# Service difficulty reports: N449SW

A list on [N449SW](https://openairdocs.org/aircraft/N449SW.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 · 239 reports

- [SDR SWIA2026030875432](https://openairdocs.org/sdr/SWIA2026030875432.md): Landing Gear · warning message · Mar 8, 2026 · N449SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE MASTER WARNING AFTER SELECTING LANDING GEAR LEVER UP. LEFT MAIN AND NOSE GEAR SUCCESSFULLY STOWED. RIGHT MAIN GEAR DID NOT COME UP. (FLIGHT 5049) PERFORMED INSPECTION CHECKS OF NOSE AND LEFT UPLOCK TARGETS AND FOUND TO BE ADJUSTED TO CORRECT LI
- [SDR SWIA2026013075421](https://openairdocs.org/sdr/SWIA2026013075421.md): Angle · broken · Jan 30, 2026 · N449SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RBL9 ANGLE AT FS 280.00 BROKEN. REPAIRED RBL9 ANGLE AT FS 280 IAW REO 601R-53-11-4048
- [SDR SWIA2025120375420](https://openairdocs.org/sdr/SWIA2025120375420.md): Skin · cracked · Dec 3, 2025 · N449SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > AFT CARGO DOOR - INTERNAL SKIN HAS A CRACK AND CORROSION. COMPLIED WITH REO: 601R-53-31-441 FOR REPAIR OF AREA
- [SDR SWIA2025112575424](https://openairdocs.org/sdr/SWIA2025112575424.md): Frame · cracked · Nov 25, 2025 · N449SW · Cndair CL6002B19 · Fuselage Main, Frame
  > AFT COMPARTMENT, FRAME FS 640.00 HAS A CRACK STRG 8,9 L/H (C-CHECK RO 03/04/2026)REMOVED AND REPLACED FOR NEW FRAME P/N: 601R350094-1 ON FS 640.00 AFT COMPARTMENT IAW CRJ200 SRM 51-42-06,51-42-20,51-40-11,51-42-06,51-23-00,
- [SDR SWIA2025112575418](https://openairdocs.org/sdr/SWIA2025112575418.md): Angle · cracked · Nov 25, 2025 · N449SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > AFT CARGO DOOR, FWD RAIL, UPPER ANGLE HAS A CRACK (C-CHECK RO 03/04/2026)REPAIRED FWD RAIL UPPER ANGLE FROM AFT CARGO DOOR IAW REO: 601R-53-61-8453
- [SDR SWIA2025112075423](https://openairdocs.org/sdr/SWIA2025112075423.md): Skin · chafed · Nov 20, 2025 · N449SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > AFT CARGO DOOR, EXTERNAL SKIN UPPER SIDE HAS CHAFING/GOUGE REMOVED THE EXISTENT DOUBLER AND REPLACED FOR NEW DOUBLER ON EXTERNAL SKIN UPPER SIDE AFT CARGO DOOR IAW REO: 601R-52-31-440 IAW CRJ200 SRM 51-42-21,51-23-00,51-40-11,51-42-22,51-24-36,51-24-16,51-2
- [SDR SWIA2025081875422](https://openairdocs.org/sdr/SWIA2025081875422.md): Skin · dented · Aug 18, 2025 · N449SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > COMPLY WITH PERMANENT REPAIR ON RA ID: 93923DENT ON RHS FUSELAGE SKIN PANEL BTWN FS185.00 - FS193.00 AND BL0.00 - BL6.10. COMPLIED WITH REO 601R-53-11-3946 NO OTHER DEFECTS NOTED. PERM REPAIR DUE WITH IN 1600 FH. COMPLIED RA93923-REO 601R-53-11-3946 MXCODEID7
- [SDR SWIA2025081875419](https://openairdocs.org/sdr/SWIA2025081875419.md): Skin · damaged · Aug 18, 2025 · N449SW · Cndair CL6002B19 · Ailerons
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA91380-REO 601R-57-21-3841. COMPLY WITH PERMANENT REPAIR ON RA ID: 91380FASTENER HOLE ON LH WING FWD OF AILERON DAMAGED DURING SCREW EXTRACTION. LOCATED JUST SLIGHTLY IB OF WS 314.40 UNDER PANEL 598KT REFERENCE REO 601
- [SDR SWIA202505270021](https://openairdocs.org/sdr/SWIA202505270021.md): Warning Message · illuminated · May 21, 2025 · N449SW · Cndair CL6002B19 · Hydraulic System, Main
  > 5 MINUTES AFTER TAKEOFF HYD 2 LO PRESS CAUTION MESSAGE, ANNUNCIATED, HYDRAULIC SYSTEM TO QUANTITY REPORTED 5%, BOTH HYDRAULIC SYSTEM TWO PUMPS OPERATED FOR 85 MINUTES WHILE QUANTITY WAS LOW BEFORE LANDING. (FLIGHT 5472 - FILED CLOSED)UPON ARRIVAL TO A/C FOUND
- [SDR SWI2025F00653](https://openairdocs.org/sdr/SWI2025F00653.md): Hydraulic System · low pressure · May 21, 2025 · N449SW · Cndair CL6002B19 · Hydraulic Indicating System
  > 5 MINUTES AFTER TAKEOFF HYD 2 LO PRESS CAUTION MESSAGE, ANNUNCIATED, HYDRAULIC SYSTEM TO QUANTITY REPORTED 5%, BOTH HYDRAULIC SYSTEM TWO PUMPS OPERATED FOR 85 MINUTES WHILE QUANTITY WAS LOW BEFORE LANDING. (FLIGHT 5472 - FILED OPEN)THIS IS CURRENTLY A WORK IN
- [SDR SWI2024060700489](https://openairdocs.org/sdr/SWI2024060700489.md): Seat Track · corroded · May 22, 2024 · N449SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED AT LBL 9.00 BETWEEN FS 364.00 AND FS 409.00 (C-CHECK RO 6/6/2024) COMPLIED WITH REO 601R-53-00-764 REV -- DATED 2019-10-11 AND REO 601R-53-00-766 REV -- DATED: 2019-10-17 FOR USE OF THE MCFARLANE SEAT TRACK. REMOVED AND REPLACED THE SEA
- [SDR SWI20240607000488](https://openairdocs.org/sdr/SWI20240607000488.md): Seat Track · corroded · May 22, 2024 · N449SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED AT RBL 9.00 BETWEEN FS 364.00 AND FS 409.00 (C-CHECK RO 6/6/2024) COMPLIED WITH REO 601R-53-00-764 REV -- DATED 2019-10-11 AND REO 601R-53-00-766 REV -- DATED: 2019-10-17 FOR USE OF THE MCFARLANE SEAT TRACK. REMOVED AND REPLACED THE SEA
- [SDR SWIA2024060700522](https://openairdocs.org/sdr/SWIA2024060700522.md): Nut Plate · corroded · May 22, 2024 · N449SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CORROSION AROUND NUT PLATES ON STRAP ASSY THAT RUNS BETWEEN LBL 45.00 AND LBL 27.00 AT FS 559.00 (C-CHECK RO 6/6/2024) REMOVED AND REPLACED STRAP ASSEMBLY THAT RUNS BETWEEN LBL 45.00 AND LBL 27.00 AT FS 559.00 WITH REFERENCE TO SRM 51-42-06 AND SRM 53-41-4
- [SDR SWIA20240516](https://openairdocs.org/sdr/SWIA20240516.md): Window Post · cracked · May 16, 2024 · N449SW · Cndair CL6002B19 · Fuselage Main, Structure
  > WINDSHIELD CENTER POST LOWER FITTING CRACKED ON AFT RIGHT FACE FROM LOWER EDGE TO SECOND/UPPER FASTENER. (C-CHECK RO 6/6/2024) REMOVED AND REPLACED WINDSHIELD CENTER POST LOWER RIGHT FITTING WITH REFERENCE TO SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1
- [SDR SWI2023F00146](https://openairdocs.org/sdr/SWI2023F00146.md): Unknown · damaged · Jun 23, 2023 · N449SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN SPLICE @ FS 755 BETWEEN STR20L AND STR20R, PN 601R210303-1 IS DAMAGED AND REQUIRES REPLACEMENT. (FILED CLOSED)FUSELAGE SKIN SPLICE @ FS 755 BETWEEN STR20L AND STR20R, PN 601R210303-1 REMOVED. FABRICATED NEW SKIN SPLICE SAME AS ORIGINAL PN 601R210
- [SDR SWI2023F00145](https://openairdocs.org/sdr/SWI2023F00145.md): Unknown · bent · Jun 23, 2023 · N449SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STR 26R IS BENT AND REQUIRES REPLACEMENT. (FILED CLOSED)REMOVED DAMAGED STR 26R PN 601R35005-12, AND INTERCOSTAL PN 600-75233-56. LOCATED DRILLED AND INSTALLED NEW STR 26R PN 601R35005-12 AND INTERCOSTAL 600-75233-56 REF CRJ 200 SRM 51-40-11, 51-42-06 AND REO
- [SDR SWIA2023072500623](https://openairdocs.org/sdr/SWIA2023072500623.md): Unknown · bent · Jun 23, 2023 · N449SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STR 26L IS BENT AND REQUIRES REPLACEMENT.(FILED CLOSED)REMOVED DAMAGED STR 26L PN 601R35005-11, AND INTERCOSTAL PN 600-75233-55. LOCATED DRILLED AND INSTALLED NEW STR 26L PN 601R35005-11 AND INTERCOSTAL 600-75233-55 REF CRJ 200 SRM 51-40-11, 51-42-06 AND REO 6
- [SDR SWI2023F00139](https://openairdocs.org/sdr/SWI2023F00139.md): Unknown · damaged · Jun 23, 2023 · N449SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN SPLICE @ FS 755 BETWEEN STR20L AND STR20R, PN 601R210303-1 IS DAMAGED AND REQUIRES REPLACEMENT. (FILED OPEN)FUSELAGE SKIN SPLICE @ FS 755 BETWEEN STR20L AND STR20R, PN 601R210303-1 REMOVED. FABRICATED NEW SKIN SPLICE SAME AS ORIGINAL PN 601R21030
- [SDR SWI2023F00138](https://openairdocs.org/sdr/SWI2023F00138.md): Unknown · bent · Jun 23, 2023 · N449SW · Cndair CL6002B19 · Fuselage Main, Frame
  > STR 26R IS BENT AND REQUIRES REPLACEMENT. (FILED OPEN)REMOVED DAMAGED STR 26R PN 601R35005-12, AND INTERCOSTAL PN 600-75233-56. LOCATED DRILLED AND INSTALLED NEW STR 26R PN 601R35005-12 AND INTERCOSTAL 600-75233-56 REF CRJ 200 SRM 51-40-11, 51-42-06 AND REO 6
- [SDR SWIA2023062403](https://openairdocs.org/sdr/SWIA2023062403.md): Unknown · bent · Jun 23, 2023 · N449SW · Cndair CL6002B19 · Fuselage Main, Frame
  > STR 26L IS BENT AND REQUIRES REPLACEMENT.(FILED OPEN)REMOVED DAMAGED STR 26L PN 601R35005-11, AND INTERCOSTAL PN 600-75233-55. LOCATED DRILLED AND INSTALLED NEW STR 26L PN 601R35005-11 AND INTERCOSTAL 600-75233-55 REF CRJ 200 SRM 51-40-11, 51-42-06 AND REO 601
- [SDR SWIA20230411](https://openairdocs.org/sdr/SWIA20230411.md): Unknown · unknown · Apr 11, 2023 · N449SW · Cndair CL6002B19 · Flight Compartment Windows
  > CA SIDE WINDSHIELD SHATTERED IN CLIMBOUT (FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 26479671 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVED AND REPLACED LH WINDSHIELD PER TASKCARD 56-220-1000-SKY LEAK CHECK GOOD AT THIS TIME"
- [SDR SWIA2023041200001](https://openairdocs.org/sdr/SWIA2023041200001.md): Unknown · unknown · Apr 11, 2023 · N449SW · Cndair CL6002B19 · Flight Compartment Windows
  > CA SIDE WINDSHIELD SHATTERED IN CLIMBOUT (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA202264603](https://openairdocs.org/sdr/SWIA202264603.md): None · odor · Feb 23, 2022 · N449SW · Cndair CL6002B19 · Air Conditioning System
  > DURING APPROACH WITH ENGINE BLEEDS SELECTED, JUST AFTER STARTING APU, NOTICED A STRONG OIL. FA CALLED AND REPORTED THAT SHE AND THE PASSENGERS SMELL A STRONG OILY ODER. FUMES WENT AWAY AFTER DESELECTING 10TH STAGE BLEED AIR. (FLIGHT 4273 - FILED CLOSED) ST
- [SDR SWIA202157826](https://openairdocs.org/sdr/SWIA202157826.md): Frame · damaged · Mar 23, 2021 · N449SW · Cndair CL6002B19 · Fuselage Main, Frame
  > UPPER FRAME SEGMENT AT FS379 (PN 601R32009-41) REQUIRES REPAIR. (C-CHECK RO 4/25/2021) REPAIRED LH UPPER FRAME SEGMENT AT FS 379 PN 601R32009-41 IAW MHIRJ REO 601R-53-21-3414 REV -- DATED 2021-03-23, SKY CARD 51-900-1003-SKY AND ATTACHED FORM M-337 / W
- [SDR SWIA202157825](https://openairdocs.org/sdr/SWIA202157825.md): Stringer · corroded · Mar 23, 2021 · N449SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND TO BE ON MATING SURFACE OF STR23L BETWEEN FS 379 AND 409. REQUIRES SRM REPAIR. (C-CHECK RO 4/25/2021) REMOVED AND INSTALLED NEW STR 23L FROM FS 370 TO 409, IAW CRJ 200 SRM 53-00-03 DATED MAY 10/2015, AND ATTACHED SKYCARD 51-900-1003-SKY
- [SDR SWIA202157872](https://openairdocs.org/sdr/SWIA202157872.md): Attach Angle · corroded · Mar 11, 2021 · N449SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > DISCOVERED CORROSION ON MULTIPLE ATTACHING ANGLES TO THE FRAME AT F.S. 409, STGR 27. (C-CHECK RO 4/25/2021) REMOVED AND INSTALLED SERVICABLE ATTACHING ANGELS IAW CRJ 200 SRM 51-42-06, 51-40-11 REFERENCE CONTINUATION CARD FOR WORK PERFORMED
- [SDR SWIA202157785](https://openairdocs.org/sdr/SWIA202157785.md): Frame · corroded · Mar 8, 2021 · N449SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 589 UPPER FRAME SEGMENT, (PN 601R36025-45) HAS CORROSION AND REQUIRES REPLACEMENT. (C-CHECK RO 4/25/2021) REMOVED AND REPLACED UPPER FRAME AT FS 589 (PN 601R36025-45) IAW CRJ 200 SRM 51-42-06, 51-42-21 AND 51-40-11 REV 38 DATED 10 JULY 2019 AND REFER
- [SDR SWIA202157824](https://openairdocs.org/sdr/SWIA202157824.md): Stringer · bent · Mar 7, 2021 · N449SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > UPON REMOVAL OF STR 27 AT FS 394 TO409. FOUND PART BENT FROM CORROSION FROM FRAME ASSEMBLY. (C-CHECK RO 4/25/2021) REMOVED AND REPLACED STR 27 FROM FS 394 TO FS 409 IAW CRJ 200 SRM 51-40-11, 51-42-06 REV 38 DATED 10 JULY 2019 AND REFERENCED DWG 601R310
- [SDR SWIA202157795](https://openairdocs.org/sdr/SWIA202157795.md): Frame · damaged · Mar 4, 2021 · N449SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME AT F.S. 589.00 REQUIRES REPLACEMENT. (C-CHECK RO 4/25/2021) REMOVED AND INSTALLED SERVICEABLE FS 589.00 FROM STG 20L TO 20R IAW CRJ-200 SRM 51-42-06, SKYWEST STRUCTURAL MAJOR REPAIR TASK 51-900-1003-SKY AND ATTACHED 337. NO WEIGHT CHANGE.
- [SDR SWIA202157822](https://openairdocs.org/sdr/SWIA202157822.md): Former · corroded · Mar 2, 2021 · N449SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FWD FORNER IS CORRODED BETWEEN DD6 AND DD7. (C-CHECK RO 4/25/2021) REMOVED & REPLACED PAX DOOR FWD FORMER P/N 601R318031-5 IAW CRJ 200 SRM 51-40-11, 51-42-06 & 51-42-21 REV 38 DATED 7-10-19
- [SDR SWIA202157821](https://openairdocs.org/sdr/SWIA202157821.md): Intercostal · corroded · Mar 2, 2021 · N449SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL, PN 601R31902-317, IS CORRODED. (C-CHECK RO 4/25/2021) REMOVED AND REPLACED CORRODED PAX DOOR INTERCOSTAL IAW CRJ 200 SRM 51-40-11 AND 51-42-06 REV 38 DATED JUL 10/19, DWG 601R31902 AND SKY CARD 51-900-1003-SKY AND ATTACHED FORM M-3
- [SDR SWIA202157786](https://openairdocs.org/sdr/SWIA202157786.md): Stringer · corroded · Mar 2, 2021 · N449SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER SEGMENT 26L FROM STA 394 TO 409 IS CORRODED OUT OF LIMITS P/N 601R31022-49. (C-CHECK RO 4/25/2021) REMOVED AND REPLACED STRINGER 26L SEGMENT FROM FS 394-409 ( PN 601R31022-49) IAW CRJ 200 SRM 51-40-11, 51-42-06 AND 51-42-21, SKYCARD 51-900-100
- [SDR SWIA202157820](https://openairdocs.org/sdr/SWIA202157820.md): Doubler · corroded · Mar 1, 2021 · N449SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FS379 SKIN BUTTJOINT DOUBLER IS CORRODED AT STR 23L (C-CHECK RO 4/25/2021) REPAIRED FS379 SKIN BUTTJOINT DOUBLER AT STR 23L IAW MHIRJ REO 601R-53-21-3420 REV. -- DATED 2021-03-29, SKYWEST STRUCTURAL MAJOR REPAIR TASK 51-900-1003-SKY AND ATTACHED FORM
- [SDR SWIA202157789](https://openairdocs.org/sdr/SWIA202157789.md): Frame · corroded · Mar 1, 2021 · N449SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME SECTOR AND SPLICE AT FS 394 ARE CORRODED AT STR 23L. (C-CHECK RO 4/25/2021) REMOVED CORRODED FRAME SECTOR AND REPLACE WITH SERVICABLE FRAME SECTOR AND SRM SPLICE, FS 394, STR 19L - 23L. / NDT CUT LINE, DRILLED UP AND INSTALLED, IAW CRJ 200 SRM 53
- [SDR SWIA202157792](https://openairdocs.org/sdr/SWIA202157792.md): Frame · corroded · Feb 28, 2021 · N449SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS379 FRAME AT STRG 23L IS CORRODED (C-CHECK RO 4/25/2021) REMOVED CORRODED FRAME SEGMENT AND INSTALLED SERVICABLE FRAME SEGMENT, P/N 601R32009-3, IAW CRJ 200 SRM 51-42-06 AND 51-42-21 REV 38B DATED NOV 25/2020 AND SKYCARD 51-900-1003-SKY (CL600-2B19) A
- [SDR SWIA202157790](https://openairdocs.org/sdr/SWIA202157790.md): Frame · corroded · Feb 28, 2021 · N449SW · Cndair CL6002B19 · Fuselage Main, Frame
  > UPON REMOVAL OF FRAME SPLICE AT FS 364 STR 22L AND 23L,FOUND FRAME CORRODED AT MATTING SURFACE. (C-CHECK RO 4/25/2021) REMOVED CORRODED FRAME SECTOR AND INSTALLED SERVICABLE FRAME SECTOR, P/N 601R32007-99, IAW MHIRJ REO 601R-53-21-3415, REV --, DATED 2
- [SDR SWIA202157830](https://openairdocs.org/sdr/SWIA202157830.md): Rib · cracked · Feb 27, 2021 · N449SW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > FOUND R/H BAT RIB LOCATED AT W.S 48.30 TO BE CRACKED NEAR TOP RIB REQUIRES REPLACEMENT (C-CHECK RO 4/25/2021) REMOVED AND INSTALLED SERVICEABLE RH BATT RIB AT WS 48.30 IAW CRJ 200 ARM 51-42-06 AND 51-42-21 REFERENCE ATTACHED CONTINUATION CARD FOR WORK
- [SDR SWIA202157819](https://openairdocs.org/sdr/SWIA202157819.md): Gusset · chafed · Feb 27, 2021 · N449SW · Cndair CL6002B19 · Spoilers
  > LH APRON STRUCTURE GUSSET PN 601R31058-217 AT FS 538.70 IS CHAFFED FROM CONTACT WITH LH INBD GROUND SPOILER RETURN LINE HYDRAULIC LINE PN 601R75147-1, CHAFFE DAMAGE IS.300 WIDE BY.500 LONG. (C-CHECK RO 4/25/2021) PERFORMED A MAJOR REPAIR BY REPLACING
- [SDR SWIA202157871](https://openairdocs.org/sdr/SWIA202157871.md): Support Angle · corroded · Feb 26, 2021 · N449SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FORMER ANGLE CORRODED AND HAS OVERSIZED HOLE PART NUMBER 601R318732-3 (C-CHECK RO 4/25/2021) REMOVED AND REPLACED PAX DOOR FORMER ANGLE WITH NEW SERVICABLE PART IAW CRJ 200 SRM 51-40-11 AND 51-42-06 REV 38 DATED JUL 10/19.
- [SDR SWIA202157870](https://openairdocs.org/sdr/SWIA202157870.md): Doubler · corroded · Feb 26, 2021 · N449SW · Cndair CL6002B19 · Fuselage Main, Structure
  > FOUND O/B DOUBLER ON BATT RIB W.S 53.60 TO HAVE CORROSION AROUND CANNONPLUG MOUNTING HOLES (C-CHECK RO 4/25/2021) REMOVED AND INSTALLED SERVICEABLE DOUBLER IAW CRJ 200 SRM 51-42-06
- [SDR SWIA202157869](https://openairdocs.org/sdr/SWIA202157869.md): Frame · corroded · Feb 24, 2021 · N449SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FOUND FRAME SECTOR CORRODED UPON REMOVAL, FS 364 STR 23L - 24L (C-CHECK RO 4/25/2021) RECIEVED AND DRILLED UP NEW PART, IAW CRJ 200 SRM 51-40-06, 51-40-11. PART TO BE INSTALLED ON MX TRANS# 22363959.
- [SDR SWIA202157868](https://openairdocs.org/sdr/SWIA202157868.md): Splice · corroded · Feb 24, 2021 · N449SW · Cndair CL6002B19 · Fuselage Main, Structure
  > FOUND PART CORRODED UPON REMOVAL AT FS 364 STR 23R TO 24R (C-CHECK RO 4/25/2021) FOUND SPLICE PLATE TO BE OUT OF LIMITS, INSTALLED FABRICATED SPLICE PLATE (REF MX TRANS #22475509) FS 364.00, STR 23R - 24R. IAW CRJ 200 SRM 51-42-06, 51-42-21
- [SDR SWIA202157867](https://openairdocs.org/sdr/SWIA202157867.md): Not Reported · corroded · Feb 24, 2021 · N449SW · Cndair CL6002B19 · Fuselage Structure (General)
  > FOUND PART CORRODED UPON REMOVAL AT FS364 STR 23R - 24R (C-CHECK RO 4/25/2021) RECIEVED AND DRILLED UP NEW PART FROM AIRCRAFT, IAW CRJ 200 SRM 51-40-06, 51-40-11. PART TO BE INSTALLED ON MX TRANS# 22329418 ITEM 11.
- [SDR SWIA202157866](https://openairdocs.org/sdr/SWIA202157866.md): Splice · corroded · Feb 24, 2021 · N449SW · Cndair CL6002B19 · Fuselage Main, Structure
  > FOUND SPLICE ANGLE CORRODED UPON REMOVAL FS364 STR23L. (C-CHECK RO 4/25/2021) BLENDED CORROSION, FOUND TO BE OUT OF LIMITS, PART WAS FABRICATED ON CAMP #22472047, LOCATED, DRILLED AND INSTALLED. / IAW CRJ 200 SRM 51-40-11, 51-42-06, 51-42-21
- [SDR SWIA202157865](https://openairdocs.org/sdr/SWIA202157865.md): Support · corroded · Feb 24, 2021 · N449SW · Cndair CL6002B19 · Aerodynamic Fairings
  > WING TO BODY FAIRING SUPPORT ASSY AT STRINGER 24L F.S 559-80 TO F.S. 574 APPROX HAS A CORRODED ANGLE FOOT THAT REQUIRES REPLACEMENT (C-CHECK RO 4/25/2021) REMOVED AND REPLACED WING TO BODY FAIRING ASSY ANGLE IAW CRJ-200 SRM 51-42-06-00
- [SDR SWIA202157787](https://openairdocs.org/sdr/SWIA202157787.md): Support · corroded · Feb 24, 2021 · N449SW · Cndair CL6002B19 · Aerodynamic Fairings
  > FOUND WING TO BODY SUPPORT ASSY AT STRINGER 24R F.S. 559+80 TO F.S. 574 APPROX IS CORRODED AND REQUIRES REPLACEMENT. (C-CHECK RO 4/25/2021) REMOVED AND INSTALLED SERVICEABLE BODY SUPPORT ASSY AT STRINGER 24R F.S. 559+80 TO F.S. 574 IAW CRJ-200 SRM 51-42
- [SDR SWIA202157784](https://openairdocs.org/sdr/SWIA202157784.md): Skin · damaged · Feb 24, 2021 · N449SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > UPON REMOVAL OF FWD FUSE SKIN PANEL 600-33052-145, FOUND ELONGATED HOLE IN FWD CORNER OF SKIN PANEL AT APPROX FS 173, WL 73.50. (C-CHECK RO 4/25/2021) REPAIRED IAW MHIRJ REO 601R-53-11-3669 REV-- DATED 2021-03-22 COMPLETED SKYCARD 51-900-1003-SKY (CL600
- [SDR SWIA202157782](https://openairdocs.org/sdr/SWIA202157782.md): Tie Down · corroded · Feb 24, 2021 · N449SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO TIE DOWN PLATE CORRODED AROUND ALL NUTPLATE ATTACH HOLES AT APPROX FS 619 BETWEEN LBL 27 AND LBL 36. (C-CHECK RO 4/25/2021) REMOVED BAD TIE DOWN PLATE AND REPLACED WITH NEW TIE DOWN PLATE IAW CRJ-200 SRM 51-41-02 AND CRJ-200 SRM 53-61-43.
- [SDR SWIA202157874](https://openairdocs.org/sdr/SWIA202157874.md): Stop Fitting · chafed · Feb 23, 2021 · N449SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR CUTOUT LOWER PIN STOP FITTING CHAFED AT FS349. (C-CHECK RO 4/25/2021) INSTALLED SERVICEABLE PAX DOOR CUTOUT LOWER PIN STOP IAW CRJ-200 AMM 53-21-23-400-801 ADJUSTMENTS AND OP'S TEST COMPLIED WITH. SEE CONTINUE CARD FOR DETAILS.
- [SDR SWIA202157873](https://openairdocs.org/sdr/SWIA202157873.md): Stop Fitting · chafed · Feb 23, 2021 · N449SW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR CUTOUT LOWER PIN STOP FITTING CHAFED AT FS310. (C-CHECK RO 4/25/2021) INSTALLED SERVICEABLE LOWER PAX DOOR PIN STOP FITTING IAW CRJ-200 AMM 53-21-23-400-801 ADJUSTMENT AND OP'S CHECK COMPLIED WITH

Next page: https://openairdocs.org/aircraft/N449SW/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 = 'N449SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N449SW/reports

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