N455SW

Service difficulty reports · 196

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 = 'N455SW' 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 SWIA2026043077188Intercostal · corrodedPAX DOOR, CENTER INTERCOSTAL DD4 WAS CORRODED. PAX DOOR, CENTER INTERCOSTAL DD4 WAS REMOVED & REPLACED WITH A NEW ONE IAW SRM 51-42-06-00, & SRM 51-42-21-00. COMPLETED TASK CARD 51-900-1003-SKY. NO WEIGHT CHANGE. REF CONTINUATION CARD FOR WORK PERFORMED.Apr 30, 2026 · N455SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026043077181Intercostal · corrodedPAX DOOR, CENTER INTERCOSTAL DD3 IS CORRODED. PAX DOOR, CENTER INTERCOSTAL DD3 WAS REMOVED AND REPLACED WITH A NEW ONE IAW SRM 51-42-06-00 AND SRM 51-42-21-00. COMPLETED TASK CARD 51-900-1003-SKY. NO WEIGHT CHANGE, REF CONTINUATION CARD FOR WORK PERFORMED.Apr 30, 2026 · N455SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2026042877170Skin · chafedCARGO DOOR OUTER SKIN WAS CHAFED, AT TOP OF DOOR FROM CONTACT WITH CARGO LINER HARDWARE. REPAIRED THE CARGO DOOR OUTER SKIN CHAFE DAMAGE IAW REO 601R-52-32-451, REV -.Apr 28, 2026 · N455SW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR SWIA2025030777185Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE RA95454-601R-53-11-3962 MXCODEID106127-PR - TEMPORARY DISPOSITION FOR DENT DAMAGE ON FUSELAGE SKIN PANEL FWD OF BS 280 AND ABOVE STR 6L. SUBJECT CONDITION IS ACCEPTABLE FOR 500 FH FROM TIME OF INCORPORATION OF REO 601R-53Mar 7, 2025 · N455SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2025030777173Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE RA73304-601R-53-11-3730 455SW MXCODEID59029-PR - DENT ON RT FUSELAGE NOSE SKIN AT FS21000 BETWEEN STR 12R AND 13R COMPLIED WITH TEMPORARY DISPOSTION PER REO 601R-53-11-3730 REV -- DATED 2021-10-03 PERMANENT REPAIR DUE WITMar 7, 2025 · N455SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2024080700006Gauge · fluctuatesL ENG OIL PRESS MASTER WARNING AT CRUISE ALTITUDE. OIL PRESS GAUGE CYCLED IN AN OUT OF LOW PRESSURE. COMPLETED QRH, WITH ENG AT IDLE MASTER WARNING CONTINUED AND OIL PRESS GAUGE CONTINUED TO CYCLE IN AND OUT OF LOW PRESS INDICATION. DIVERTED TO KRAP. NO OTHER Aug 6, 2024 · N455SW · Cndair CL6002B19 · Engine Oil PressureSDR SWIA2024040300002Window Frame · crackedCRACKED FRAME AROUND WINDOW BY SEAT 13BC: DEFERRED SEAT 13B WINDOW TRIM USING NEF-CAB-6D. SHARP EDGES COVERED WITH TAPE. NO FURTHER DISCREPANCIES FOUND. PLACARD PLACEDCAT: CDUE DATE: 11 APRIL 2024CRACKED FRAME AROUND WINDOW BY SEAT 13B (FILED CLOSED)REMOVED ANApr 2, 2024 · N455SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2024032600005Floor Support · damagedNUTPLATE RIVET HOLES DAMAGED IN PRESSURE FLOOR SILL ASSEMBLY BETWEEN FS349.00 - FS449.85 AND LBL36.00 0 LBL45.00. (C-CHECK RO 3/24/2024) REPAIRED DAMAGE TO PRESSURE FLOOR SILL BETWEEN FS349.00 - FS449.85 AND LBL36.00 0 LBL45.00 IN REF TO REO 601R-53-41-321Mar 5, 2024 · N455SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2024032600002Skin · dented2 SMALL DENTS WITH GOUGES/CREASES NOTED JUST AFT OF FS 640.00 AND ADJACENT TO STRINGER 25R. (C-CHECK RO 3/24/2024) REPAIRED DENT / GOUGE DAMAGE TO FUSELAGE SKIN BETWEEN FS621.00 - FS654.50 AND BETWEEN STR23R - STR26R IN REF TO REO 601R-53-61-8167 REV--, DAMar 2, 2024 · N455SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2024032600028Floor Support · corrodedSURFACE CORROSION FOUND AT SEVERAL FS LOCATIONS ON THE L/H PRESSURE FLOOR SILL ASSY ADJACENT TO LBL 36.00. LOCATIONS ARE AS FOLLOWS: FS 435, FS 439, FS 447, FS 451, 6 BETWEEN FS 473-FS 479, FS 500, FS 505, FS 522, FS 531, FS 537, FS 540, FS 544, FS 559 (C-CFeb 28, 2024 · N455SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2024032600026Bracket · crackedAFT SIDE OF FS621.00 JUST OUTBOARD OF RBL 36.20 AND INLINE WITH STRINGER 15R, INTERCOSTAL CRACKED. (C-CHECK RO 3/24/2024) REMOVED AND REPLACED INTERCOSTAL ON THE AFT SIDE OF FS621.00 JUST OUTBOARD OF RBL 36.20 AND INLINE WITH STRINGER 15R IN REF TO SRM 51-Feb 26, 2024 · N455SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202403260025Angle · corrodedFOUND CORROSION ON THE PAX DOOR ANGLE OF THE FUSELAGE PAX DOOR CUT OUT SURROUND STRUCTURE.-REF. SRM 53-21-23-00 PAGE 5 ITEM #56B PN: 601R31527-221 (C-CHECK RO 3/24/2024) REMOVED AND REPLACED PAX DOOR SILL ANGLE IN REF TO SRM 51-42-06 AND 51-42-21. APPLIEDFeb 25, 2024 · N455SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2024032600024Pressure Blkhd · gougedAFT PRESSURE BULKHEAD (FS621.00) FWD FACE HAS 6 GOUGES AND 7 GOUGED RIVET HEADS IN THE WEB DOUBLERS AT RBL 36.20, RBL 27.50, RBL 18.00, RBL9.50, LBL 9.50, LBL 18.00, LBL 27.50, AND LBL 36.20. (C-CHECK RO 3/24/2024) BLENDED 6 GOUGES AND REPLACED 7 GOUGED RIFeb 24, 2024 · N455SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA202265644None · failedD:GEAR DISAGREE. NOSE GEAR WOULD NOT RETRACT. WOW INPUT CAUTION MESSAGE. STEERING INOP MESSAGE. LANDED OVER WEIGHT AT 49500 LBS TOUCH DOWN AT LESS THAN 100FT/MIN / C:MEL 32-30-1 / CAT A DUE WITHIN 1 FLIGHT DAY / NOTE:MX ACTION C/W / ***** REPEAT ODIMay 20, 2022 · N455SW · Cndair CL6002B19 · Landing Gear Door ActuatorSDR SWIA202265623None · failedRECEIVED GEAR DISAGREE WARNING MESSAGE. BOTH MAINS RETRACTED BUT NOT THE NOSE GEAR. COMPLETED QRH PROCEDURE. LANDED BACK IN DEN WITHOUT ANY PROBLEMS. (FLIGHT 5111 - FILED CLOSED) PLEASE REFERENCE AML 911332 REMOVED AND REPLACED NLG SELECTOR VALVE PER AMMMay 18, 2022 · N455SW · Cndair CL6002B19 · Landing Gear Door ActuatorSDR SWIA202154934Hydraulic System · leakingUPON GEAR EXTENSION, GEAR DISAGREE WARNING MESSAGE AND HYD 3 LO PRESS CAUTION MESSAGE WITHIN 6 SECONDS. NOSE GREEN, MAINS YELLOW WITH XS. ATTEMPTED TO CYCLE GEAR WITHIN ABOUT 30 SECONDS, SAME RESULT. MANUALLY EXTENDED GEAR. THREE GREEN GEAR. HYD 3 SYSTEM Jan 2, 2021 · N455SW · Cndair CL6002B19 · Hydraulic System, MainSDR SWIA2019091146277Stringer Splice · corrodedSPLICE STRAP AT STR 23R AND BETWEEN FS 310 AND FS 333 IS CORRODED. (C-CHECK) RO: 09/10/2019 COMPLIED WITH PERMANENT REPAIR IAW REO.Aug 21, 2019 · N455SW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA2019091146276Frame · corrodedFRAME AT FS319, STR23R CORRODED. (C-CHECK) RO: 09/10/2019 INSTALLED NEW FRAME SPLICE PN 601R32003-25 AT FS 310.0 & STRINGER 23R IAW SRM.Aug 19, 2019 · N455SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2019091146275Frame · corrodedFRAME AT FS 310 , STR 23R CORRODED AT LOWER SPLICE. (C-CHECK) RO: 09/10/2019 REWORKED FRAME 310 AT STR 23 AND COMPLIED WITH ALL STEPS IAW REO. LEAK CHECKS GOOD.Aug 19, 2019 · N455SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2019091146274Frame · corrodedFS 310 FRAME BETWEEN STR 26R- 26L CORRODED. (C-CHECK) RO: 09/10/2019 REWORKED 310 FRAME AND COMPLIED WITH ALL STEPS IAW REO. LEAK CHECKS GOOD.Aug 19, 2019 · N455SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2019091146273Floor Support · corrodedBL9R FLOOR BEAM INBOARD & OUTBOARD FLANGES HAVE CORROSION FS569.00 - FS608.00. (C-CHECK) RO: 09/10/2019 REMOVED AND REPLACED NEW FLOOR BEAM CAP IAW REO AND SRM.Aug 15, 2019 · N455SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019091146272Buttstrap · corrodedBUTT STRAP AT FS 333 FROM STR 23L TO STR 23R PN#601R31022-9 CORRODED AT MULTIPLE LOCATIONS. (C-CHECK) RO: 09/10/2019 REMOVED AND INSTALLED NEW BUTT STRAP AT FS 333, BETWEEN STR 23L TO STR 23R IAW REO AND SRM.Aug 10, 2019 · N455SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019091146271Strap · corrodedCORROSION ON STRAP FS559.00, BL27L - BL42L. (C-CHECK) RO: 09/10/2019 REMOVED AND REPLACED STRAP P/N 601R31025-29 IAW AMM.Aug 9, 2019 · N455SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019091146265Trunnion · damagedHOLE #14 ON RT MLG TRUNNION OVERSIZED AT .340". (C-CHECK) RO: 09/10/2019 REPAIRED RT TRUNNION HOLE #14 IAW REO.Aug 9, 2019 · N455SW · Cndair CL6002B19 · Main Landing Gear Attach SectionSDR SWIA2019091146264Trunnion · damagedHOLE #14 LT MLG TRUNNION OVERSIZED AT .340". (C-CHECK) RO: 09/10/2019 COMPLIED WITH PERMANENT REPAIR HOLE #14 IAW REO.Aug 9, 2019 · N455SW · Cndair CL6002B19 · Main Landing Gear Attach SectionSDR SWIA2019091146270Frame · corrodedFS 349 CORROSION ON FRAME BETWEEN STR 26L-27. (C-CHECK) RO: 09/10/2019 COMPLIED WITH STEPS OF PERMANENT REPAIR IAW REO.Aug 7, 2019 · N455SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2019091146269Floor Support · corrodedCORROSION ON THE INNER & OUTER FLANGES OF THE BL27L FLOORBEAM FS559.00+80 - FS569.00. (C-CHECK) RO: 09/10/2019 REPAIRED FLOORBEAM IAW SRM AND REO.Aug 7, 2019 · N455SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019091146268Door Sill · corrodedLEFT HAND FLOOR SILL MULTIPLE AREAS OF CORROSION, FS559.00+84 - FS562.00. (C-CHECK) RO: 09/10/2019 REPLACED LEFT FLOOR IAW REO.Aug 7, 2019 · N455SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019091146267Doubler · corrodedDOUBLER ON RIGHT FLOOR SILL CORRODED, FS310.00 - FS319.00. (C-CHECK) RO: 09/10/2019 INSTALLED NEW DOUBLER AT RT FLOOR SILL AT FS 310.00 - FS 319.00 IAW SRM.Aug 5, 2019 · N455SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019091146266Door Sill · corrodedRIGHT FLOOR SILL CORRODED, FS310.00 - FS319.00. (C-CHECK) RO: 09/10/2019 REMOVED AND INSTALLED NEW RT SILL PLATE AT FS310 TO FS319 IAW SRM.Aug 5, 2019 · N455SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201904115735Pin · failedRECEIVED GEAR DISAGREE WARNING MSG ON APPROACH. (FLT#7418) CLOSED REMOVED AND REPLACED NLG UP LOCK PIN AND BRACKET IAW AMM. PERFORMED OPS CHECK GOOD AT THIS TIME.Apr 11, 2019 · N455SW · Cndair CL6002B19 · Nose/Tail Landing GearSDR SWIA201743688Frame · corrodedFRAME SECTOR AT BS 605 BETWEEN STRINGERS 20L AND 20R HAS OUT OF LIMITS CORROSION. REMOVED AND INSTALLED A NEW LOWER FRAME SECTOR IAW SRM. NO LEAKS NOTED.Aug 8, 2017 · N455SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA201743687Web · corrodedPAX DOOR AFT WEB HAS CORROSION. REMOVED AND REPLACED THE WEB IAW SRM. OPS TESTED GOOD.Aug 4, 2017 · N455SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA201743686Web · corrodedPAX DOOR FWD STAIR WEB HAS CORROSION. REMOVED AND REPLACED THE STAIR WEB IAW SRM. OPS TESTED GOOD.Aug 4, 2017 · N455SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA201743685Angle · bentPASSENGER DOOR BOTTOM ANGLE FOUND BENT. REPLACED THE BOTTOM ANGLE IAW SRM.Aug 1, 2017 · N455SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA201743684Hinge · galledPAX DOOR FUSELAGE SIDE HINGE HAS GALLING BETWEEN EACH LUG. REMOVED AND INSTALLED NEW PASSENGER DOOR HINGE IAW SRM.Aug 1, 2017 · N455SW · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA201743683Door · chafedAFT CARGO DOOR LOWER SURROUND, HAS A DEEP CHAFE AND WEAR MARKS AT FWD SIDE. REMOVED AND INSTALLED A NEW UPPER AND UPPER DOOR COAMING IAW SRM. NO LEAKS NOTED.Jul 30, 2017 · N455SW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR SWIA201541394Frame · corrodedFS 349.0, AVIONICS BAY, FRAME FLANGE AT STR 27 HAS CORROSION. BELOW FLOORBOARD. REPLACED FS 349, FRAME FROM STR 23L-STR 23R WITH NEW FRAME AND INSTALLED NEW FRAME IAW SRM. LEAK CHECK GOOD.Jul 23, 2015 · N455SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA201541393Frame · corrodedAVIONICS BAY, FS 319.70, FRAME FLANGE HAS CORROSION AT STR 27. BELOW AVIONICS BAY FLOORBOARD. REPLACED LOWER FRAME AT FS 319 IAW SRM. LEAK CHECK GOOD.Jul 23, 2015 · N455SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA201439247Wire Harness · failedWOW INPUT CAUTION MESSAGE AFTER GEAR RETRACTION ALONG WITH LT OTBD BTMS INDICATOR DASHED. DURING GEAR EXTENSION, ANTI-SKID OTBD CAUTION MESSAGE AND PROX SYSTEM FAULT STATUS MESSAGE. R & R LT MLG OTBD HARNESS SUB ASSY, ANTI-SKID SUB HARNESS, AND ANTI SKID HARSep 4, 2014 · N455SW · Cndair CL6002B19 · Landing Gear System WiringSDR SWIA201438536Lamp · inoperativeNR 3 EMERGENCY LIGHT POD IS INOPERATIVE. REPLACED THE LAMP.Jul 4, 2014 · N455SW · Cndair CL6002B19 · Emergency LightingSDR SWIA201436761Charger · inoperativeEMERGENCY LIGHT AT PASSENGER INTERIOR WALL DOES NOT ILLUMINATE. REPLACED NR 2 EMERGENCY LIGHT BATTERY CHARGER IAW AMM.Mar 13, 2014 · N455SW · Cndair CL6002B19 · Emergency LightingSDR SWIA201334883Plate · damagedBLENDED AREA FOUND OUT OF LIMITS ON INBD SIDE PLATE ON RT INBD FLAP, INBD HINGE ARM. C-CHECK REPLACED INBD SIDE PLATE ON RT INBD FLAP ON INBD HINGE ARM IAW SRM.Sep 29, 2013 · N455SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201334873Sill · corrodedSERVICE DOOR LOWER SILL CORRODED IN SEVERAL AREAS, FOUR EACH WITH ONE LARGE PATCH OF CORROSION AROUND DOOR LUGS. C-CHECK REPLACED SERVICE DOOR LOWER SILL IAW SRM.Sep 29, 2013 · N455SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201334874Skin · chafedLT AILERON UPPER LE CHAFED BEYOND ALLOWABLE LIMITS. C-CHECK REPLACED LT AILERON UPPER LE SKIN IAW SRM.Sep 28, 2013 · N455SW · Cndair CL6002B19 · AileronsSDR SWIA201334878Structure · crackedFLOOR AT FWD LT SIDE EQUIPMENT COMPARTMENT CRACKED AT FS193.0. C-CHECK REPAIRED FWD LT SIDE EQUIPMENT COMPARTMENT CRACKED AT FS 193 IAW REO.Sep 25, 2013 · N455SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201334877Skin · corrodedCORROSION ON LT WING, WING PLANK ON ACCESS 540BB. C-CHECK BLENDED WING PLANK ON ACCESS 540BB IAW REO.Sep 25, 2013 · N455SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA201334876Vane · chafedLT INBD FLAP VANE CENTER LE IS CHAFED BEYOND LIMITS & NEEDS TO BE REPLACED. C-CHECK REPLACED WITH NEW LT INBD FLAP VANE CENTER LE, PN 601R14303-51S IAW SRM.Sep 25, 2013 · N455SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201334875Floorbeam · crackedFS 280 FLOOR BEAM WEB CRACKED AT RBL 9. C-CHECK REPAIRED FS 280 FLOOR BEAM WEB IAW REO.Sep 25, 2013 · N455SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA201334888Bulkhead · crackedLT FS 202.0 BULKHEAD CRACKED AT THE PARKING BRAKE CABLE CUTOUT. C-CHECK REPAIRED LT FS 202.0 BULKHEAD CRACK AT THE PARKING BRAKE CUTOUT IAW REO.Sep 24, 2013 · N455SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
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