# Service difficulty reports: N944SW

A list on [N944SW](https://openairdocs.org/aircraft/N944SW.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 · 212 reports

- [SDR SWIA2026101377605](https://openairdocs.org/sdr/SWIA2026101377605.md): Windshield · cracked · Oct 13, 2026 · N944SW · Cndair CL6002B19 · Flight Compartment Windows
  > RIGHT WINDSHIELD CRACKED DURING FLIGHT, RT WINDSHIELD HEAT CAUTION CAME ON WITH IT. FLIGHT 5942. REMOVED AND REPLACED FO WINDSHIELD IAW AMM 56-11-01 OPS CHECKS GOOD
- [SDR SWIA2026040875677](https://openairdocs.org/sdr/SWIA2026040875677.md): Landing Gear · warning message · Apr 7, 2026 · N944SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE WARNING MESSAGE ON DEPARTURE, RIGHT MAIN GEAR AFFECTED. WARNING MESSAGE CLEARED BY QRH WITH GEAR INDICATING DOWN AND THREE GREEN, FLIGHT COMPLETED WITH GEAR EXTENDED AT OR BELOW 200KIAS WITH NO FURTHER ABNORMALITIES. (FLIGHT 5323) COMPLIED WIT
- [SDR SWIA2026021575293](https://openairdocs.org/sdr/SWIA2026021575293.md): Skin · dented · Feb 15, 2026 · N944SW · Cndair CL6002B19 · Passenger/Crew Doors
  > TRANSFER FROM EAML 1821768: REF EAML 1821319 FOR MCD DENT IN OUTER SKIN MEASURING 3.85" L X 2.75" W X 0.130" D (W/D = 21) AND IS BEYOND LIMITS IN REF TO CRJ 200 SRM 52-00-31FERRY DISPOSITION REO 601R-52-11-3081 (FLIGHT 5132) COMPLIED WITH PAX DOOR DENT REPA
- [SDR SWI2025F01863](https://openairdocs.org/sdr/SWI2025F01863.md): Bulkhead Web · gouged · Oct 27, 2025 · N944SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND FS 280.00 RH BULKHEAD CHANNEL GOUGED BETWEEN WL 91.70 & WL 97.80 AND AT RBL 11.05 (C-CHECK RO 12/19/2025)COMPLIED WITH REO 601R-53-11-4035 REV-- 2025-12-07 AND REPAIRED DAMAGE TOFS 280.00 RH BULKHEAD CHANNEL BETWEEN WL 91.70 & WL 97.80 AND AT RBL 11.0.
- [SDR SWIA202512221027](https://openairdocs.org/sdr/SWIA202512221027.md): Bulkhead Web · damaged · Oct 27, 2025 · N944SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND FS 280.00 RH BULKHEAD WEB DAMAGED BETWEEN WL 91.70 & WL 97.80 AND AT RBL 11.05. COMPLIED WITH REO 601R-53-11-4035 REV-- 2025-12-07 AND REPAIRED DAMAGE TO FS 280.00 RH BULKHEAD WEB DAMAGED BETWEEN WL 91.70 & WL 97.80 AND AT RBL 11.05. REFERENCE CP 31122
- [SDR SWIA202512221004](https://openairdocs.org/sdr/SWIA202512221004.md): Frame · cracked · Oct 4, 2025 · N944SW · Cndair CL6002B19 · Fuselage Main, Frame
  > CRACK IN FLANGE AT FS589 STR26R-25R INBOARD MOST FASTENER FORMED DURING INSTALLATION OF RIVETS. (C-CHECK RO 12/19/2025)PERFORMED REPAIR TO FS589.00 FRAME SECTOR LOWER FLANGE BETWEEN STR25R-STR26R WITH REFERENCE TO REO 601R-53-61-8396 REV "--" DATED 2025-10-17
- [SDR SWI2025F01862](https://openairdocs.org/sdr/SWI2025F01862.md): Floor Support · corroded · Oct 3, 2025 · N944SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > EXFOLIATING CORROSION FOUND ON RH PRESSURE FLOOR SILL STRAP AT FS559.00, WL73.00 BETWEEN RBL36.00 AND RBL45.00. REMOVED AND REPLACED THE RH PRESSURE FLOOR SILL STRAP AT FS559.00, WL73.00 BETWEEN RBL36.00 AND RBL45.00 IN REFERENCE WITH THE SRM 53-41-43 AND SRM
- [SDR SWIA202512221003](https://openairdocs.org/sdr/SWIA202512221003.md): Floor Support · corroded · Oct 3, 2025 · N944SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING INSPECTION AND CORROSION REMOVAL OF THE LH PRESSURE FLOOR SILL ASSY, FOUND 2 CRACKED NUTPLATE HOLES ON LH PRESSURE FLOOR SILL ASSY APPROX. FS 449.85 - FS 461.50 IN BETWEEN LBL 36.00 - 45.00. (C-CHECK RO 12/19/2025)PERFORMED REPAIR OF LH PRESSURE FLOOR
- [SDR SWI2025F01854](https://openairdocs.org/sdr/SWI2025F01854.md): Tie Down · no discrepancy · Oct 2, 2025 · N944SW · Cndair CL6002B19 · Standard Practices/Structures
  > REMOVED AFT CARGO TIE DOWN SUPPORT ANGLES BETWEEN FS605 - FS621 (ITEMS 9 & 10 SRM 53-61-43) TO FOM. INSTALLED AFT CARGO TIE DOWN SUPPORT ANGLES BETWEEN FS605 - FS621 (ITEMS 9 & 10 SRM 53-61-43) WITH REFERENCE TO SRM 51-42-06 AND SRM 51-42-21. COMPLIED WITH
- [SDR SWI2025F01853](https://openairdocs.org/sdr/SWI2025F01853.md): Tie Down · no discrepancy · Oct 2, 2025 · N944SW · Cndair CL6002B19 · Standard Practices/Structures
  > REMOVED CENTER CARGO TIE DOWN SUPPORT ANGLES BETWEEN FS589 - FS605 (ITEMS 6 & 8 SRM 53-61-43) TO FOM INSTALLED CENTER CARGO TIE DOWN SUPPORT ANGLES BETWEEN FS589 - FS605 (ITEMS 6 & 8 SRM 53-61-43) WITH REFERENCE TO SRM 51-42-06 AND SRM 51-42-21. COMPLIED WITH
- [SDR SWIA20251222002](https://openairdocs.org/sdr/SWIA20251222002.md): Drain Valve · corroded · Oct 2, 2025 · N944SW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > LH WING WATER DRAIN VALVE COVER FOOTPRINT ADJACENT TO STANDBY BOOST PUMP HAS CORROSION ON WING PLANK. (C-CHECK RO 12/19/2025)PERFORMED REPAIR FOR CORROSION DAMAGE TO LHS LOWER WING PLANK AROUND ELECTRIC BOOST PUMP WATER DRAIN CUTOUT AT BL5.00 BTWN STR 5 - STR
- [SDR SWIA202512220927](https://openairdocs.org/sdr/SWIA202512220927.md): Frame · corroded · Sep 27, 2025 · N944SW · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION BEYOND ALLOWABLE LIMITS AT FS589 BETWEEN STR26L-26R REMOVED RIVETS AS NEEDED AT FS 589.00 FROM STR26L- STR26R IAW SRM 51-42-06. BLENDED CORROSION AT FS 589.00 FROM STR26L- STR26R IAW SRM 51-21-06. PERFORMED UT REMAINING THICKNESS MEASUREMENT IAW NDT
- [SDR SWI2025F01857](https://openairdocs.org/sdr/SWI2025F01857.md): Frame · chafed · Sep 18, 2025 · N944SW · Cndair CL6002B19 · Fuselage Main, Frame
  > IN THE AFT EQUIPMENT BAY, ON FS718.00, BELOW STGR 17 THERE IS MINOR CHAFE DAMAGE ON THE FRAME. REPAIRED INNER FLANGE OF FRAME FS718.00 BETWEEN STGR 16R - STGR 17R WITH REFERENCE TO REO 601R-53-61-8387 REV-. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA202512220918](https://openairdocs.org/sdr/SWIA202512220918.md): Bracket · cracked · Sep 18, 2025 · N944SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR FWD TRACK BRACKET CRACKED AT FS574 AT STRG16L (MARKED WITH STEAMER) (C-CHECK RO 12/19/2025)REMOVED AND REPLACED CARGO DOOR FWD TRACK BRACKET AT FS574.00 AND STGR 16L WITH REFERENCE TO SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLET
- [SDR SWI2025F01861](https://openairdocs.org/sdr/SWI2025F01861.md): Tie Down · corroded · Sep 17, 2025 · N944SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CORROSION AND CRACK FOUND ON MIDDLE CARGO TIE DOWN AT FS 605. REMOVED AND REPLACED MIDDLE CARGO TIE DOWN PLATE AT FS 605.00 WITH REFERENCE TO SRM 51-42-06 AND SRM 51-42-21. C
- [SDR SWI2025F01860](https://openairdocs.org/sdr/SWI2025F01860.md): Tie Down · corroded · Sep 17, 2025 · N944SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CORROSION FOUND ON AFT CARGO TIE DOWN AT FS 621 REMOVED AND REPLACED AFT CARGO TIE DOWN PLATE AT FS 621.00 WITH REFERENCE TO SRM 51-42-06 AND SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA202512220917](https://openairdocs.org/sdr/SWIA202512220917.md): Door Sill · corroded · Sep 17, 2025 · N944SW · Cndair CL6002B19 · Fuselage Main, Structure
  > CORROSION FOUND ALONG PAX DOOR SILL FS319 TO FS349 (C-CHECK RO 12/19/2025)REMOVED AND REPLACED THE PASSENGER DOOR SILL ANGLE IN REFRERENCE WITH THE CRJ-200 SRM 53-21-23, SRM 51-42-06, SRM 51-42-13, AND SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY. CO
- [SDR SWI2025F01858](https://openairdocs.org/sdr/SWI2025F01858.md): Scroll · corroded · Sep 16, 2025 · N944SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > 6" OF MINOR SURFACE CORROSION NOTED UNDER CARGO DOOR SCUFF PLATE LOWER EDGE AT FS 605.00 (C-CHECK RO 12/19/2025)UPON INVESTIGATION FOUND THE CORROSION TO BE 12.7" L X 1.5" W. BLENDED MINOR SURFACE CORROSION NOTED UNDER CARGO DOOR SCUFF PLATE LOWER EDGE AT FS
- [SDR SWIA202512220916](https://openairdocs.org/sdr/SWIA202512220916.md): Skin · dented · Sep 16, 2025 · N944SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > 1 DENT LOCATED APRROXIMATELY 6" AFT OF FS 654.50 BETWEEN STRINGERS 22L AND 23L. (C-CHECK RO 12/19/2025)COMPLIED WITH REO 601R-53-61-8393 REV "--" DATED 2025-10-16. REPAIR FOR DENT AND GOUGE DAMAGE TO FUSELAGE SKIN BETWEEN FS654.50 - FS672.20 AND STR21L - STR2
- [SDR SWI2025F01859](https://openairdocs.org/sdr/SWI2025F01859.md): Floor Support · corroded · Sep 7, 2025 · N944SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND MULTIPLE SPOTS OF CORROSION ON RT PRESSURE FLOOR SILL MEMEBER FROM FS 409.00 +128 TO FS 559.00. MULTIPLE SPOTS OF CORROSION ARE ON AREAS THAT WERE PREVIOUSLY BLENDED OUT, BLENDED CORROSION ON RH PRESSURE FLOOR SILL ASSY WL73.00 BETWEEN FS409 + 128 TO
- [SDR SWIA2025122200907](https://openairdocs.org/sdr/SWIA2025122200907.md): Floor Support · corroded · Sep 7, 2025 · N944SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND MULTIPLE SPOTS OF CORROSION ON LH PRESSURE FLOOR SILL MEMEBER FROM FS 409.00 +128 TO FS 559.00. MULTIPLE SPOTS OF CORROSION ARE ON AREAS THAT WERE PREVIOUSLY BLENDED OUT, BLENDED CORROSION ON LH PRESSURE FLOOR SILL ASSY WL73.00 BETWEEN FS409 + 128 TO FS
- [SDR SWIA2025122200906](https://openairdocs.org/sdr/SWIA2025122200906.md): Skin · gouged · Sep 6, 2025 · N944SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > EXTERNAL SKIN OF BAGGAGE BAY DOOR GOUGED AROUND HANDLE ASSYMBLY. (C-CHECK RO 12/19/2025)UPON FURTHER INSPECTION FOUND ONLY CARGO DOOR HANDLE HOUSING TO BE GOUGED. REMOVED AND REPLACED CARGO DOOR HANDLE HOUSING WITH REFERENCE TO SRM 51-42-21. COMPLIED WITH
- [SDR SWI2025F01856](https://openairdocs.org/sdr/SWI2025F01856.md): Door · gouged · Jul 15, 2025 · N944SW · Cndair CL6002B19 · Service Doors
  > FORWARD, UPPER CORNER OF SERVICE DOOR SURROUND FOUND TO BE DAMGED. BLENDED GOUGE AREA AT UPPER FWD CORNER OF THE FUSE SERVICE DOOR APERTURE MEASURING 0.75" L X 0.187"W X 0.045" MAX D, DAMAGE LOCATED AT FS319.70, S9R-S10R. COMPLIED WITH REO601R-53-21-3606, REV
- [SDR SWI2025F01855](https://openairdocs.org/sdr/SWI2025F01855.md): Door · damaged · Jul 15, 2025 · N944SW · Cndair CL6002B19 · Service Doors
  > FORWARD, UPPER CORNER OF SERVICE DOOR FOUND TO BE DAMAGED. DAMAGE DEFORMED AREA ON OUTER DOUBLER LOCATED BETWEEN FS320.680-FS328.100 AT UPPER FORWARD CORNER OF SERVICE DOOR, AFTER DRESS BACK OUTER DOUBLER HAS A 0.035" MAX DEFLECTION REMAINING WITH MATING OUTER
- [SDR SWIA202512220715](https://openairdocs.org/sdr/SWIA202512220715.md): Skin · dented · Jul 15, 2025 · N944SW · Cndair CL6002B19 · Rudder, Plate/Skin
  > RUDDER HAS A DENT LOCATED AT APPROXIMATELY RS69.00.25" FROM RIB 4. COMPLIED WITH TEMP REPAIR PER REO 601R-55-41-290 DATED 2024-06-05. TEMORARY DISPOSITION FOR DENT TO RH SKIN OF RUDDER BETWEEN RS66.758 AND RS 72.788 DUE TO HAIL. IS VALID FOR 3275 FLIGHT HOUR
- [SDR SWIA20250603](https://openairdocs.org/sdr/SWIA20250603.md): A/C Pack · warning message · Jun 3, 2025 · N944SW · Cndair CL6002B19 · Cabin Cooling System
  > RIGHT PACK FAILED IN FLIGHT CAUSING CABIN ALT MESSAGE (FLIGHT 5060 - FILED OPEN)REMOVED AND REPLACED RH AIR CYCLE MACHINE IN REFERENCE WITH CRJ 200 AMM 21-51-10. OPS CK GOOD AT THIS TIME.
- [SDR SWIA202406100001](https://openairdocs.org/sdr/SWIA202406100001.md): Unknown · damaged · Jun 1, 2024 · N944SW · Cndair CL6002B19 · Standard Practices/Structures
  > CLASSIFICATION OF DAMAGE REPAIR MAJOR/MINOR REUIRED PER GMM 3.25 AND 3.26 (FILED CLOSED)THE DOCUMENTED DAMAGE WILL REQUIRED MAJOR REPAIR IAW GMM 3.26THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA202406030601](https://openairdocs.org/sdr/SWIA202406030601.md): Unknown · unknown · Jun 1, 2024 · N944SW · Cndair CL6002B19 · Standard Practices/Structures
  > CLASSIFICATION OF DAMAGE REPAIR MAJOR/MINOR REUIRED PER GMM 3.25 AND 3.26 (FILED OPEN)THE DOCUMENTED DAMAGE WILL REQUIRED MAJOR REPAIR IAW GMM 3.26THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA20240501430](https://openairdocs.org/sdr/SWIA20240501430.md): Warning Message · false activation · Apr 30, 2024 · N944SW · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > WING OVHT WARNING ON TAKEOFF. QRH RESOLVED. (FLIGHT 5348 FILED CLOSED)PERFORMED OPS CHECK OF THE WING CONTROL AND INDICATION SYSTEM IN REFERENCE WITH AMM 30-12-00. OPS CHECK GOOD AT THIS TIME
- [SDR SWIA2024041700014](https://openairdocs.org/sdr/SWIA2024041700014.md): Proximity Sensor · damaged · Apr 14, 2024 · N944SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > NOSE GEAR DOOR WARNING MESSAGE PAIRED WITH GEAR DISAGREE WARNING MESSAGE. NOSE GEAR SHOWING DOWN. RAN QRH, CLEARED BOTH MESSAGES GEAR REMAINED DOWN. (FLIGHT 4636) ARRIVED AT A/C AND FOUND NLG OLEO CENTERED/EXTENDED PROX SENSOR AND ITS MOUNTING BRACKET DAMAGED
- [SDR SWIA202404150004](https://openairdocs.org/sdr/SWIA202404150004.md): Proximity Sensor · damaged · Apr 14, 2024 · N944SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > NOSE GEAR DOOR WARNING MESSAGE PAIRED WITH GEAR DISAGREE WARNING MESSAGE. NOSE GEAR SHOWING DOWN. RAN QRH, CLEARED BOTH MESSAGES GEAR REMAINED DOWN. (FLIGHT 4636 FILED OPEN)ARRIVED AT A/C AND FOUND NLG OLEO CENTERED/EXTENDED PROX SENSOR AND ITS MOUNTING BRACKE
- [SDR SWIA20230923](https://openairdocs.org/sdr/SWIA20230923.md): Unknown · warning message · Sep 23, 2023 · N944SW · Cndair CL6002B19 · Landing Gear System
  > GEAR DISAGREE WARN CLIMBING THROUGH 20,000. EXTINGUISHED BEFORE QRH WAS RUN. CAME BACK ABOUT 2 MINUTES LATER. RAN INITIAL QRH BUT MESSAGE DID NOT EXIT EXTINGUISH. HAD TO GET LOWER TO SLOW TO QRH REQUESTED AIRSPEED. MESSAGE EXTINGUISHED BELOW 16,000. NORMAL LA
- [SDR SWIA2023083101](https://openairdocs.org/sdr/SWIA2023083101.md): Unknown · smoke · Aug 30, 2023 · N944SW · Cndair CL6002B19 · Airborne Auxiliary Power Unit (APU) System
  > DURING APU TO ENGINE BLEED SWAP ON DEPARTURE, A SULFUR ODOR WAS NOTICED ALONG WITH A SMALL PLUME OF SMOKE OUT OF THE FO SIDE LARGE GASPER. SMELL AND ODOR CLEARED IMMEDIATELY AND DID NOT RETURN. DID NOT RESTART APU OR SWAP BLEEDS ON ARRIVAL. PACKS WERE OPERATIN
- [SDR SWIA202266318](https://openairdocs.org/sdr/SWIA202266318.md): None · elongated · Jul 19, 2022 · N944SW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > RH FLOOR SILL HAS ELONGATED HOLE FWD OF FS295.00 (C-CHECK RO 8/15/2022) COMPLIED WITH REO REPAIR 601R-53-21-3558 REV--, DATED: 2022-08-01. TASK CARD 51-900-1003-SKY COMPLIED WITH.
- [SDR SWIA202266317](https://openairdocs.org/sdr/SWIA202266317.md): None · elongated · Jun 29, 2022 · N944SW · Cndair CL6002B19 · Doors
  > ON REMOVAL, FOUND OVERSIZE ELONGATED HOLE ON AFT PULL IN LEVER BEARING SUPPORT FITTING. (C-CHECK RO 8/15/2022) COMPLIED WITH REPAIR REF. REO 601R-52-11-2930 REV--, DATED: 2022-08-01, ALL STEPS COMPLIED WITH. TASK CARD 51-900-1003-SKY COMPLIED WITH.
- [SDR SWIA202266316](https://openairdocs.org/sdr/SWIA202266316.md): None · corroded · Jun 29, 2022 · N944SW · Cndair CL6002B19 · Doors
  > PAX DOOR FWD SUPPORT ANGLE FOR FWD FORMER IS CORRODED. (C-CHECK RO 8/15/2022) REMOVED BAD ANGLE REF CRJ200 SRM 51-42-06 AND REF CRJ200 SRM 51-42-21 AND ORDERED AND RECEIVED REPLACEMENT FASTENERS AND INSTALLED REPLACEMENT ANGLE WITH REPLACEMENT FASTENERS
- [SDR SWIA202266315](https://openairdocs.org/sdr/SWIA202266315.md): None · corroded · Jun 28, 2022 · N944SW · Cndair CL6002B19 · Doors
  > PAX DOOR INTERNAL STRUCTURE FWD UPPER INTERCOASTAL DD7A IS CORRODED. MARKED (C-CHECK RO 8/15/2022) REMOVED BAD INTERCOASTAL REF CRJ200 SRM 51-42-06 AND ORDERED AND RECEIVED REPLACEMENT FASTENERS AND INSTALLED REPLACEMENT INTERCOASTAL WITH REPLACEMENT FA
- [SDR SWIA202266314](https://openairdocs.org/sdr/SWIA202266314.md): None · bent · Jun 27, 2022 · N944SW · Cndair CL6002B19 · Doors
  > PAX DOOR INTERNAL STRUCTURE AFT LOWER INTERCOASTAL DD1 IS BENT. MARKED (C-CHECK RO 8/15/2022) REMOVED AND REPLACED BENT AFT LOWER INTERCOASTAL DD1 WITH A NEW SERVICEABLE UNIT REF CRJ200 SRM 51-42-06 AND DWG 601R31702 REV N. LEAK CHECK GOOD. SEE CONTINUA
- [SDR SWIA202266313](https://openairdocs.org/sdr/SWIA202266313.md): None · bent · Jun 27, 2022 · N944SW · Cndair CL6002B19 · Doors
  > PAX DOOR INTERNAL STRUCTURE FWD LOWER INTERCOASTAL IS BENT. MARKED (C-CHECK RO 8/15/2022) REMOVED AND REPLACED BENT FWD LOWER INTERCOASTAL WITH A NEW SERVICEABLE UNIT P/N 600-31902-259 REF CRJ200 SRM 51-42-06 AND REF DWG. 601R31702 REV N. LEAK CHECK GOO
- [SDR SWIA202266312](https://openairdocs.org/sdr/SWIA202266312.md): None · bent · Jun 27, 2022 · N944SW · Cndair CL6002B19 · Doors
  > PAX DOOR INTERNAL STRUCTURE FWD UPPER INTERCOASTAL DD7 IS BENT. MARKED (C-CHECK RO 8/15/2022) REMOVED AND REPLACED BENT FWD UPPER INTERCOASTAL DD7 WITH A NEW SERVICEABLE UNIT REF CRJ200 SRM 51-42-06 AND DWG 601R31702 REV N. LEAK CHECK GOOD. SEE CONTINUA
- [SDR SWIA202266311](https://openairdocs.org/sdr/SWIA202266311.md): None · bent · Jun 27, 2022 · N944SW · Cndair CL6002B19 · Doors
  > PAX DOOR INTERNAL STRUCTURE AFT UPPER INTERCOASTAL DD7 IS BENT. MARKED (C-CHECK RO 8/15/2022) REMOVED AND REPLACED AFT UPPER INTERCOASTAL DD7 AT THE PAX DOOR INTERNAL STRUCTURE REF CRJ200 SRM 51-42-06 AND REF DWG. 601R31702 REV N. LEAK CHECK GOOD. SEE C
- [SDR SWIA202266310](https://openairdocs.org/sdr/SWIA202266310.md): None · corroded · Jun 23, 2022 · N944SW · Cndair CL6002B19 · Doors
  > CORROSION ON PAX DOOR FWD FORMER INSIDE UNDER PANEL 832HL. (C-CHECK RO 8/15/2022) REMOVED FWD FORMER FROM PASSENGER DOOR UNDER PANEL 832 HL. REF CRJ200 SRM 51-42-21 AND REF CRJ200 SRM 51-42-06 AND ORDERED AND RECEIVED REPLACEMENT FASTENERS AND INSTALLE
- [SDR SWIA202266309](https://openairdocs.org/sdr/SWIA202266309.md): None · corroded · Jun 22, 2022 · N944SW · Cndair CL6002B19 · Fuselage Structure (General)
  > *RH PRESSURE FLOOR SILL MEMBER FROM FS409.0+128-FS559 HAS MULTIPLE AREAS OF CORROSION (MARKED) (C-CHECK RO 8/15/2022) REMOVED CORROSION ON RH PRESSURE FLOOR SILL MEMBER (15 LOCATIONS) FROM FS409+128 TO FS559 AND FOUND THEM WITHIN LIMITS REF. REO 601R-53
- [SDR SWIA202266308](https://openairdocs.org/sdr/SWIA202266308.md): None · corroded · Jun 22, 2022 · N944SW · Cndair CL6002B19 · Fuselage Structure (General)
  > *LH PRESSURE FLOOR SILL MEMBER FROM FS409.0+128-FS559 HAS MULTIPLE AREAS OF CORROSION (MARKED) (C-CHECK RO 8/15/2022) REMOVED CORROSION ON LH PRESSURE FLOOR SILL MEMBER FROM FS409+128 TO FS559 ON MULTIPLE AREAS OF CORROSION AND FOUND THEM WITHIN LIMITS
- [SDR SWIA202266307](https://openairdocs.org/sdr/SWIA202266307.md): None · corroded · Jun 21, 2022 · N944SW · Cndair CL6002B19 · Doors
  > CORROSION ON PAX DOOR FRAME AFT SIDE UNDER PNL. 832 GR. (MARKED) (C-CHECK RO 8/15/2022) REMOVED AFT FORMER FROM PASSENGER DOOR. REF: CRJ200 SRM 51-42-21 AND CRJ200 SRM 51-42-06 AND ORDERED AND RECEIVED REPLACEMENT FASTENERS AND INSTALLED REPLACEMENT FOR
- [SDR SWIA202266306](https://openairdocs.org/sdr/SWIA202266306.md): None · corroded · Jun 20, 2022 · N944SW · Cndair CL6002B19 · Elevator Tab, Attach Fittings
  > R/H ELEVATOR FITTING LOCATED AT E.S. 16.520 HAS CORROSION INSIDE BORE FOR BEARING. (C-CHECK RO 8/15/2022) REMOVED AND REPLACED RH ELEVATOR FITTING ASSEMBLY P/N 600-24043-1 LOCATED AT E.S. 16.520. REF CRJ 200 SRM 51-42-06, SRM 51-42-21 AND BOMBARDIER DWG
- [SDR SWIA202266305](https://openairdocs.org/sdr/SWIA202266305.md): None · corroded · Jun 19, 2022 · N944SW · Cndair CL6002B19 · Elevator Tab, Attach Fittings
  > L/H ELEVATOR FITTING LOCATED @ BL15.25 HAS CORROSION INSIDE THE BORE AND WILL NEED TO BE REPLACED. (C-CHECK RO 8/15/2022) INSTALLED NEW L/H ELEVATOR FITTING (PN 600-24043-1) LOCATED @ BL 15.25 REF CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-21 AND DWG# 601R
- [SDR SWIA202266304](https://openairdocs.org/sdr/SWIA202266304.md): None · dented · Jun 18, 2022 · N944SW · Cndair CL6002B19 · Fuselage Structure (General)
  > *EVALUATE DENTS ON EXTERNAL SKIN BETWEEN FS 589.00 - 605.00, STGR 23L - 24L (C-CHECK RO 8/15/2022) / EVALUATED DENTS ON EXTERNAL SKIN BETWEEN FS 589.00 - 605.00, STGR 23L - 24L. FOUND TO BE OUT OF LIMIT. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED R
- [SDR SWIA202266303](https://openairdocs.org/sdr/SWIA202266303.md): None · cracked · Jun 16, 2022 · N944SW · Cndair CL6002B19 · Fuselage Main, Keel
  > *FS 625 STR 14R CLIP CRACKED (C-CHECK RO 8/15/2022) REMOVED AND REPLACED INTERCOSTAL CLIP AT FS625.30 STGR14 P/N 601-35012-52. REF: DRAWING 601-35012 REV -D AND CRJ-200 SRM 51-42-06. SKYWEST TASK CARD 51-900-1003-SKY COMPLIED WITH
- [SDR SWIA202266302](https://openairdocs.org/sdr/SWIA202266302.md): None · chafed · Jun 14, 2022 · N944SW · Cndair CL6002B19 · Ailerons
  > LH WING I/B FLAP VANE HAS CHAFE MARKS X2 (MARKED) (C-CHECK RO 8/15/2022) REMOVED AND REPLACED THE L/H I/B FLAP VANE L/E SKINS AT THE CENTER (601R14303-51S) AND O/B (601R14303-43S) LOCATION REF: CRJ-200 SRM 51-42-13 AND DRAWING 601R14302 REV E. OP CHECK

Next page: https://openairdocs.org/aircraft/N944SW/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 = 'N944SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N944SW/reports

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