# Service difficulty reports: N453SW

A list on [N453SW](https://openairdocs.org/aircraft/N453SW.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 · 183 reports

- [SDR SWIA2026082876969](https://openairdocs.org/sdr/SWIA2026082876969.md): Seal · destroyed · Aug 28, 2026 · N453SW · Cndair CL6002B19 · Landing Gear System
  > GEAR DISAGREE ON TAKE OFF NOSE WHEEL DID NOT COME UP. COMPLIED WITH QRH AND MESSAGE EXTINGUISHED WHEN GEAR FULLY DEPLOYED. (FLIGHT 5614) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 32922634 WITH THE FOLLOWING CORRECTIVE ACTION: "SEE CP 32928113 FOR NLG STRU
- [SDR SWIA2026020676010](https://openairdocs.org/sdr/SWIA2026020676010.md): Floor Support · corroded · Feb 6, 2026 · N453SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT CABIN- RBL 9"00 FLOOR BEAM FROM FS 559 +64 TO FS 559 +80 HAS CORROSION. REMOVED AND REPLACED WITH NEW FLOOR BEAM PART # 601R31119-75 FROM FS 559.00 + 64 TO 559.00 + 80 FROM THE AFT CABIN IAW CRJ 200 SRM'S 51-21-16, 53-51-43, 51-40-11, 51-42-36, 51-42-06,
- [SDR SWIA2026012776009](https://openairdocs.org/sdr/SWIA2026012776009.md): Support · cracked · Jan 27, 2026 · N453SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > AFT CARGO COMPARTMENT- UPPER SUPPORT DOOR HAS A CRACK. REPAIRED THE BEAM ASSY CAM TRACK SUPPORT OF THE CARGO DOOR IAW REO: 601R-536-61-8490. IAW SRM 51-42-20, 53-61-23,53-00-00,51-24-36,51-24-16,51-24-21,51-40-11,51-21-11,51-25-06,51-25-16.
- [SDR SWIA2026012176008](https://openairdocs.org/sdr/SWIA2026012176008.md): Skin · dented · Jan 21, 2026 · N453SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FOUND MULTIPLE DENTS AND SCRATCHES BELOW AND AFT OF THE LOW-PRESSURE AIR GROUND CONNECTION DOOR. IF DAMAGE IS FOUND WITHIN LIMITS, ELIMINATE ALL EVIDENCE OF DAMAGE. COMPLIED REPAIR TO FUSELAGE SKIN BETWEEN FS 574.00 AND FS 605.00 STGR 20R TO STRG 27 IAW REO:
- [SDR SWIA2025092600024](https://openairdocs.org/sdr/SWIA2025092600024.md): Computer · loose · Sep 24, 2025 · N453SW · Cndair CL6002B19 · Rudder Control System
  > EXPERIENCED THE RUDDER OSCILLATIONS IN FLIGHT, WITH THE RUDDER RANDOMLY SWINGING TO ONE SIDE. IT SEEMED AS IF THE RUDDER IS LOOSE, WHERE YOU COULD FEEL IT HIT A STOP. (FLIGHT 5832 - FILED CLOSED)PLEASE REFERENCE AML 1712505 PLEASE REFERENCE AML 1712677. REM
- [SDR SWIA202507070006](https://openairdocs.org/sdr/SWIA202507070006.md): Detector · faulted · Jul 6, 2025 · N453SW · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLAP FAIL, AT 20. (FLIGHT 5420 - FILED CLOSED)TROUBLESHOT FLAP FAIL AT 20 DEG IN REFERENCE WITH CRJ200 FIM 27-50-00. INTERROGATED FECU FAULT LOG IN REFERENCE WITH AMM 27-51-05. FOUND LATEST CODES CORRELATING TO LOSS OF A/C POWER 1 AND LOSS OF A/C POWER 2. DET
- [SDR SWIA2025021403](https://openairdocs.org/sdr/SWIA2025021403.md): Hydraulic Line · leaking · Feb 13, 2025 · N453SW · Cndair CL6002B19 · Hydraulic System, Main
  > AFTER TAKEOFF, RECEIVED GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGES. QRH PROCEDURE FOLLOWED AND RETURN TO FIELD ACCOMPLISHED. ON POST-FLIGHT INSPECTION, HYDRAULIC FLUID FOUND LEAKING OUT OF NOSE GEAR ASSEMBLY. (FLIGHT 5513 - FILED CLOSED) PSEU CO
- [SDR SWI2025F00071](https://openairdocs.org/sdr/SWI2025F00071.md): Uplock Sensor · faulted · Jan 17, 2025 · N453SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > IN CRUISE, GOT A GEAR DISAGREE WARNING MESSAGE. EICAS INDICATED RIGHT MAIN GEAR WAS UNLOCKED. NO ABNORMAL YAW OR AIRSPEED VARIATIONS THAT WOULD INDICATE THE GEAR WAS DOWN. MESSAGE WOULD GO AWAY ON ITS OWN AFTER SEVERAL SECONDS AND THEN RETURN. TURNED ON PUMPS
- [SDR SWIA202411120822](https://openairdocs.org/sdr/SWIA202411120822.md): Floor Support · corroded · Aug 22, 2024 · N453SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > TWO AREAS OF CORROSION BETWEEN FS 559.00 - FS 559.00 + 16, STR 17R FLOOR SILL. (FILED CLOSED) REPAIRED TWO AREAS OF CORROSION BETWEEN FS 559.00 - FS 559.00 + 16 STR 17R FLOOR SILL / INTERCOSTAL WITH REFERENCE TO REO 601R-53-51-684 REV "--" DATED 2024-08-
- [SDR SWIA2024091200822](https://openairdocs.org/sdr/SWIA2024091200822.md): Floor Support · corroded · Aug 22, 2024 · N453SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > TWO AREAS OF CORROSION BETWEEN FS 559.00 - FS 559.00 + 16, STR 17R FLOOR SILL. (FILED OPEN) REPAIRED TWO AREAS OF CORROSION BETWEEN FS 559.00 - FS 559.00 + 16 STR 17R FLOOR SILL / INTERCOSTAL WITH REFERENCE TO REO 601R-53-51-684 REV "--" DATED 2024-08-24
- [SDR SWIA202411120819](https://openairdocs.org/sdr/SWIA202411120819.md): Skin · bent · Aug 19, 2024 · N453SW · Cndair CL6002B19 · Wing, Plate/Skin
  > LH LEADING EDGE 530JL HAS SLIGHT BEND NEAR TRAILING EDGE INBOARD SIDE. APPROX 1.25" FROM TRAILING EDGE, AND 5.75" LONG STARTING FROM INBOARD EDGE. (FILED CLOSED) REMOVED LEADING EDGE 530JL INBOARD RIB AND REWORKED DENT NEAR TRAILING EDGE INBOARD SIDE. AP
- [SDR SWIA2024091200819](https://openairdocs.org/sdr/SWIA2024091200819.md): Structure · bent · Aug 19, 2024 · N453SW · Cndair CL6002B19 · Nacelle/Pylon Structure
  > LH LEADING EDGE 530JL HAS SLIGHT BEND NEAR TRAILING EDGE INBOARD SIDE. APPROX 1.25" FROM TRAILING EDGE, AND 5.75" LONG STARTING FROM INBOARD EDGE. (FILED OPEN) REMOVED LEADING EDGE 530JL INBOARD RIB AND REWORKED DENT NEAR TRAILING EDGE INBOARD SIDE. APPR
- [SDR SWI2024F01207](https://openairdocs.org/sdr/SWI2024F01207.md): Pressure Blkhd · damaged · Aug 17, 2024 · N453SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD FS621.00 FWD FACE HAS SCREW DAMAGE ON DOUBLERS LOCATED AT RBL36.20, 27.50, 18.00, 9.50 AND LBL 9.50, 18.00, 27.50 AND 36.20 @ WL103.50 AS WELL AS RIVETS AT WL87.00 WITH SAME BUTTOCK LINES. (FILED CLOSED) COMPLIED WITH REO 601R-53-6
- [SDR SWI2024F01206](https://openairdocs.org/sdr/SWI2024F01206.md): Access Panel · corroded · Aug 17, 2024 · N453SW · Cndair CL6002B19 · Wing, Plate/Skin
  > RH WING FUEL ACCESS PANEL 650EB, OPENING EDGE HAS PITTING AND SURFACE CORROSION ON AFT SIDE, ONE INCH INBOARD OF CENTER EDGE. (FILED CLOSED) BLENDED CORRODED AREA OF RH WING FUEL ACCESS PANEL 650EB LANDING OPENING EDGE ON AFT SIDE ONE INCH INBOARD OF CEN
- [SDR SWI2024F01205](https://openairdocs.org/sdr/SWI2024F01205.md): Access Panel · corroded · Aug 17, 2024 · N453SW · Cndair CL6002B19 · Wing, Plate/Skin
  > RH WING FUEL ACCESS PANEL 640BB, OPENING EDGE HAS PITTING AND SURFACE CORROSION ON INBOARD EDGE AND FWD OUTBOARD EDGE. (FILED CLOSED) BLENDED CORRODED AREA OF RH WING FUEL ACCESS PANEL 640BB LANDING OPENING EDGE ON INBOARD EDGE AND FWD OUTBOARD EDGE WITH
- [SDR SWIA20240817](https://openairdocs.org/sdr/SWIA20240817.md): Pressure Blkhd · cracked · Aug 17, 2024 · N453SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT SIDE OF PRESSURE BULKHEAD @ FS621.00 JUST OUTBOARD OF LBL 36.20 AND INLINE WITH STRINGER 14R, CLIP/ANGLE CRACKED. (FILED CLOSED) REMOVED AND REPLACED INTERCOSTAL ON AFT SIDE OF PRESSURE BULKHEAD @ FS621.00 JUST OUTBOARD OF RBL 36.20 (CORRECTED LOCATIO
- [SDR SWIA2024091200817](https://openairdocs.org/sdr/SWIA2024091200817.md): Access Panel · corroded · Aug 17, 2024 · N453SW · Cndair CL6002B19 · Wing, Plate/Skin
  > RH WING FUEL ACCESS PANEL 650EB, OPENING EDGE HAS PITTING AND SURFACE CORROSION ON AFT SIDE, ONE INCH INBOARD OF CENTER EDGE. (FILED OPEN) BLENDED CORRODED AREA OF RH WING FUEL ACCESS PANEL 650EB LANDING OPENING EDGE ON AFT SIDE ONE INCH INBOARD OF CENTE
- [SDR SWI202409120803](https://openairdocs.org/sdr/SWI202409120803.md): Pressure Blkhd · damaged · Aug 17, 2024 · N453SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD FS621.00 FWD FACE HAS SCREW DAMAGE ON DOUBLERS LOCATED AT RBL36.20, 27.50, 18.00, 9.50 AND LBL 9.50, 18.00, 27.50 AND 36.20 @ WL103.50 AS WELL AS RIVETS AT WL87.00 WITH SAME BUTTOCK LINES. (FILED OPEN) COMPLIED WITH REO 601R-53-61-
- [SDR SWIA202408190017](https://openairdocs.org/sdr/SWIA202408190017.md): Pressure Blkhd · cracked · Aug 17, 2024 · N453SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT SIDE OF PRESSURE BULKHEAD @ FS621.00 JUST OUTBOARD OF LBL 36.20 AND INLINE WITH STRINGER 14R, CLIP/ANGLE CRACKED. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWI2024F01208](https://openairdocs.org/sdr/SWI2024F01208.md): Floor Support · corroded · Aug 13, 2024 · N453SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON SEVERAL AREAS OF THE LH PRESSURE FLOOR SILL FROM FS461.00 TO FS499.00 (FILED CLOSED) UPON FURTHER INSPECTION FOUND ADDITIONAL AREAS OF CORROSION ON THE LH PRESSURE FLOOR SILL BETWEEN FS449.85 - FS559.00. REPAIRED ALL CORROSION DAMAGE
- [SDR SWIA202411120813](https://openairdocs.org/sdr/SWIA202411120813.md): Floor Support · corroded · Aug 13, 2024 · N453SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON SEVERAL AREAS OF THE RH PRESSURE FLOOR SILL FS559.00, FS544.00, FS529.00, FS513.00, FS499.00, FS473.15, FS461.00, FS449.85 AND FS439 (FILED CLOSED) UPON FURTHER INSPECTION FOUND ADDITIONAL AREAS OF CORROSION ON THE RH PRESSURE FLOOR SI
- [SDR SWIA2024091200813](https://openairdocs.org/sdr/SWIA2024091200813.md): Floor Support · corroded · Aug 13, 2024 · N453SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON SEVERAL AREAS OF THE RH PRESSURE FLOOR SILL FS559.00, FS544.00, FS529.00, FS513.00, FS499.00, FS473.15, FS461.00, FS449.85 AND FS439 (FILED OPEN) UPON FURTHER INSPECTION FOUND ADDITIONAL AREAS OF CORROSION ON THE RH PRESSURE FLOOR SILL
- [SDR SWIA202266439](https://openairdocs.org/sdr/SWIA202266439.md): None · damaged · Aug 30, 2022 · N453SW · Cndair CL6002B19 · Wing Structure
  > REMOVED DAMAGED RIGHT WING WINGLET TRAILING EDGE RIB P/N 600-10381-20 LOCATED AT WS404.08 IN REFERENCE TO SRM 57-31-14. (FILED CLOSED) INSTALLED SERVICEABLE R/H WINGLET TRAILING EDGE RIB P/N 600-10381-20 LOCATED AT WS404.08 (ITEM #8 FIG1 SHEET 1 CRJ200 SR
- [SDR SWIA202266142](https://openairdocs.org/sdr/SWIA202266142.md): None · cracked · Jul 21, 2022 · N453SW · Cndair CL6002B19 · Doors
  > PAX DOOR AFT DRAG ANGLE PREVIOUSLY REPAIRED PER REO 601R-52-11-53, REV B, IS CRACKED BETWEEN DATUM 4 - DATUM 5. (FLIGHT 3070 - FILED CLOSED) REPAIRED PAX DOOR AFT DRAG ANGLE WITH REFERENCE TO REO 601R-52-11-53 REV C DATED 2020-10-22.
- [SDR SWIA202266140](https://openairdocs.org/sdr/SWIA202266140.md): None · cracked · Jul 19, 2022 · N453SW · Cndair CL6002B19 · Doors
  > TRANSFER FROM EAML 953047: CRACK TO PAX DOOR INNER SKIN DUE TO SIX (6) FASTENERS PULLED THROUGH FORMER AT FS347.27 LOCATED / UNDER THE PULLEY MOUNTING BRACKET (P/N: 601R317106) (FLIGHT #5345 FILED CLOSED) REPAIRED MCD INNER SKIN AND FORMER AT FS347.25,
- [SDR SWIA202266209](https://openairdocs.org/sdr/SWIA202266209.md): None · damaged · Jul 19, 2022 · N453SW · Cndair CL6002B19 · Doors
  > D: COMPLY WITH GMM 3-26, AIRCRAFT REPAIRS (MAJOR/MINOR), MAJOR REPAIR REQUIREMENTS DURING PERMANENT REPAIR FOLLOWING SPECIAL FLIGHT / C: MCI (FILED CLOSED) COMPLIED WITH GMM 3-26, MAIN CABIN DOOR FORMER AT FS347.27 DEEMED MAJOR REPAIR. REF. CP 25187636 FOR
- [SDR SWIA202264203](https://openairdocs.org/sdr/SWIA202264203.md): None · malfunctioned · Feb 10, 2022 · N453SW · Cndair CL6002B19 · Landing Gear Door Actuator
  > D:AFTER TAKEOFF SELECTED GEAR UP AND GOT A GEAR DISAGREEMENT WARNING MESSAGE AND A NOSE DOOR OPEN WARNING MESSAGE. FOLLOW QRH PROCEDURE ONE WE HAD 3 GREEN WE BURNED ENOUGH FUEL FOR A UNDERWEIGHT LANDING, AND RETURNED TO THE FIELD. / C:MEL 32-30-1 / CAT A DUE
- [SDR SWIA202264200](https://openairdocs.org/sdr/SWIA202264200.md): None · failed · Feb 8, 2022 · N453SW · Cndair CL6002B19 · Landing Gear Door Actuator
  > GEAR LEVER SELECTED UP DURING CLIMB OUT GEAR DISAGREE WARNING MESSAGE WITH NOSE DOOR OPEN WARNING MESSAGE DISPLAYED. NOSE GEAR WAS DOWN WHILE BOTH MAINS RETRACTED. RAN QRH MESSAGE EXTINGUISHED GEAR WOULD NOT RETRACT. (FLIGHT 5616 - FILED OPEN) THIS IS CUR
- [SDR SWIA202054347](https://openairdocs.org/sdr/SWIA202054347.md): Pcu · out of tolerance · Nov 22, 2020 · N453SW · Cndair CL6002B19 · Elevator Structure
  > RIGHT ELEVATOR NR 3 PCU IS OUT OF BACKLASH LIMITS. FILED CLOSED. REMOVED AND REPLACED RT ELEVATOR NR 3 PCU, REF CRJ200 MIP AND REF CP 21894363 FOR PASSING BACKLASH RESULTS. TQ WRENCH SN: 0913800841 DUE: 09/2021. DIGITAL PROTRACTOR NR 1 SN: COS-DP1 DUE: 08/
- [SDR SWIA202054346](https://openairdocs.org/sdr/SWIA202054346.md): Bushing · out of tolerance · Nov 22, 2020 · N453SW · Cndair CL6002B19 · Elevator Structure
  > LEFT ELEVATOR NR 3 PCU BUSHING IS OUT OF BACKLASH LIMITS. FILED CLOSED. REMOVED AND REPLACED BUSHING AND HARDWARE ON ELEVATOR SIDE OF NR 3 ELEVATOR PCU. REFERENCE APPLICABLE STEPS IN AMM. NO FIX, SEE CP 21878626-1 FOR FURTHER TROUBLESHOOTING.
- [SDR SWIA202054345](https://openairdocs.org/sdr/SWIA202054345.md): Bushing · out of tolerance · Nov 22, 2020 · N453SW · Cndair CL6002B19 · Elevator Structure
  > LEFT ELEVATOR NR 2 PCU BUSHING IS OUT OF BACKLASH LIMITS. FILED CLOSED. REMOVED AND REPLACED BUSHING AND HARDWARE ON ELEVATOR SIDE OF NR 2 ELEVATOR PCU. REFERENCE APPLICABLE STEPS IN AMM. NO FIX, SEE CP 21878623-1 FOR FURTHER TROUBLESHOOTING.
- [SDR SWIA202054344](https://openairdocs.org/sdr/SWIA202054344.md): Bushing · out of tolerance · Nov 22, 2020 · N453SW · Cndair CL6002B19 · Elevator Structure
  > LEFT ELEVATOR NR 1 PCU BUSHING IS OUT OF BACKLASH LIMITS. FILED CLOSED. REMOVED AND REPLACED BUSHING AND HARDWARE ON ELEVATOR SIDE OF NR 1 ELEVATOR PCU. REFERENCE APPLICABLE STEPS IN AMM. NO FIX, SEE CP 21878612-1 FOR FURTHER TROUBLE SHOOTING.
- [SDR SWIA2020072051339](https://openairdocs.org/sdr/SWIA2020072051339.md): Line · broken · Jul 19, 2020 · N453SW · Cndair CL6002B19 · Fuel Controlling System
  > CREW REPORTED ON ARRIVAL, WHILE DESCENDING FROM 15K TO 11K FEET, NOT AT IDLE, THE RT ENG BECAME UNRESPONSIVE, NOTICEABLE LOSS OF POWER, FUEL FLOW WENT TO ZERO, FUEL SYNOPTIC PAGE SHOWED 300LB FUEL QTY DIFFERENCE BETWEEN LT & RT TANKS BUT STILL GREEN. CREW
- [SDR SWIA2019111446762](https://openairdocs.org/sdr/SWIA2019111446762.md): Warning Message · false activation · Nov 14, 2019 · N453SW · Cndair CL6002B19 · Landing Gear Steering System
  > STEERING INOP CAUTION MESSAGE IN FLIGHT. RAN QRH, MESSAGE PERSISTED. FLIGHT 3797 CLOSED THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 19890415 WITH THE FOLLOWING CORRECTIVE ACTION: "TROUBLESHOT STEERING INOP CAUTION IAW FIM. NO DEFECTS NOTED. OPC GOOD."
- [SDR SWIA2019101646484](https://openairdocs.org/sdr/SWIA2019101646484.md): Acm · smoke · Oct 13, 2019 · N453SW · Cndair CL6002B19 · Cabin Cooling System
  > HAD A RISE IN CABIN ALTITUDE FOLLOWED BY A CABIN ALT CAUTION AND WARNING. RAN THE EMERGENCY DECENT QRC WHICH INCLUDED PASS OXY SWITCH PRESSED. THEN THE QRH ITEMS WHICH INCLUDED PRESS CONT TO MAN AND ATTEMPTED TO PRESSURIZE MANUALLY THAT DID NOT WORK. LEFT PA
- [SDR SWIA2019100246395](https://openairdocs.org/sdr/SWIA2019100246395.md): Trunnion · damaged · Sep 13, 2019 · N453SW · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > REWORKING THE MLG TRUNNION IAW THE ACCOMPLISHMENT INSTRUCTIONS OF SERVICE BULLETIN. COMPLIED WITH BY REWORKING THE MLG TRUNNION IAW SERVICE BULLETIN. RT AND LT MLG TRUNNIONS OPERATIONAL CK GOOD.
- [SDR SWIA2019100246394](https://openairdocs.org/sdr/SWIA2019100246394.md): Landing · cracked · Aug 23, 2019 · N453SW · Cndair CL6002B19 · Fuselage Main, Structure
  > WHILE REMOVING GROUND POWER RECEPTICAL FOUND CRACK IN GROUND POWER DOOR LANDING. REPAIRS MADE TO GROUND POWER DOOR LANDING IAW REO.
- [SDR SWIA2019100246393](https://openairdocs.org/sdr/SWIA2019100246393.md): Post · cracked · Aug 23, 2019 · N453SW · Cndair CL6002B19 · Fuselage Main, Structure
  > FS409+128 VERTICAL POSTS, RBL27 I/B HALF, LOWER CORNER CRACKED @ FASTENER. (C-CHECK) RO: 09/28/2019 / REPAIRED CRACK AT FS 409+128 VERTICAL POST IAW REO. OPS CHECK GOOD.
- [SDR SWIA2019100246392](https://openairdocs.org/sdr/SWIA2019100246392.md): Post · cracked · Aug 23, 2019 · N453SW · Cndair CL6002B19 · Fuselage Main, Structure
  > FS409+128 VERTICAL POST, LBL27, I/B HALF, LOWER CORNER CRACKED @ FASTENER. (C-CHECK) RO: 09/28/2019 / REPAIRED CRACK AT FS 409+128 VERTICAL POST IAW REO. OPS CHECK GOOD.
- [SDR SWIA2019100246391](https://openairdocs.org/sdr/SWIA2019100246391.md): Trunnion · cracked · Aug 23, 2019 · N453SW · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > WHILE C/W S/B 601R-57-046 RH SIDE AFTER REMOVAL OF FASTENERS FOUND 1EA FASTENER HOLE CRACKED. REPAIRED DAMAGE TO R/H TRUNION LOWER PLAUGE HOLE #17 CRACK IAW REO.
- [SDR SWIA2019100246390](https://openairdocs.org/sdr/SWIA2019100246390.md): Trunnion · damaged · Aug 23, 2019 · N453SW · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > WHILE C/W S/B 601R-57-046 LH SIDE, AFTER REMOVAL OF FASTENERS FOUND 2EA FASTENER HOLES O/S.342 DIA. INSTALLED O/S FASTENERS ON LEFT HAND SIDE OF TRUNION IAW REO.
- [SDR SWIA2019100246389](https://openairdocs.org/sdr/SWIA2019100246389.md): Housing · cracked · Aug 23, 2019 · N453SW · Cndair CL6002B19 · Cargo/Baggage Doors
  > WHILE WORKING AFT CARGO DOOR HANDLE GOUGE, FOUND HOUSING CRACKED FWD AND AFT SIDES (C-CHECK) RO: 09/28/2019 / REMOVED AND REPLACED AFT CARGO DOOR HANDLE HOUSING ASSY IAW SRM. FUNCTIONAL CHECK AND OPS CHECK GOOD PER AMM.
- [SDR SWIA2019100246388](https://openairdocs.org/sdr/SWIA2019100246388.md): Landing · corroded · Aug 23, 2019 · N453SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFTER REMOVAL OF LH MAIN FUEL TANK CLIMB VENT TUBING FOUND LONGERON SHROUD LANDING CORRODED. REPAIRED CLIMB VENT TUBE LANDING IAW REO.
- [SDR SWIA2019100246387](https://openairdocs.org/sdr/SWIA2019100246387.md): Frame · cracked · Aug 10, 2019 · N453SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME 235 IS CRACKED JUST BELOW THE LH SIDE WINDOW POST FITTING, IN THE FLT DECK. REMOVED AND REPLACED FRAME 235 BELOW L/H WINDOW POST IAW SRM.
- [SDR SWIA2019100246386](https://openairdocs.org/sdr/SWIA2019100246386.md): Angle · cracked · Aug 9, 2019 · N453SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE CLIP IS CRACKED AT RBL 6.75 FS 202.75, IN THE NOSE WHEEL WELL UPPER RH SIDE. (C-CHECK) RO: 09/28/2019 / REMOVED AND REPLACED ANGLE CLIP IN THE NLG WHEEL WELL IAW SRM. OPS CK WINDSHIELD WIPER SYS GOOD IAW AMM.
- [SDR SWIA2019100246385](https://openairdocs.org/sdr/SWIA2019100246385.md): Floor Support · corroded · Aug 9, 2019 · N453SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LH FLOOR SILL HAS CORROSION SPOTS AT THE TOP AND BOTTOM SIDE BETWEEN FS 559+32 THRU FS 559+80, IN THE CABIN. REPAIRED DAMAGE AT TOP & BOTTOM FS 559+32 AND FS559+80 FLOOR SILL IAW REO.
- [SDR SWIA2019100246384](https://openairdocs.org/sdr/SWIA2019100246384.md): Threshold · corroded · Aug 9, 2019 · N453SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR THRESHOLD HAS CORROSION. REMOVED CORROSION IAW SRM.
- [SDR SWIA2019100246383](https://openairdocs.org/sdr/SWIA2019100246383.md): Panel · damaged · Aug 9, 2019 · N453SW · Cndair CL6002B19 · Standard Practices/Structures
  > PNL 684AB HAS ELONGATED SCREW HOLE. REPLACED UNSERVICEABLE PANEL 684AB IAW SRM.
- [SDR SWIA2019100246382](https://openairdocs.org/sdr/SWIA2019100246382.md): Bulkhead Web · damaged · Aug 9, 2019 · N453SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621.00 FWD FACE OF RPB, RBL42, WL77. DAMAGED BY CONTACT WITH BULKHEAD ATTACH HDWR. PERFORMED REPAIR IAW REO.
- [SDR SWIA2019100246381](https://openairdocs.org/sdr/SWIA2019100246381.md): Skin · scratched · Aug 9, 2019 · N453SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > AFT EQUIP BAY DOOR CUT OUT AT STRG 25L HAS DEEP SCRATCHES AND A DENT. REMOVED AND REPLACED LH WEB ON AFT EQUP BAY CUTOUT IAW SRM.

Next page: https://openairdocs.org/aircraft/N453SW/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 = 'N453SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N453SW/reports

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