BULKHEAD AND FASTENER REPLACEMENT TO
- [SDR SWI2024F00898](https://openairdocs.org/sdr/SWI2024F00898.md): Floor Support · corroded · Aug 8, 2024 · N956SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON SEVERAL AREAS OF THE RH PRESSURE FLOOR SILL FS 424.00, FS449.85, FS473.15, FS484.00, FS513.00, FS526.00 (FILED CLOSED) BLENDED CORROSION ON THE RH PRESSURE FLOOR SILL FS 424.00, FS449.85, FS473.15, FS484.00, FS513.00, FS526.0
- [SDR SWIA20240808](https://openairdocs.org/sdr/SWIA20240808.md): Floor Support · corroded · Aug 8, 2024 · N956SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON SEVERAL AREAS OF THE LH PRESSURE FLOOR SILL. FS 409.00+128, FS424.00, FS439.00, FS473.15, 494.00, FS513.00, 548.00. (FILED CLOSED) BLENDED CORROSION ON THE LH PRESSURE FLOOR SILL FS 409.00+128, FS424.00, FS439.00, FS473.15, 49
- [SDR SWIA20240806](https://openairdocs.org/sdr/SWIA20240806.md): Angle · corroded · Aug 6, 2024 · N956SW · Cndair CL6002B19 · Passenger/Crew Doors
  > CORROSION FOUND IN MULTIPLE SPOTS ON THE PASSENGER DOOR ENTRANCE ANGLE JUST ABOVE STINGER 18L (FILED CLOSED) REMOVED AND REPLACED PASSENGER DOOR ENTRANCE ANGLE JUST ABOVE STR 18L WITH REFERENCE TO SRM 51-42-06 AND SRM 51-42-21. COMPLIED WITH TASK CARD 5
- [SDR SWIA2024011800007](https://openairdocs.org/sdr/SWIA2024011800007.md): Wire · loose · Jan 17, 2024 · N956SW · Cndair CL6002B19 · Fire Protection System Wiring
  > L JET OVHT FAIL CAUTION MESSAGE INTERMITTENT. RAN QRH AND IT DID NOT RETURN UNTIL WE WERE PULLING INTO THE GATE. ONLY APPEARED FOR A COUPLE SECONDS EACH TIME. (FLIGHT 5253 FILED CLOSED)INSPECTED LH JET PIPE DETECTION SYSTEM IN REFERENCE TO AMM 26-11-04. WHILE
- [SDR SWIA202266145](https://openairdocs.org/sdr/SWIA202266145.md): None · fluctuates · Jul 23, 2022 · N956SW · Cndair CL6002B19 · Stabilizer Position Indicating
  > D: THIS IS AN **ODI EVENT** - UPPER MGMT /SMOD APPROVAL REQ'D TO RTS THIS A/C AFTER CAMPS COMPLETE / C: MCI / SEE A/C MX LOG'S 956358 & 955518 (FLIGHT 5123 - FILED CLOSED) DID OPERATIONAL CHECK OF THE STAB-TRIM SYSTEM REFERENCING THE APPLICABLE STEPS IN
- [SDR SWIA202158376](https://openairdocs.org/sdr/SWIA202158376.md): Strut · underserviced · May 22, 2021 · N956SW · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > GEAR DISAGREE WARNING MESSAGE AFTER TAKEOFF WITH NOSE DOOR OPEN WARNING MESSAGE. RETURNED TO FIELD (FLIGHT 1395 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 22837592 WITH THE FOLLOWING CORRECTIVE ACTION: "JACKED THE AIRCRAFT OFF THE GROU
- [SDR SWIA202158333](https://openairdocs.org/sdr/SWIA202158333.md): Bracket · damaged · May 2, 2021 · N956SW · Cndair CL6002B19 · Horizontal Stabilizer Miscellaneous Structure
  > RH LOWER HSTA MOTOR CONTROL UNIT MOUNT BRACKET HAS MOUNTING HOLE RIPPED OUT. (C-CHECK RO 5/20/2021) REMOVED AND REPLACED NEW LOWER HORIZONTAL STABILIZER MOTOR CONTROL UNIT MOUNT BRACKET ON RIGHTHAND SIDE IAW CRJ 200 SRM 51-42-06 AND DWG 601R92303 REV-A.
- [SDR SWIA202158332](https://openairdocs.org/sdr/SWIA202158332.md): Channel · cracked · May 1, 2021 · N956SW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > WS RH 53.60 CHANNEL OUTBRD SIDE UPPER INBRD CORNER IS CRACKED. (C-CHECK RO 5/20/2021) REMOVED THE CRACKED OTBD SUPPORT CHANNEL AT RH WS.53.60 AND INSTALLED A NEW SUPPORT CHANNEL REF DWG #601R10203 REV -G, CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-21, AND
- [SDR SWIA202158331](https://openairdocs.org/sdr/SWIA202158331.md): Plate · chafed · Apr 29, 2021 · N956SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 319 RH STRG RH 10 GUSSET PLATE HAS CHAFING DAMAGE UPPER SIDE AS MARKED (C-CHECK RO 5/20/2021) FS 319 RH STRG RH 10 GUSSET PLATE - REMOVED AND REPLACED WITH NEW - REF CRJ200 SRM 51-42-21, DRAWING # 601R38303 REV AR. /.COMPLIED WITH TASK CARD 51-900-1
- [SDR SWIA202158330](https://openairdocs.org/sdr/SWIA202158330.md): Angle · cracked · Apr 25, 2021 · N956SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACKED CLIP AT FS.280 ON LBL9 INBD SIDE (MARKED) (C-CHECK RO 5/20/2021) REMOVED AND INSTALLED A NEW FS.280 CLIP ON LBL9 INBD SIDE REF CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-21 AND DWG # 601R31113 REV -M. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA202158368](https://openairdocs.org/sdr/SWIA202158368.md): Splice · broken · Apr 7, 2021 · N956SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR SPLICE 131MB BROKEN (C-CHECK RO 5/20/2021) REMOVED AND REPLACED PAX DOOR SPLICE SP131MB REF ESPM 30-17-10. OPS TEST GOOD
- [SDR SWIA202158329](https://openairdocs.org/sdr/SWIA202158329.md): Skin · corroded · Apr 7, 2021 · N956SW · Cndair CL6002B19 · Passenger/Crew Doors
  > AFTER REMOVAL OF PAX DOOR INNER SKIN FOUND SERVRE CORROSION ON INTERCOSTAL DD3 (C-CHECK RO 5/20/2021) REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD3 REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21, AND DWG 601R31702 REV-N. PRESSURE CHECK GOOD. COMPLIED
- [SDR SWIA202158328](https://openairdocs.org/sdr/SWIA202158328.md): Floorbeam · dented · Apr 7, 2021 · N956SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RBL 27.00 PRESSURE FLOOR-SUPPORT BEAM CHANNEL HAS DENT LOCATED AT APPROX. FS 461.00 (MARKED). (C-CHECK RO 5/20/2021) REPAIRED THE RBL 27.00 PRESSURE FLOOR-SUPPORT BEAM CHANNEL AT APPROX. FS 461.00 WITH REO 601R-53-41-2921 REV -- DATED 2021-05-17. COMPLI
- [SDR SWIA202158327](https://openairdocs.org/sdr/SWIA202158327.md): Floor Support · corroded · Apr 7, 2021 · N956SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RBL9.00 PRESSURE FLOOR-SUPPORT BEAM CHANNEL BETWEEN FS 409.00+128 TO FS 559.00 HAS APPROX. 71 CORROSION LOCATIONS (MARKED WITH GREASE PENCIL). (C-CHECK RO 5/20/2021) REPAIRED PRESSURE FLOOR SUPPORT BEAM CHANNEL BETWEEN FS409.00+118 TO FS559.00+10 RBL9 I
- [SDR SWIA202158326](https://openairdocs.org/sdr/SWIA202158326.md): Roller · cracked · Apr 7, 2021 · N956SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SUSPECTED CRACK ON ROLLER FAIRLEAD BRACKET ASSY ATTACHED TO RBL36.00 FLOOR BEAM AT FS 484.00 (MARKED) (C-CHECK RO 5/20/2021) REMOVED DEFECT AND INSTALLED REPAIR MATERIAL. REF REO 601R-53-41-059 REV -C DATED 2020-03-11. PRESSURE CHECKS ARE SATISFACTORY.
- [SDR SWIA202158325](https://openairdocs.org/sdr/SWIA202158325.md): Floorbeam · cracked · Apr 7, 2021 · N956SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > SUSPECTED CRACK ON RBL27.00 PRESSURE FLOOR-SUPPORT BEAM CLIP ATTACHED TO ROLLER FAIRLEAD BRACKET ASSY AT FS 484.00 (MARKED) (C-CHECK RO 5/20/2021) REMOVED CRACKED CLIP AND INSTALLED NEW CLIP REF PREVIOUSLY INCORPERATED REO 601R-53-41-059 REV-B DATED 200
- [SDR SWIA202158324](https://openairdocs.org/sdr/SWIA202158324.md): Floorbeam · cracked · Apr 7, 2021 · N956SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > SUSPECTED CRACK ON LBL36.00 FLOOR BEAM TO FLIGHT CONTROL CABLE ROLLER FAIRLEAD BRACKET ASSY CLIP AT FS484.00 (MARKED) (C-CHECK RO 5/20/2021) REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE AT LBL36.00 FS484.00 REF CRJ200 SRM 51-42-21 AND REO 601R-53-41-0
- [SDR SWIA202158323](https://openairdocs.org/sdr/SWIA202158323.md): Floorbeam · cracked · Apr 7, 2021 · N956SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > SUSPECTED CRACK ON LBL9.00 PRESSURE FLOOR-SUPPORT BEAM TIE-CLIP TO CROSS-MEMBER AT FS484.00 (MARKED) (C-CHECK RO 5/20/2021) REMOVED AND INSTALLED NEW CLIP AT FS484 ON LBL9 REF DWG 601R31171 REV-B AND REO 601R-53-41-2908 REV--, DATED 2021-04-23. COMPLIED
- [SDR SWIA202158322](https://openairdocs.org/sdr/SWIA202158322.md): Window Post · cracked · Apr 7, 2021 · N956SW · Cndair CL6002B19 · Fuselage Main, Structure
  > RH WINDSHIELD SIDE POST LOWER SUPPORT STRUCTURE CRACKED (MARKED-OUT OF SCOPE) (C-CHECK RO 5/20/2021) REMOVED AND REPLACED ANGLE REF CRJ200 SRM 51-42-06 & DWG 601R34032 REV -V DATED 2009-04-29. PRESSURE CHECK GOOD REF CRJ200 AMM 21-32-00-863-801. COMPLI
- [SDR SWIA202158321](https://openairdocs.org/sdr/SWIA202158321.md): Window Post · cracked · Apr 7, 2021 · N956SW · Cndair CL6002B19 · Fuselage Main, Structure
  > LH WINDSHIELD SIDE POST LOWER SUPPORT STRUCTURE CRACKED (MARKED-OUT OF SCOPE) (C-CHECK RO 5/20/2021) REPLACED L/H WINDSHIELD SIDE POST LWR ANGLE. REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-11, & DWG 601R34032 REV V. PRESSURE CHECK WAS SATISFACTORY. / S
- [SDR SWIA202158367](https://openairdocs.org/sdr/SWIA202158367.md): Bracket · broken · Apr 6, 2021 · N956SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS.621 BULKHEAD HAS 3EA BROKEN BRACKETS @ APPROX. STRG.13-15 (MARKED) (C-CHECK RO 5/20/2021) REMOVED AND INSTALLED 3 NEW BRACKETS (PN:601R45156-75) ON THE FS.621 BULKHEAD AT APPROX STRG 13R-15R REF CRJ 200 SRM 51-42-06. LEAK CHECK GOOD.
- [SDR SWIA202158360](https://openairdocs.org/sdr/SWIA202158360.md): Anchor Fitting · corroded · Apr 6, 2021 · N956SW · Cndair CL6002B19 · Fuselage Main, Structure
  > * PAX DOOR FORWARD ANCHOR FITTING HARDWARE IS CORRODED. (C-CHECK RO 5/20/2021) REMOVED AND INSTALLED NEW HARDWARE ON PAX DOOR FORWARD ANCHOR FITTING. REF - CRJ 200 AMM 52-11-17-000-803 AND CRJ 200 AMM 52-11-17-400-803. / TUC8619 DUE: 10/31/2021 / 6 EACH
- [SDR SWIA202158359](https://openairdocs.org/sdr/SWIA202158359.md): Door Sill · corroded · Apr 6, 2021 · N956SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * PAX DOOR SILL FORWARD AND AFT HANDRAIL CUPS ( CLEATS) HAVE CORROSION. (C-CHECK RO 5/20/2021) REMOVED CORROSION ON THE PAX DOOR SILL FWD AND AFT HANDRAIL CUPS REF CRJ 200 SRM 51-21-06 FOUND TO BE OUT OF LIMITS. REPLACED THE FWD AND AFT PAX DOOR SILL H
- [SDR SWIA202158320](https://openairdocs.org/sdr/SWIA202158320.md): Hinge · gouged · Apr 6, 2021 · N956SW · Cndair CL6002B19 · Fuselage, Door Hinge
  > PAX DOOR HINGE ON FUSELAGE SIDE HAS SEVERAL WORN/EGG SHAPED LUG HOLES, ON THE FWD/AFT ENDS AND FLAT 27 IS GOUGED (MARKED) (C-CHECK RO 5/20/2021) REPLACED PAX DOOR HINGE (FUSELAGE SIDE) REF CRJ200 SRM 53-21-23 AND REO 601R-53-21-656 REV -A DATED 2017-03
- [SDR SWIA202158319](https://openairdocs.org/sdr/SWIA202158319.md): Stiffener · cracked · Apr 6, 2021 · N956SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS409.00+128 PRESSURE BULKHEAD LBL 27 SUPPORT POST CRACKED AT BOTTOM INNER (MARKED - OUT OF SCOPE) (C-CHECK RO 5/20/2021) REMOVED AND INSTALLED A NEW FS.409+128 LBL 27 SUPPORT POST REF REO 601R-53-41-2909 REV -- DATED 2021-05-05 AND DWG #601R32208 REV
- [SDR SWIA202158318](https://openairdocs.org/sdr/SWIA202158318.md): Door Frame · cracked · Apr 6, 2021 · N956SW · Cndair CL6002B19 · Fuselage Main, Structure
  > * CREW ESCAPE HATRCH SURROUND, ( STRUCTURAL) DIAPHRAM AT APPROX. FS270.10 AND LBL 11.160 HAS POSSIBLE CRACK. MARKED. (C-CHECK RO 5/20/2021) REMOVED AND REPLACED CREW ESCAPE HATCH SURROUND STRUCTURAL DIAPHRAM REF CRJ200 SRM 51-42-06, DWG# 601R33048 REV-
- [SDR SWIA202158317](https://openairdocs.org/sdr/SWIA202158317.md): Angle · corroded · Apr 6, 2021 · N956SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * PAX DOOR UPPER SILL ANGLE IS CORRODED AT THE FORWARD END. APPROX FS 310.00. (C-CHECK RO 5/20/2021) REMOVED AND REPLACED WITH NEW - BRACKET ATTACHED TO THE PAX DOOR UPPER SILL ANGLE AT/ABOUT FS310.00. REF CRJ200 SRM 51-42-06. BOMBARDIER DWG # 601R31527
- [SDR SWIA202158316](https://openairdocs.org/sdr/SWIA202158316.md): Angle · corroded · Apr 6, 2021 · N956SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > * GALLEY SERVICE DOOR LOWER SILL ANGLE IS CORRDED AROUND FORWARD STOP FITTING. (C-CHECK RO 5/20/2021) REPLACED GALLEY SERVICE DOOR LOWER SILL ANGLE PN# 601R38303-253. REF BOMBARDIER DWG 601R38303 REV-AR, AND DWG 601R38301 REV-AD, CRJ-200 SRM 51-42-06, S
- [SDR SWIA202158366](https://openairdocs.org/sdr/SWIA202158366.md): Stop Fitting · chafed · Apr 5, 2021 · N956SW · Cndair CL6002B19 · Fuselage Main, Structure
  > *CARGO DOOR SURROUND TOP AFT STOP FITTING CHAFFED/WORN (MARKED) (C-CHECK RO 5/20/2021) REPLACED CARGO DOOR TOP AFT FITTING REF CRJ 200 SRM 51-41-02 TUC 4200 CAL DUE 9 -30 -2021
- [SDR SWIA202158365](https://openairdocs.org/sdr/SWIA202158365.md): Stop Fitting · chafed · Apr 5, 2021 · N956SW · Cndair CL6002B19 · Fuselage Main, Structure
  > *CARGO DOOR SURROUND TOP FWD STOP FITTING CHAFFED/WORN (MARKED) (C-CHECK RO 5/20/2021) REPLACED CARGO DOOR TOP FORWARD FITTING REF CRJ 200 SRM 51-41-02 TUC 4200 CAL DUE 9- 30 -2021
- [SDR SWIA202158364](https://openairdocs.org/sdr/SWIA202158364.md): Stop Fitting · chafed · Apr 5, 2021 · N956SW · Cndair CL6002B19 · Fuselage Main, Structure
  > *CARGO DOOR SURROUND AFT CROTCH STOP FITTING CHAFFED/WORN (MARKED) (C-CHECK RO 5/20/2021) BLENDED CARGO DOOR SURROUND AFT CROTCH STOP FITTING REF CRJ200 SRM 51-12-00. FOUND OUT OF LIMITS. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 601R-53-61-7637 REV-
- [SDR SWIA202158363](https://openairdocs.org/sdr/SWIA202158363.md): Stop Fitting · chafed · Apr 5, 2021 · N956SW · Cndair CL6002B19 · Fuselage Main, Structure
  > *CARGO DOOR SURROUND FWD CROTCH STOP FITTING CHAFFED/WORN (MARKED) (C-CHECK RO 5/20/2021) REMOVED AND REPLACED CARGO DOOR SURROUND FWD CROTCH STOP FITTING IAW REO 601R-53-61-7637 REV-- DATED 2021-04-20, & DWG 600-35072 REV -C, OPS TEST GOOD AT THIS TIM
- [SDR SWIA202158362](https://openairdocs.org/sdr/SWIA202158362.md): Stop Fitting · chafed · Apr 5, 2021 · N956SW · Cndair CL6002B19 · Fuselage Main, Structure
  > *CARGO DOOR SURROUND FWD LWR STOP FITTING CHAFFED/WORN (MARKED) (C-CHECK RO 5/20/2021) REMOVED AND REPLACED CARGO DOOR SURROUND FWD LWR STOP FITTING IAW REO 601R-53-61-7637 REV-- DATED 2021-04-20

Next page: https://openairdocs.org/aircraft/N956SW/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 = 'N956SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N956SW/reports

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