# Service difficulty reports: N454SW

A list on [N454SW](https://openairdocs.org/aircraft/N454SW.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 · 235 reports

- [SDR SWIA202601050221](https://openairdocs.org/sdr/SWIA202601050221.md): Skin · dented · Dec 21, 2025 · N454SW · Cndair CL6002B19 · Ailerons
  > DURING INSPECTION OF PANELS FOUND DENT IN RT AILERON UPPER SKIN, NEAR THE INBD EDGE. REPAIRED RH AILERON UPPER SKIN NEAR THE INBD EDGE IAW REO 601R-57-61-887 REV -, AND COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWI2026F00040](https://openairdocs.org/sdr/SWI2026F00040.md): Angle · corroded · Nov 2, 2025 · N454SW · Cndair CL6002B19 · Fuselage Main, Structure
  > UPON REMOVAL OF LOW-PRESSURE GROUND AIR DOOR STRUCTURES FOUND REINFORCING ANGLE CORRODED. REMOVED CORRODED REINFORCING ANGLE IAW SRM 51-42-06 AND INSTALLED NEW REINFORCING ANGLE IAW SRM 51-42-06 AND DWG 601R36025 REV. P AND COMPLIED WITH TASK 51-900-1003-SKY
- [SDR SWI2026F00039](https://openairdocs.org/sdr/SWI2026F00039.md): Angle · corroded · Nov 2, 2025 · N454SW · Cndair CL6002B19 · Passenger/Crew Doors
  > UPON REMOVAL OF LOW PRESSURE GROUND AIR DOOR AFTANGLE FOUND LANDING ANGLE CORRODED. REMOVED LOW-PRESSURE GROUND AIR DOOR AFT ANGLE LANDING IAW SRM 51-42-06 AND INSTALLED NEW LOW-PRESSURE GROUND AIR DOOR AFT ANGLE LANDING IAW SRM 51-42-06 AND DWG 601R35226 R
- [SDR SWI2026F00038](https://openairdocs.org/sdr/SWI2026F00038.md): Angle · corroded · Nov 2, 2025 · N454SW · Cndair CL6002B19 · Fuselage Main, Structure
  > LOW PRESSURE GROUND AIR DOOR FWD LANDING ANGLE IS CORRODED. REMOVED FWD LANDING ANGLE IAW SRM 51-42-06 AND INSTALLED NEW FWD LANDING ANGLE IAW SRM 51-42-06 AND DWG 601R35226 REV. P AND COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWI2026F00037](https://openairdocs.org/sdr/SWI2026F00037.md): Mount · corroded · Nov 2, 2025 · N454SW · Cndair CL6002B19 · Fuselage Main, Structure
  > LOW PRESSURE GROUND AIR DOOR MOUNTING PLATE IS CORRODED. REMOVED AND REPLACED BY NEW MOUNTING PLATE AT LOW PRESSURE GROUND AIR DOOR, REF. SRM 51-42-06, REV. 39, AND DWG 601R35226 REV. P. COMPLIED WITH TASK CARD 51-900-1003-SKY. PERFORMED LEAK CHECK GOOD, NO LE
- [SDR SWI2026F00036](https://openairdocs.org/sdr/SWI2026F00036.md): Door Frame · corroded · Nov 2, 2025 · N454SW · Cndair CL6002B19 · Fuselage Main, Structure
  > UPON REMOVAL OF LOW-PRESSURE GROUND AIR DOOR STRUCTURES FOUND FRAME SECTION AT BS 589 CORRODED. REMOVED AND REPLACED BY NEW FRAME SECTION AT BS 589, S21-20L IAW SRM 51-42-06, SRM 51-42-21 REV. 39, DWG 601R36025 REV. P, AND DWG 601R35005 REV AG,
- [SDR SWI2026F00035](https://openairdocs.org/sdr/SWI2026F00035.md): Angle · corroded · Nov 2, 2025 · N454SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF FRAME BS 574 BETWEEN S20R AND S20L FOUND REINFORCING ANGLE CORRODED AT MULTIPLE LOCATION. REMOVED AND REPLACED BY NEW REINFORCING ANGLE AT BS 574 BETWEEN S24L TO S20L IAW SRM 51-42-06 AND SRM 51-42-21 REV. 39, AND DWG 601R36024 REV. N. PERFOR
- [SDR SWIA20260105102](https://openairdocs.org/sdr/SWIA20260105102.md): Door · corroded · Nov 2, 2025 · N454SW · Cndair CL6002B19 · Air Conditioning Doors
  > LOW PRESSURE GROUND AIR DOOR AFT INTERNAL STRUCTURE ANGLE IS CORRODED. REMOVED AFT ANGLE IAW SRM 51-42-06 AND INSTALLED NEW AFT ANGLE IAW SRM 51-42-06 AND IAW DWG 601R35226 REV. P. PERFORMED LEAK CHECK GOOD,
- [SDR SWIA2026010531](https://openairdocs.org/sdr/SWIA2026010531.md): Door · corroded · Oct 31, 2025 · N454SW · Cndair CL6002B19 · Air Conditioning Doors
  > LOW PRESSURE GROUND AIR DOOR FWD INTERNAL STRUCTURE IS CORRODED. REMOVED FWD ANGLE IAW SRM 51-42-06 AND INSTALLED NEW FWD ANGLE IAW SRM 51-42-06. PERFORMED LEAK CHECK GOOD.
- [SDR SWI2026F00034](https://openairdocs.org/sdr/SWI2026F00034.md): Skin · chafed · Oct 23, 2025 · N454SW · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING LOWER SKIN CHAFED AT WS 264 WHERE FLAP FAIRING MAKE CONTACT. REPAIRED LH WING LOWER SKIN WS 264 IAW REO 601R-57-21-3988, REV-, & SKYWEST TASK CARD 51-900-1003-SKY.
- [SDR SWI2026F00033](https://openairdocs.org/sdr/SWI2026F00033.md): Intercostal · cracked · Oct 23, 2025 · N454SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > BS 625.30, S14L, ATTACHING ANGLE FROM THE FRAME TO THE INTERCOSTAL ON THE REAR PRESSURE BULKHEAD, IS CRACKED. INTERCOSTAL AND REPLACED WITH NEW INTERCOSTAL IAW DWG 601-35012 REV D, REO 601R-53-61-422 REV NC, SRM 51-42-21, AND SKYWEST TASK CARD 51-900-1003-SKY
- [SDR SWI2026F00032](https://openairdocs.org/sdr/SWI2026F00032.md): Skin · chafed · Oct 23, 2025 · N454SW · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING LOWER SKIN CHAFFED AT WS127.25 WHERE FLAP FAIRING MAKE CONTACT. REPAIRED LT WING LOWER SKIN WS127.25 IAW REO 601R-57-21-3992 REV -.
- [SDR SWIA2026010523](https://openairdocs.org/sdr/SWIA2026010523.md): Skin · gouged · Oct 23, 2025 · N454SW · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING LOWER SKIN FRETTING AND GOUGED AT TRAILING EDGE BL45.00 WHERE FAIRING MAKES CONTACT. REPAIRED RT WING LOWER SKIN FRETTING AND GOUGE AT TRAILING EDGE BL45.00 WHERE FAIRING MAKES CONTACT REF REO 601R-57-21-880 REV-D,, DWG# 601R10046 REV. V, SRM 51-1
- [SDR SWIA2026010500020](https://openairdocs.org/sdr/SWIA2026010500020.md): Frame · corroded · Oct 20, 2025 · N454SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME AT BS 605 AND BETWEEN S20L-18L HAS SEVERAL CORROSION AND CRACKED AT S18L. REMOVED AND REPLACED BY NEW FRAME SECTION AT BS 605 BETWEEN S20L-S18L AND WL 73 REF. DWG 601R36026 REV. AF, SRM 51-42-06 AND SRM 51-42-21, REV. 39. COMPLIED WITH TASK CARD 51-90
- [SDR SWIA2026010500017](https://openairdocs.org/sdr/SWIA2026010500017.md): Hinge · chafed · Oct 17, 2025 · N454SW · Cndair CL6002B19 · Elevator Structure
  > THE LT HORIZONTAL STAB ELEVATOR HINGE NR 1 IS CHAFED/GOUGED. REPAIRED LT HORIZONTAL STAB ELEVATOR HINGE NR 1 IAW REO 601R-55-11-807 REV -. AND COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWI2026F00043](https://openairdocs.org/sdr/SWI2026F00043.md): Floor Support · corroded · Oct 15, 2025 · N454SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT PRESSURE FLOOR SILL HAS MULTIPLE AREAS OF CORROSION BETWEEN FS409+128 AND FS559. REMOVED CORROSION ON RT FLOOR SILL BETWEEN FS409+128 AND FS559 AND FOUND TO BE WITHIN LIMITS. REF. GREO 601R-53-41-666, REV. C, DISPOSITION 1.2. COMPLIED WITH TASK CARD 5
- [SDR SWIA20260105001](https://openairdocs.org/sdr/SWIA20260105001.md): Floor Support · corroded · Oct 15, 2025 · N454SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT HAND PRESSURE FLOOR SILL HAS MULTIPLE AREAS OF CORROSION BETWEEN FS409 +128 AND FS559. REMOVED CORROSION ON LT FLOOR SILL BETWEEN FS409+128 AND FS559.00 AND FOUND TO BE WITHIN LIMITS. REF. GREO 601R-53-41-666, REV. -C, DISPOSITION 1.2. COMPLIED WITH TAS
- [SDR SWI2026F00031](https://openairdocs.org/sdr/SWI2026F00031.md): Hinge Box · chafed · Oct 14, 2025 · N454SW · Cndair CL6002B19 · Wing, Control Surface Attach Fittings
  > LEFT FLAP HINGE BOX AT WS220 AFT HINGE ATTACH FITTING CHAFED. REPAIRED LH FLAP HINGE BOX AT WS 220 AFT HINGE ATTACH FITTING IAW REO 601R-57-21-3984 REV -. AND COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWI2026F00030](https://openairdocs.org/sdr/SWI2026F00030.md): Rib · bent · Oct 14, 2025 · N454SW · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > LEFT WING REAR SPAR WS 130.00 RIB IS BENT. REMOVED AND REPLACED BY NEW LH WING REAR SPAR RIB, REF. DWG 601R10339, REV. D, SRM 51-42-21, REVISION 39, AND SRM 51-42-06 REVISION 39, COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.
- [SDR SWI2026F00029](https://openairdocs.org/sdr/SWI2026F00029.md): Retainer · chafed · Oct 14, 2025 · N454SW · Cndair CL6002B19 · Fuselage Main, Structure
  > FWD UPPER RETAINING PLATE FOR LT WING STUB FAIRING CHAFING AGAINST FUSELAGE EXTERNAL SKIN. REPAIRED FWD UPPER RETAINING PLATE FOR LH WING STUB FAIRING (APRON SKIN) IAW REO 601R-53-41-3365 REV -. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWI2026F00028](https://openairdocs.org/sdr/SWI2026F00028.md): Access Panel · elongated · Oct 14, 2025 · N454SW · Cndair CL6002B19 · Horizontal Stabilizer, Plate/Skin
  > 11EA OBLONG HOLES ON THE HORIZONTAL STABILIZER, UNDER ACCESS PANEL 333AL REPAIRED ELONGATED SCREW HOLES ON THE HORIZONTAL STABILIZER, UNDER ACCESS PANEL 333AL. REF REO 601R-55-11-812 REV. --,
- [SDR SWIA2026010514](https://openairdocs.org/sdr/SWIA2026010514.md): Access Panel · corroded · Oct 14, 2025 · N454SW · Cndair CL6002B19 · Horizontal Stabilizer Miscellaneous Structure
  > 2EA FASTENER HOLES WITH NOTED CORROSION ON THE HORIZONTAL STABILIZER, UNDER ACCESS PANEL 333AL (MARKED). (C-CHECK RO 01/03/2026)REMOVED CORROSION ON 2EA FASTENER HOLES ON THE HORIZONTAL STABILIZER, UNDER ACCESS PANEL 333AL. REF 601R-55-11-812 REV. --, DATED:
- [SDR SWI2026F00026](https://openairdocs.org/sdr/SWI2026F00026.md): Vane · chafed · Oct 13, 2025 · N454SW · Cndair CL6002B19 · Trailing Edge Flaps
  > CHAFING ON RT INBD FLAP OTBD FLAP VANE ACTUATOR BODY. REPAIRED RH INBD FLAP OTBD FLAP VANE ACTUATOR BODY IAW REO 601R-57-52-2533 REV.-.
- [SDR SWIA20260105013](https://openairdocs.org/sdr/SWIA20260105013.md): Vane · chafed · Oct 13, 2025 · N454SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP VANE LEADING EDGE IS CHAFED IN MULTIPLE LOCATIONS. LT INBOARD FLAP VANE LEADING EDGE 2 EA. AREAS BLENDED AND REPAIRED TO BE WITHIN LIMITS. REF REO 601R-57-52-004, REV -D, 2012-12-19. 1 EA. BLEND ON SKIN PANEL 601R14303-51 FOUND TO BE OUT OF LIMI
- [SDR SWI2026F00042](https://openairdocs.org/sdr/SWI2026F00042.md): Floor Support · corroded · Oct 12, 2025 · N454SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT CARGO FLOOR SUPPORT, RBL 9, BETWEEN BS 559+64 AND BS.559+80 HAS SPOTS OF CORROSION. BLENDED REPORTED CORROSION ON THE FLOOR SUPPORT INNER CAP FLANGE BETWEEN BS 559+64 AND BS 559+80 IAW SRM 51-21-06. BLENDED AREA WAS FOUND OUT OF LIMITED IAW SRM 53-31-43 A
- [SDR SWI2026F00041](https://openairdocs.org/sdr/SWI2026F00041.md): Hinge Arm · chafed · Oct 12, 2025 · N454SW · Cndair CL6002B19 · Wing, Control Surface Attach Fittings
  > LEFT INBD FLAP OTBD HINGE ARM CHAFED ON FWD PIVOT FITTING 3EA. LOCATIONS. REPAIRED LH INBD FLAP OTBD HINGE ARM CHAFE IAW ALL STEPS OF REO REO 601R-57-54-379 REV -. SKYWEST TASK CARD 51-900-1002-SKY COMPLIED WITH.
- [SDR SWIA2026010500012](https://openairdocs.org/sdr/SWIA2026010500012.md): Hinge Arm · chafed · Oct 12, 2025 · N454SW · Cndair CL6002B19 · Wing, Control Surface Attach Fittings
  > LH INBD FLAP INBD HINGE ARM CHAFFED ON FWD PIVOT FITTING. COMPLIED WITH REPAIR AT LH IB FLAP HINGE ARM REF. CRJ-200 REO 601R-57-54-382 REV-. ALL STEPS COMPLIED WITH. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWI2026F00027](https://openairdocs.org/sdr/SWI2026F00027.md): Cleat · gouged · Oct 9, 2025 · N454SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FRAME TO LONGERON CLEAT AT WL73.00, RH FS484.00 IS GOUGED ON AFT SIDE AT FLOOR (C-CHECK RO 01/03/2026)BLENDED GOUGED AREA ON FRAME TO LONGERON CLEAT AT WL73.00 RH FS 484.00 REF REO 601R-53-41-3366 REV -- DATED 2025-11-04 STEPS 1 THROUGH 4. ORIGINAL THICKNESS
- [SDR SWIA2026010509](https://openairdocs.org/sdr/SWIA2026010509.md): Cleat · gouged · Oct 9, 2025 · N454SW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FRAME TO LONGERON CLEAT AT WL73.00, LH FS461.50 IS GOUGED ON UPPER FORWARD SIDE. REMOVED AND REPLACED BY NEW FRAME TO LONGERON CLEAT AT WL73.00, LT FS461.50 REF. DWG 601R31145 REV. -P, DWG 601R31034 REV. -F AND SRM 51-42-21, REV. 39, PERFORMED LEAK CHECK G
- [SDR SWI2026F00025](https://openairdocs.org/sdr/SWI2026F00025.md): Floor Support · corroded · Oct 8, 2025 · N454SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT CARGO FLOOR SILL FROM BS.559+85 TO BS 559+115, RBL 36 HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND INSTALL A NEW RT CARGO FLOOR SILL, BS 559+85 - 559+115 IAW SRM 51-42-21, SRM 51-42-06, SRM 51-45-00 AND DWG 601R31133, REV J. COMPLIED WITH TASK CARD 51-9
- [SDR SWI2026F00024](https://openairdocs.org/sdr/SWI2026F00024.md): Floorbeam · corroded · Oct 8, 2025 · N454SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RBL9 HAS MULTIPLE SPOTS OF CORROSION ON TOP PLATE BETWEEN BS 409 TO BS 409+64. REPAIRED MULTIPLE SPOTS OF CORROSION ON TOP PLATE OF FLOORBEAM CAP REF SRM 53-00-43, REPAIR 2, STEP 5 A (7) FIG. 203, REO. 601R-53-31-1354, REV--, STEPS 1 - 9, ALL OTHER REQUIRE
- [SDR SWI2026F00023](https://openairdocs.org/sdr/SWI2026F00023.md): Floor Support · corroded · Oct 8, 2025 · N454SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON TOP OF RBL9 BETWEEN FS513.00 TO FS529.00. REPAIRED RBL9 BETWEEN FS513 TO FS529 FLOOR SUPPORT EXTRUSION AT RBL 9.00 FS409.00+128-FS529.00. REF. REO 601R-53-41-3361 REV -, DWG 601R31005 REV. B, DWG 601R31118 REV. L, LEAK CHECK GOOD, NO LEAKS NOTED
- [SDR SWI2026F00022](https://openairdocs.org/sdr/SWI2026F00022.md): Door Sill · corroded · Oct 8, 2025 · N454SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR LOWER SILL HAS MULTIPLE SPOTS OF CORROSION (MARKED). (C-CHECK RO 01/03/2026)AFT CARGO DOOR LOWER SILL IS REMOVED AND REPLACED WITH NEW IAW DWG 601R35011 REV. -R, SRM 51-42-06, SRM 51-42-21 AND REO 601R-53-61-593, REV. -A,
- [SDR SWIA2026010508](https://openairdocs.org/sdr/SWIA2026010508.md): Strap · corroded · Oct 8, 2025 · N454SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS559.00 ON RT SIDE JUST ABOVE SILL CORRODED ON STRAP OF INNER FACE OF FRAME. REPLACED WITH NEW STRAP P/N: 601R32026-321 AT BULKHEAD ON RH SIDE @FS559.00 IAW DWG 601R32026 REV. -T, REF SRM 51-42-06, APPLIED FILLET SEAL TO PARTS REF AMM 51-23-00 AND RESTORED
- [SDR SWIA2026010507](https://openairdocs.org/sdr/SWIA2026010507.md): Support Angle · corroded · Oct 7, 2025 · N454SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON THE LOWER SUPPORT ANGLE AT FS409.00 BETWEEN STGR26L - 26R. REMOVED AND REPLACED BY NEW LOWER SUPPORT ANGLE P/N 601R32200-17 AT FS409.00 BETWEEN STGR26L - 26R REF. DWG 601R31057 REV. -J, DWG 601R32200 REV. -V, CRJ-200, SRM 51-42-06 AND CRJ-200, SR
- [SDR SWI2026F00021](https://openairdocs.org/sdr/SWI2026F00021.md): Skin · chafed · Oct 6, 2025 · N454SW · Cndair CL6002B19 · Ailerons
  > LH AILERON LOWER LEADING EDGE CHAFFED.)REMOVED AND INSTALLED NEW LH AILERON INBOARD LOWER LEADING EDGE SKIN SHROUD P/N CC670-13053-1 REF. DWG CC670-13000 REV. -D, CRJ200 SRM 51-42-21 AND CRJ200 SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY.
- [SDR SWIA2026010500006](https://openairdocs.org/sdr/SWIA2026010500006.md): Skin · chafed · Oct 6, 2025 · N454SW · Cndair CL6002B19 · Ailerons
  > LEFT AILERON UPPER LEADING EDGE CHAFED. REMOVED DAMAGED LH AILERON UPPER LEADING EDGE SKIN REF. SRM 51-42-06, SRM 51-42-21 AND SRM 51-42-22 AND INSTALLED NEW LH AILERON UPPER LEADING EDGE SKIN REF. DWG CC670-13000 REV. -D, SRM 51-42-06, SRM 51-42-21 AND S
- [SDR SWIA20260105930](https://openairdocs.org/sdr/SWIA20260105930.md): Fairing · damaged · Sep 30, 2025 · N454SW · Cndair CL6002B19 · Aerodynamic Fairings
  > 1EA ELONGATED HOLE NOTED UNDER FUSELAGE FAIRING 191BB, BETWEEN STR18L-STR19L AT FS409+96. REPAIRED 1EA ELONGATED HOLE UNDER FUSELAGE FAIRING 191BB, BETWEEN STR18L-STR19L AT FS409+96, REF. REO REO 601R-53-31-1356 REV -.
- [SDR SWIA20260105927](https://openairdocs.org/sdr/SWIA20260105927.md): Skin · dented · Sep 27, 2025 · N454SW · Cndair CL6002B19 · Emergency Exits
  > RH OVERWING EMERGENCY EXIT HAS DENT ON EXTERNAL SKIN LOWER FWD CORNER (MARKED) (C-CHECK RO 01/03/2026)REPAIRED RH OVERWING EMER EXIT DENT IAW ALL STEPS OF REO 601R-52-21-172 REV -A DATED 2025-11-20. M-337 AND SKYWEST TASK CARD 51-900-1003-SKY COMPLIED WITH.
- [SDR SWIA20260105926](https://openairdocs.org/sdr/SWIA20260105926.md): Skin · damaged · Sep 26, 2025 · N454SW · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING LEADING EDGE HAS A FASTENER MISSING AT OTBD JOINT SEAM AT APPROX WS 353. REPAIRED RH WING LEADING EDGE ELONGATED HOKES AT OTBD JOINT SEAM @ APROX WS353.00 IAW REO 601R-57-41-1206 REV. --,
- [SDR SWI2026F00020](https://openairdocs.org/sdr/SWI2026F00020.md): Frame · corroded · Aug 18, 2025 · N454SW · Cndair CL6002B19 · Fuselage Main, Frame
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA92210-601R-53-61-8197 N454SW MXCODEID76131-PR - COMPLY WITH PERMANENT REPAIR ON RA ID: 92210CORROSION DAMAGE ON AFT WEB OF FS 574.00 BETWEEN STR20L - 21L. PERFORMED TEMPORARY REPAIR OF CORROSION DAMAGE ON AFT WEB OF
- [SDR SWI2026F00019](https://openairdocs.org/sdr/SWI2026F00019.md): Skin · damaged · Aug 18, 2025 · N454SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > PERMANENT DISPOSITION FOR BLENDED SKIN AND MISDRILL DAMAGE TO FUSELAGE SKIN BETWEEN FS559+112 €“ FS574.00 & STR15L €“ STR16L., COMPLIED WITH PERMANENT REPAIR ON FUSELAGE SKIN BETWEEN FS559+112-FS574.00, STGR15L-STGR16L, REF. REO 601R-53-61-8417, REV. --, DAT
- [SDR SWI2026F00018](https://openairdocs.org/sdr/SWI2026F00018.md): Skin · damaged · Aug 18, 2025 · N454SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > PERFORMED TEMPORARY REPAIR TO 4 DAMAGED RIVETS AND 1 BURN MARK ON RH SIDE OF FUSELAGE BETWEEN FS409+16 AND FS409+32, ALSO BETWEEN STR23R AND STR24R. WORK DONE IN ACCORDANCE WITH REO 601R-53-31-1134 REV A DATED: 2020-08-19. COMPLIED WITH EDDY CURRENT INSPECTI
- [SDR SWIA2026010200818](https://openairdocs.org/sdr/SWIA2026010200818.md): Not Reported · not reported · Aug 18, 2025 · N454SW · Cndair CL6002B19 · Standard Practices/Structures
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA92498-601R-53-61-8196 MXCODEID76417-PR - COMPLY WITH PERMANENT REPAIR ON RA ID: 92498THE SUBJECT CONDITION IS STRUCTURALLY ACCEPTABLE FOR 1700 FLIGHT HOURS FROM INCORPORATION OF REO 601R-53-61-8196., PART NUMBER: -
- [SDR SWIA202507070004](https://openairdocs.org/sdr/SWIA202507070004.md): A/C Pack · odor · Jul 4, 2025 · N454SW · Cndair CL6002B19 · Cabin Cooling System
  > BURNING SMELL FOR 1-2 MINUTES COMING FROM CAPTAINS SIDE COCKPIT VENT. ONCE WE IDENTIFIED IT WAS COMING FROM CA SIDE VENT, SMELL STARTED TO GO AWAY ON ITS OWN WITHOUT ANY INTERVENTION. REFER TO ML 30434357 FOR REMOVAL AND REPLACEMENT OF THE LH AIR CYCLE MACHINE
- [SDR SWIA2024092500001](https://openairdocs.org/sdr/SWIA2024092500001.md): Landing Gear · warning message · Sep 24, 2024 · N454SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > D: GEAR DISAGREE WARNING MESSAGE, SHOWED THE RIGHT LANDING GEAR WAS NOT RETRACTED. RAN QRH AND FIXED THE PROBLEM. GOT THREE GREEN LIGHTS AND RETURNED TO PRC.C: MEL 32-30-1CAT: A DUE DATE: 1 FC TAC NOT EXCEED: 36090. ODI EVENT REQUIRES UPPER MANAGEMENT APPROVA
- [SDR SWIA202408140007](https://openairdocs.org/sdr/SWIA202408140007.md): Skin · punctured · Aug 7, 2024 · N454SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > PUNCTURE ON THE R/H FUSELAGE BETWEEN FS 559+96 AND 559+112 AND BETWEEN STGR 16R AND 17R MEASURING APPROX 3.5" H X 4" L. THIS IS CLASSIFIED AS A MAJOR REPAIR. FORM M-337 INITIATED. (FILED CLOSED) PERFORMED PERMANENT REPAIR ON R/H FUSELAGE BETWEEN FS 559+96
- [SDR SWIA202407101](https://openairdocs.org/sdr/SWIA202407101.md): Web · corroded · Jul 10, 2024 · N454SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION DAMAGE ON AFT WEB OF FS 574.00 BETWEEN STR20L - 21L (FILED CLOSED) PERFORMED TEMPORARY REPAIR OF CORROSION DAMAGE ON AFT WEB OF FRAME FS 574.00 BETWEEN STR20L - 21L WITH REFERENCE TO REO 601R-53-61-8197 REV A DATED 07/11/2024. PERFORMED EDDY CU
- [SDR SWIA202407120010](https://openairdocs.org/sdr/SWIA202407120010.md): Web · corroded · Jul 10, 2024 · N454SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION DAMAGE ON AFT WEB OF FS 574.00 BETWEEN STR20L - 21L (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA202407290008](https://openairdocs.org/sdr/SWIA202407290008.md): Skin · dented · Jul 8, 2024 · N454SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT LOCATED 1.5" FORWARD OF FS 605.00 BETWEEN STR 19L AND STR 20L. (FILED CLOSED)REPAIRED DENT LOCATED 1.5" FORWARD OF FS 605.00 BETWEEN STR 19L AND STR 20L IN REF TO REO 601R-53-61-8202, REV--, DATED 2024-07-18. COMPLETED TASK CARD 51-900-1003-SKY AND M-337.

Next page: https://openairdocs.org/aircraft/N454SW/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 = 'N454SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N454SW/reports

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