N457SW

Service difficulty reports · 147

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 = 'N457SW' 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.

SDR SWIA2026042076115Skin · corrodedCORROSION FOUND AROUND FASTENERS ON SKIN BETWEEN STR 23R AND 24R @ FRAME 559+96. PERFORMED BLEND REPAIR AROUND FASTENERS ON SKIN BETWEEN STR 23R AND 24R @ FRAME 559+96 IAW REO 601R-53-51-740 REV--Apr 20, 2026 · N457SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2026042076113Skin · corrodedEXTERIOR SKIN CORRODED BETWEEN FS 559+80 AND FS559+96 AT STRINGERS 21R AND 23R. COMPLIED WITH BLEND REPAIR TO EXTERIOR SKIN BETWEEN FS559+80 - FS559+96 AT STGR 21R AND 23R IAW REO 601R-53-51-740 REV--. COMPLETE TASK CARD 51-900-1003-SKY.Apr 20, 2026 · N457SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2026030676134Window Frame · crackedCOPILOT WINDSHIELD UPPER SILL AFT WEB HAS A CRACK LOCATED I/B OF THE RH WINDSHIELD SIDE POST. REPAIRED COPILOT WINDSHIELD UPPER SILL AFT WEB BY CUTTING AWAY DAMAGE AND REPAIRING AREA IAW REO 601R-53-11-4062 REV-- . COMPLETED TASK CARD 51--900-1003-SKY.Mar 6, 2026 · N457SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2026022876125Intercostal · chafedLEFT OVERWING EMERGENCY EXIT CUTOUT SURROUND INTERCOSTAL CHAFED BETWEEN FS439 TO FS449.85, STGR 9L AND STGR 10L. REMOVED AND REPLACED INTERCOSTAL LOCATED AT LH OVERWING EE CUTOUT SURROUND BETWEEN FS439-449.85 STGR9L AND 10L IAW SRM 51-42-06.Feb 28, 2026 · N457SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2026022776133Landing · corrodedLEFT WING FUEL PANEL CUTOUT LANDING UNDER 510AB CORRODED. REPAIRED CORROSION ON LH WING FUEL PANEL 510AB CUTOUT LANDING IAW REO 601R-57-21-030- REV L DATED 2014-02-05Feb 27, 2026 · N457SW · Cndair CL6002B19 · Wing Main, Frame StructureSDR SWIA2026022776118Landing · corrodedRH WING FUEL PANEL CUTOUT LANDING UNDER 650CB CORRODED. REPAIRED CORROSION ON RH WING FUEL PANEL 650CB LANDING IAW REO 601R-57-21-030- REV L DATED 2014-02-05. COMPLETED TASK CARD 51-900-1003-SKYFeb 27, 2026 · N457SW · Cndair CL6002B19 · Wing Main, Frame StructureSDR SWIA2026022676129Floor Support · corrodedRIGHT CABIN PRESSURE FLOOR SILL IS CORRODED AT FS500 RBL 45. REPAIRED RT CABIN PRESSURE FLOOR SILL BY REMOVING CORROSION AND REPAIRING AREA AT BS 500, RBL 45 IAW REO 601R-53-41-3415 REV-- DATED 2026-05-11.Feb 26, 2026 · N457SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2026022676128Floor Support · corrodedLT CABIN PRESSURE FLOOR SILL IS CORRODED AT LBL43 FS 476. REMOVED CORROSION BY BLENDING LH CABIN PRESSURE FLOOR SILL AT LBL43 FS 476 IAW BOMBARDIER REO 601R-53-41-666 REV C DATED 2012-11-06.Feb 26, 2026 · N457SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2026022676124Floor Support · corrodedRIGHT CABIN PRESSURE FLOOR SILL IS CORRODED AROUND SCREW HOLE AT \RBL 45 FS520. REPAIRED RH CABIN PRESSURE FLOOR SILL BY REMOVING CORROSION AND REPAIRING AREA AT FS 520 RBL 45 IAW REO 601R-53-41-3415 REV-- DATED 2026-05-11. COMPLETED TASK CARD 51-900-1003-SKYFeb 26, 2026 · N457SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2026022676122Floorbeam · corrodedLH CABIN PRESSURE FLOOR ANGLE IS CORRODED AT FS 501 LBL 42. REMOVED CORROSION BY BLENDING AT LH CABIN PRESSURE FLOOR ANGLE FS 501 LBL 42 IAW REO 601R-53-41-666 REV-C DATED 2012-11-06. COMPLETED TASK CARD 51-900-1003-SKY.Feb 26, 2026 · N457SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2026022676117Floor Support · corrodedLH CABIN PRESSURE FLOOR SILL IS CORRODED AT FS 449.87 LBL 45. PERFORMED A MAJOR REPAIR TO THE LH PRESSURE FLOOR SILL AT FS 449.87 IAW REO 601R-53-41-666 REV-C DATED 2012-11-06Feb 26, 2026 · N457SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2026022676116Floor Support · corrodedLEFT CABIN PRESSURE FLOOR SILL IS CORRODED AT FS518 LBL 45. REMOVED CORROSION BY BLENDING AT LH CABIN PRESSURE FLOOR ANGLE FS 518 LBL 45 IAW REO 601R-53-41-666 REV-C DATED 2012-11-06.Feb 26, 2026 · N457SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2026022676112Floor Support · corrodedRIGHT CABIN PRESSURE FLOOR SILL IS CORRODED AT FS506 RBL 42. REPAIRED RT CABIN PRESSURE FLOOR SILL BY REMOVING CORROSION AND REPAIRING AREA AT FS 506 RBL 42 IAW MHIRJ REO 601R-53-41-3415 REV-- DATED 2026-05-11. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHEDFeb 26, 2026 · N457SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2026022476135Frame · corrodedBS 333 FRAME IS CORRODED AT STGR 23R. INSTALLED NEW SERVICEABLE RH LOWER FRAME SEGMENT OF BS 333 IAW SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY.Feb 24, 2026 · N457SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2026022476131Frame · corrodedBS 319 FRAME IS CORRODED BETWEEN STGR 26R TO STGR 25R. REPLACED FS 319 FRAME SECTOR FROM STGR 23L-23R IAW SRM 51-42-06 AND 51-42-21.Feb 24, 2026 · N457SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2026022476130Intercostal · corrodedAVI DOOR FWD INTERCOSTAL IS CORRODED BETWEEN STGR 27 TO STGR 26R. REPLACED AVI DOOR INTERCOSTAL PN:601R31049-10 IAW SRM 51-42-06 AND 51-42-21.Feb 24, 2026 · N457SW · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR SWIA2026022476119Frame · corrodedBS 333 FRAME IS CORRODED BETWEEN STGR 20L TO STGR 21L. LOCATED DRILLED AND INSTALLED NEW SERVICEABLE FS 333 LH SIDE FRAME SEGMENT IAW SRM 51-40-11, 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY.Feb 24, 2026 · N457SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2026022476114Stringer · corrodedSTGR 23R IS CORRODED BETWEEN F.S. 319 TO F.S. 333. UPON FURTHER INVESTIGATION FOUND CORROSION TO BE ON FS333 SPLICE STRAP AND STGR23R LAP JOINT. COMPLIED WITH BLEND REPAIR TO FS333 SPLICE STRAP AND STGR23R LAP JOINT IAW MHIRJ REO 601R-53-21-3803 REV --. COMFeb 24, 2026 · N457SW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA2026022376138Skin · corrodedEXTERIOR SKIN CORRODED IN SEVERAL AREAS FS559+80 TO FS559+112 STRINGER 26L TO 26R. PERFORMED REPAIR BY BLENDING CORROSION IAW REO 601R-53-51-734 REV-A DATED 2026-04-23.Feb 23, 2026 · N457SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2026022376132Skin · chafedRT LOWER WING PLANK IS CHAFED AT RBL45. COMPLIED WITH REPAIR TO LOWER WING PLANK CHAFE AT RBL45 IAW REO 601R-57-21-880 REV -D DATED 2017-03-06.Feb 23, 2026 · N457SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2026022376121Skin · chafedLEFT LOWER WING PLANK IS CHAFED AT LBL45. COMPLIED WITH BLEND REPAIR TO LOWER WING PLANK CHAFE AT LBL45 IAW REO 601R-57-21-880 REV -D DATED 2017-03-06.Feb 23, 2026 · N457SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2026021776126Hinge Fitting · gougedPAX DOOR HINGE ON THE FUSELAGE SIDE 11TH, 13TH, 14TH LUGS FROM FWD SIDE OF HINGE ARE GOUGED. REPLACED PAX DOOR HINGE ON THE FUSELAGE SIDE IAW SRM 53-21-23 AND REO 601R-53-21-656 REV--DATED 2024-03-15. COMPLETED TASK CARD 51-900-1003-SKY .Feb 17, 2026 · N457SW · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA2026021776123Pan · corrodedSERVICE DOOR LOWER PAN IS CORRODED. INSTALLED NEW SERVICEABLE SERVICE DOOR PAN P/N:601R38437-2 IAW CRJ 200 SRM 51-42-06, 51-42-13, 51-42-21, 51-40-11 AND 51-42-22. COMPLETED TASK CARD 51-900-1003-SKY.Feb 17, 2026 · N457SW · Cndair CL6002B19 · Service DoorsSDR SWIA2026021776120Hinge · gougedPAX DOOR HINGE ON THE DOOR SIDE 11TH, 12TH, 13TH, 16TH LUG LANDINGS FROM FWD SIDE OF HINGE ARE GOUGED. REMOVED UNSERVICEABLE PAX DOOR HINGE ON THE DOOR SIDE AND REPLACED WITH A SERVICEABLE HINGE IAW SRM 52-10-31. CFeb 17, 2026 · N457SW · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA2026020176127Post · failed inspFS409+128 BL0 VERTICAL POST RH & LH SIDES HAVE INDICATIONS: LH IS 60% FSH .3? LONG, AND RH IS 50% FSH .3? LONG IN THE AFT RADIUS OF POST @ WL69. FAILED NDT INSPECTION. INSTALLED NEW SERVICEABLE BL0 VERTICAL POST LH AND RH ANGLES AND LH/RH STIFFENERS AT FS 40Feb 1, 2026 · N457SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2026012476136Skin · chafedHORIZONTAL STAB UPPER SURFACE RBL 6.0 APPROXIMATELY 4 INCHES FROM FWD EDGE THERE ARE 2 CHAFES, ONE ON SUPPORT ANGLE FOR FAIRING AND ONE ON SPLICE DOUBLER. PERFORMED BLEND OUT AND DOUBLER REPAIR TO HORIZONTAL STAB UPPER SURFACE RBL6.0 IAW MHIRJ REO 601R-55-822Jan 24, 2026 · N457SW · Cndair CL6002B19 · Horizontal Stabilizer, Plate/SkinSDR SWIA2025092476137Floor Panel · corrodedTHE LH PRESSURE FLOOR PANEL BETWEEN FS 409+128 AND FS 559 HAS MULTIPLE SPOTS OF CORROSION. REPAIRED LT PRESSURE FLOOR PANEL BETWEEN FS 409+128 AND FS 559 REF REO 601R-53-41-666 REV C DATED 2012-11-06. COMPLIED WITH 51-900-1003-SKY DETAILED VISUAL INSPECT BLENSep 24, 2025 · N457SW · Cndair CL6002B19 · Fuselage Floor PanelSDR SWIA2025F01361Attach Fitting · gougedL/H WING AFT ATTACHMENT FITTING AT WS264.0 HAS GOUGING ON THE CENTER TWO LUGS. (MARKED) (S/N#00603) (C-CHECK RO 09/24/2025)BLENDED-OUT DAMAGES TO SMOOTH CONTOUR ON L/H WING AFT ATTACHMENT FITTING FOR HINGE BOX WS264.0 AT I/B AND O/B CENTER LUGS. REF. CRJ200 SAug 1, 2025 · N457SW · Cndair CL6002B19 · Wing, Fuselage Attach FittingsSDR SWIA202266947Skin · damagedREMOVE AND REPLACE LEFTHAND INBOARD FLAP VANE SKIN PANEL P/N: 601R14303-51S (C-CHECK) REMOVED AND REPLACED LH INBD FLAP VANE SKIN PANEL P/N 601R14303-51S REF DWG #PL601R14302 REV.E AND CRJ 200 SRM 51-42-13 REV.39 DATED MAR-10-2021. COMPLIED WITH TASK CANov 17, 2022 · N457SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202266946Skin · damagedREMOVE AND REPLACE RIGHTHAND INBOARD FLAP VANE SKIN PANEL P/N: 601R14303-54S (C-CHECK) REMOVED AND INSTALLED NEW SKIN PANEL P/N: 601R14303-54S AT RIGHTHAND INBOARD FLAP VANE REF CRJ200 SRM 51-42-13 AND DWG# PL601R14302 REV E, COMPLIED WITH TASKCARD 51-Nov 17, 2022 · N457SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202266945Skin · wornREMOVE AND REPLACE RIGHTHAND INBOARD FLAP VANE SKIN PANEL P/N: 601R14303-52S (C-CHECK RO 12/1/2022) REMOVED WORN LEADING EDGE VANE CAP AND INSTALLED NEW R/H MID FLAP VANE SKIN P/N: 601R14303-52. REF: CRJ 200 SRM 51-42-13 AND DWG 601R14302 REV. E. COMPLINov 17, 2022 · N457SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202266944Support Bracket · crackedAFT CARGO DOOR FWD TRACK LOWER SUPPORT BRACKET IS CRACKED (C-CHECK RO 12/1/2022) REMOVED AND INSTALLED NEW AFT CARGO DOOR FWD TRACK LOWER SUPPORT BRACKET ASSY REF DWG # 601R35050 REV AC, REF CRJ200 SRM 51-42-06, SRM 51-41-02. COMPLIED WITH 51-900-1003-SNov 6, 2022 · N457SW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR SWIA202265258None · failedL MAIN AND R MAIN DID NOT COME DOWN WHEN LANDING GEAR WERE LOWERED ON APPROACH. THE F/A HEARD A BANG OR POP FOLLOWED BY A GRINDING SOUND ON TAKEOFF/DEPARTURE. SHE INFORMED US OF THIS AT 10,000 FEET OUT OF STERILE COCKPIT. WITH NO ABNORMAL MESSAGES OR PRESSURIZMar 31, 2022 · N457SW · Cndair CL6002B19 · Landing Gear Door ActuatorSDR SWIA202265257None · failedL MAIN AND R MAIN DID NOT COME DOWN WHEN LANDING GEAR WERE LOWERED ON APPROACH. THE F/A HEARD A BANG OR POP FOLLOWED BY A GRINDING SOUND ON TAKEOFF/DEPARTURE. SHE INFORMED US OF THIS AT 10,000 FEET OUT OF STERILE COCKPIT. WITH NO ABNORMAL MESSAGES OR PRESSURIZMar 31, 2022 · N457SW · Cndair CL6002B19 · Landing Gear Door ActuatorSDR SWIA202161607Sensor · obstructedPERFROM FULL FLAP FAIL AD 2009-06-12 WITH IN 10 FC DUE TO FLAPS FAILED AT 20 ON ARRIVAL. C:MCI / DUE TAC 34821, FLAPS FAILED AT 20 ON ARRIVAL. CLOSED RESET AND OPERATED FLAPS 5 FULL CYCLES AND COMPLETED AD 2009-06-12/10 COMPLIANCE FORM. OK TO CONTINUE IN SEROct 5, 2021 · N457SW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR SWIA2019102346557Frame · corrodedL/H FUSELAGE FRAME HAS CORROSION ON UPPER SURFACE, JUST ABOVE FLOOR LEVEL. (C-CHECK) RO: 10/20. COMPLIED WITH STRUCTURAL MAJOR REPAIR.Oct 22, 2019 · N457SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2018091845080Actuator · failedGEAR DISAGREE WARNING AFTER PUTTING GEAR DOWN FOR LANDING. (FLT 7438) CLOSED REMOVED AND REPLACED NLG DOOR ACTUATOR IAW AMM. PERFORMED GEAR SWINGS AND EMERGENCY EXTENSION CHECK IAW AMM. OPS CHECK GOOD.Sep 18, 2018 · N457SW · Cndair CL6002B19 · Landing Gear Door Retract SectionSDR SWIA2018061544781Engine · failedLOST RIGHT ENGINE RESPONSE JUST OUTSIDE OF THE FINAL APPROACH FIX WHEN RIGHT THRUST LEVER WAS ADVANCED. RIGHT ENGINE SPOOLED DOWN AND ITT WENT RED. ACCOMPLISHED ENGINE SHUTDOWN IN FLIGHT. (FLT 7423) 06/15/2018 CLOSED REMOVED AND REPLACED RT ENGINE. OPS AND LEAJun 15, 2018 · N457SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA2017100243806Pressure Deck · corrodedRIGHT PRESSURE FLOOR BS 520 HAS CORROSION. REMOVED THE CORROSION IAW REO AND SRM.Aug 27, 2017 · N457SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2017100243805Skin · chafedLEFT AILERON LOWER LEADING EDGE SKIN CHAFED INBD OF CENTER HINGES. REMOVED AND REPLACED THE AILERON LOWER LEADING EDGE SKIN PANEL IAW SRM.Aug 24, 2017 · N457SW · Cndair CL6002B19 · AileronsSDR SWIA2017100243804Vane · chafedRIGHT INBOARD FLAP VANE SKIN LEADING EDGE CHAFED. REMOVED AND REPLACED THE RT INBD FLAP LEADING EDGE VANE IAW SRM.Aug 23, 2017 · N457SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2017100243803Vane · chafedLEFT INBOARD FLAP VANE SKIN LEADING EDGE HAS TWO CHAFED AREAS. REMOVED AND REPLACED THE LT INBD FLAP, OTBD SIDE LEADING EDGE VANES IAW SRM.Aug 23, 2017 · N457SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201439675Adg · unwanted deployADG DEPLOYED ON WEIGHT OFF WHEELS. ALL OTHER SYSTEMS NORMAL. COMPLIED WITH INSPECTION AFTER ADG - INFLIGHT DEPLOYMENT IAW AMM. INSPECTION CK GOOD. ADG AUTO DEPLOYMENT PANEL FAILED OPS CK. R & R ADG AUTO DEPLOYMENT CONTROL PANEL IAW AMM. OPS CK OF ADG AUTOct 26, 2014 · N457SW · Cndair CL6002B19 · AC Generation SystemSDR SWIA201439484Element · brokenANTI-ICE DUCT WARNING 1000' AFTER T/O. RAN QRH, MSG PERSISTED FOR 15 MIN THEN WENT OUT. RETURN TO FIELD. SHUTDOWN LT ENGINE TAXIING IN, LT FUSELAGE ANTI-ICE DUCT MSG RETURNED. R & R BROKEN SENSING ELEMENT IN THE LT WHEEL WELL IAW AMM, PN 35548-3-255.Oct 12, 2014 · N457SW · Cndair CL6002B19 · Pneumatic Indicating SystemSDR SWIA201439239Smoke Detector · no testCARGO BOTTLE, TEST 2 INOPERATIVE. NO MASTER WARNING, RED "SMOKE CARGO" EICAS ANNUNCIATION, OR CARGO SMOKE PUSH BUTTON LIGHTS ON FIRE EXTINGUISHER CONTROL PANEL. SQUIB CHECKS GOOD. R & R CARGO SMOKE DETECTOR 2 IAW AMM. CARGO SMOKE DETECTION SYSTEM, OPS CHECKSep 1, 2014 · N457SW · Cndair CL6002B19 · Smoke DetectionSDR SWIA201438459Window · crackedCAPTAIN'S SIDE WINDOW CRACKED CLIMBING OUT OF 7,000-8,000'. R & R SIDE WINDOW IAW AMM. PN ON: NP-139322-11, SN ON:13213H4868, PN OFF: NP-139322-001, SN OFF: 02329H1945.Jun 27, 2014 · N457SW · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA201436640Battery · dischargedOVERHEAD EMERGENCY LIGHT BY EXIT DOES NOT ILLUMINATE. SERVICE REPLACED THE NR 2 EMERGENCY BATTERY ASSEMBLY, PN AD-2013-1A, SN ON 69013 & SN OFF 50481.Mar 7, 2014 · N457SW · Cndair CL6002B19 · Emergency LightingSDR SWIA201435846Uplock · failedGEAR DISAGREE WARNING MESSAGE AFTER RETRACTING THE GEAR. AFTER QRH PROCEDURE, GEAR INDICATED DOWN, 3 GREEN. FLT 4760 REPLACED LT MLG UPLOCK ASSEMBLY IAW AMM. SWUNG GEAR, PERFORMED EMERGENCY EXTENSION & CONSECUTIVE SWINGS, OPERATIONS CHECKED GOOD.Jan 4, 2014 · N457SW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA201335152Door · chafedRT MLG DOOR CHAFED ON LE CORNER. C-CHECK REPAIRED MLG DOOR RT IAW REO.Oct 26, 2013 · N457SW · Cndair CL6002B19 · Landing Gear DoorsSDR SWIA201335153Flap · dentedLT INBD FLAP DENTED APPROXIMATELY 11 INCHES FROM OTBD EDGE ON THE TE. C-CHECK REPAIRED LT INBD FLAP BY REPLACING TE STRIP IAW SHORTS DRAWING.Oct 21, 2013 · N457SW · Cndair CL6002B19 · Trailing Edge Flaps
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