N453SW
Service difficulty reports · 183
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "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"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SWIA2026082876969Seal · destroyedGEAR 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 STRUSDR SWIA2026020676010Floor Support · corrodedAFT 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 SWIA2026012776009Support · crackedAFT 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 SWIA2026012176008Skin · dentedFOUND 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 SWIA2025092600024Computer · looseEXPERIENCED 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. REMSDR SWIA202507070006Detector · faultedFLAP 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. DETSDR SWIA2025021403Hydraulic Line · leakingAFTER 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 COSDR SWI2025F00071Uplock Sensor · faultedIN 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 SWIA202411120822Floor Support · corrodedTWO 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 SWIA2024091200822Floor Support · corrodedTWO 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 2024-08-24SDR SWIA202411120819Skin · bentLH 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. APSDR SWIA2024091200819Structure · bentLH 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. APPRSDR SWI2024F01207Pressure Blkhd · damagedREAR 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-53-6SDR SWI2024F01206Access Panel · corrodedRH 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 CENSDR SWI2024F01205Access Panel · corrodedRH 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 SWIA20240817Pressure Blkhd · crackedAFT 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 LOCATIOSDR SWIA2024091200817Access Panel · corrodedRH 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 CENTESDR SWI202409120803Pressure Blkhd · damagedREAR 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 SWIA202408190017Pressure Blkhd · crackedAFT 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 PROGRESSSDR SWI2024F01208Floor Support · corrodedFOUND 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 SWIA202411120813Floor Support · corrodedFOUND 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 SISDR SWIA2024091200813Floor Support · corrodedFOUND 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 SILLSDR SWIA202266439None · damagedREMOVED 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 SRSDR SWIA202266142None · crackedPAX 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 SWIA202266140None · crackedTRANSFER 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 SWIA202266209None · damagedD: 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 FORSDR SWIA202264203None · malfunctionedD: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 SWIA202264200None · failedGEAR 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 CURSDR SWIA202054347Pcu · out of toleranceRIGHT 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 SWIA202054346Bushing · out of toleranceLEFT 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 SWIA202054345Bushing · out of toleranceLEFT 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 SWIA202054344Bushing · out of toleranceLEFT 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 SWIA2020072051339Line · brokenCREW 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 SWIA2019111446762Warning Message · false activationSTEERING 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 SWIA2019101646484Acm · smokeHAD 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 PASDR SWIA2019100246395Trunnion · damagedREWORKING 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 SWIA2019100246394Landing · crackedWHILE REMOVING GROUND POWER RECEPTICAL FOUND CRACK IN GROUND POWER DOOR LANDING. REPAIRS MADE TO GROUND POWER DOOR LANDING IAW REO.SDR SWIA2019100246393Post · crackedFS409+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 SWIA2019100246392Post · crackedFS409+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 SWIA2019100246391Trunnion · crackedWHILE 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 SWIA2019100246390Trunnion · damagedWHILE 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 SWIA2019100246389Housing · crackedWHILE 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 SWIA2019100246388Landing · corrodedAFTER REMOVAL OF LH MAIN FUEL TANK CLIMB VENT TUBING FOUND LONGERON SHROUD LANDING CORRODED. REPAIRED CLIMB VENT TUBE LANDING IAW REO.SDR SWIA2019100246387Frame · crackedFRAME 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 SWIA2019100246386Angle · crackedANGLE 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 SWIA2019100246385Floor Support · corrodedLH 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 SWIA2019100246384Threshold · corrodedSERVICE DOOR THRESHOLD HAS CORROSION. REMOVED CORROSION IAW SRM.SDR SWIA2019100246383Panel · damagedPNL 684AB HAS ELONGATED SCREW HOLE. REPLACED UNSERVICEABLE PANEL 684AB IAW SRM.SDR SWIA2019100246382Bulkhead Web · damagedFS 621.00 FWD FACE OF RPB, RBL42, WL77. DAMAGED BY CONTACT WITH BULKHEAD ATTACH HDWR. PERFORMED REPAIR IAW REO.SDR SWIA2019100246381Skin · scratchedAFT 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.
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