N920SW

Service difficulty reports · 167

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 = 'N920SW' 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 SWIA202266123None · crackedTRANSFER FROM EAML 947626 : RIGHT (FO SIDE) WINDSHIELD CRACKED AFTER ARCHING WAS OBSERVED DURING THE DESCENT ( FLIGHT #5615 - FILED CLOSED) REPLACED RIGHT (FO SIDE) WINDSHIELD IN REFERENCE TO CRJ200 AMM. 56-11-01 AND TASK CARD 56-220-1000-SKY. OPERATIONALJul 12, 2022 · N920SW · Cndair CL6002B19 · Window/Windshield SystemSDR SWIA202158614Retainer · corrodedMAIN AVIONICS DOOR SEAL RETAINER TRACK HAS MULTIPLE AREAS OF CORROSION. (FILED CLOSED) REMOVED AND REPLACED ALL FOUR MAIN AVIONICS DOOR SEAL RETAINER SEGMENTS IN REF TO SRM 51-42-06.May 28, 2021 · N920SW · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR SWIA202158613Track · crackedCARGO DOOR FORWARD TRACK, LOWER SUPPORT BRACKET AT FS 574.00, WL 77.61 IS CRACKED. (FILED CLOSED) REMOVED AND REPLACED CARGO DOOR FORWARD TRACK, LOWER SUPPORT BRACKET AT FS 574.00, WL 77.61 IN REF TO SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY.May 27, 2021 · N920SW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR SWIA202158612Support Angle · crackedCARGO DOOR CUTOUT, UPPER BEAM AFT SUPPORT ANGLE IS CRACKED. FS 621.00 AT WL 115.08. (FILED CLOSED) REMOVED AND REPLACED CARGO DOOR CUTOUT, UPPER BEAM AFT SUPPORT ANGLE IN REF TO SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED M-337.May 27, 2021 · N920SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202158615Skin · corrodedSERVICE DOOR HAS CORRODED FASTENERS ON THE LOWER AFT CORNER AND UPPER FORWARD CORNERS OF THE INNER SKIN. (FILED CLOSED) REMOVED AND REPLACED CORRODED FASTENERS ON THE LOWER AFT CORNER AND UPPER FORWARD CORNERS OF THE SERVICE DOOR INNER SKIN IN REF TO SRMMay 26, 2021 · N920SW · Cndair CL6002B19 · Service DoorsSDR SWIA202156302Nut · looseRIGHT REV UNLOCKED IN FLIGHT, FLIGHT 5038 - FILED CLOSED. PLEASE REFERENCE AML 581409. THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 22323893 WITH THE FOLLOWING CORRECTIVE ACTION: BEFORE RIGGING THE RT ENGINE STOW MICRO SWITCH, FOUND THE JAM NUTS LOOSE CAUSIFeb 17, 2021 · N920SW · Cndair CL6002B19 · Engine Thrust ReverserSDR SWIA202051279Bpsu · failedWHEN CONFIGURING FOR APPROACH AND LAND INTO DENVER FLAPS FAIL CAUTION MESSAGE WHEN SELECTING FLAP 8. FLAPS WERE AT 0 FOR APPROACH, LANDED AT 42700 LBS AND AT 100 PFM VSI. FLIGHT 5791. INSTALLED NEW RH BPSU IN REF WITH AMM. OPS CHECK GOOD AT THIS TIME. FJun 29, 2020 · N920SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA2019122647104Engine · failedDURING CLIMB-OUT, LOSS OF NR 1 ENGINE AND LOUD BANG. ENGINE ITT WAS IN THE RED FOR ABOUT 15-20 SECONDS WITH NEEDLE FLUTTERING AT THE BOTTOM OF THE GAUGE. N1 AND N2 SPOOLED DOWN DURING THE FAILURE. CREW WAS NOT ABLE TO IDENTIFY ANY MESSAGES. AFTER ENGINE RESTARDec 22, 2019 · N920SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA2019080946177Gusset · corrodedCORROSION ON GUSSET ATTACHED TO FRAME 364 AT STR 26L. (C-CHECK) RO: 08/07/2019 REMOVED AND REPLACED GUSSET ATTACHED TO FRAME 364 AT STR 26L IAW SRM.Jul 31, 2019 · N920SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019080946172Gusset · corrodedCORROSION ON GUSSET ATTACHED TO FRAME 364 AT STR 26R. (C-CHECK) RO: 08/07/2019 REPLACED GUSSET ATTACHED TO FRAME 364 AT STR 26R IAW SRM.Jul 31, 2019 · N920SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019080946176Angle · corrodedCORROSION ON ANGLE ATTACHED TO AFT SIDE OF FRAME 364. (C-CHECK) RO: REMOVED AND REPLACED ATTACH ANGLE TO FRAME AT FS364 STGR 25L - STGR 25R IAW SRM.Jun 13, 2019 · N920SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019080946175Floorbeam · corrodedFLOOR BEAM AT FS 574 IS CORRODED AT THE L/H FLOOR SILL. (C-CHECK) REMOVED CORROSION ON FLOOR BEAM LOCATED AT FS574.00. C/W ALL STEPS OF REO.Jun 13, 2019 · N920SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2019080946174Floorbeam · crackedBOTH INBOARD AND OUTBOARD CLIPS ON THE BL9L FLOOR BEAM, AT THE FS280.00 BULKHEAD, ARE CRACKED. (C-CHECK) REPLACED INBOARD AND OUTBOARD CLIPS ON THE BL9L FLOOR BEAM, AT THE FS280.00 IAW REO.Jun 13, 2019 · N920SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2019080946173Fairing · chafedL/H FLAP STUB FAIRING IS CHAFED. (C-CHECK) REMOVED AND REPLACED L/H FLAP STUB FAIRING IAW SRM.Jun 6, 2019 · N920SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2018110945157Sensor · out of adjustON TAKEOFF NOSE GEAR DID NOT COME UP. LANDED WITHOUT INCIDENT. (FLT#5517) FO: 10/18/2018 CLOSED ADJUSTED NLG OLEO EXTENDED/CENTERED SENSOR IAW AMM. PERFORMED FULL STRUT SERVICE OF NLG IAW AMM.Oct 17, 2018 · N920SW · Cndair CL6002B19 · Landing Gear Position and WarningSDR SWIA2018101845157Not Reported · malfunctionedON TAKEOFF NOSE GEAR DID NOT COME UP. LANDED WITHOUT INCIDENT. (FLT 5517) FO: 10/18/2018 WORK IN PROGRESS.Oct 17, 2018 · N920SW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA2018102545137Sensor · out of adjustGEAR DISAGREE WARNING SHORTLY AFTER GEAR SELECTED UP FOLLOWED BY NOSE DOOR WARNING MESSAGE. THE NOSE GEAR WAS STILL SHOWING DOWN AND LOCKED. COMPLIED WITH QRH FOR GEAR DISAGREE UNTIL MANUAL RELEASE HANDLE STEP. BOTH HYDRAULIC 3B AND 2B PUMPS SELECTED ON. MESSAOct 15, 2018 · N920SW · Cndair CL6002B19 · Landing Gear Position and WarningSDR SWIA201743484Floorbeam · corrodedFLOORBEAM ANGLE CORRODED OUT OF LIMITS FWD AT BS 280 BETWEEN LBL 9 AND RBL 9. REMOVED AND REPLACED THE FWD FLOORBEAM ANGLE IAW SRM.Jun 22, 2017 · N920SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA201743490Bracket · corrodedPASSENGER DOOR SILL ANGLE. BOTH MOUNT BRACKETS FOR THE DOOR HARNESS BLOW OUT. INBD SIDE OF THE ANGLE. REMOVED AND REPLACED THE BRACKETRS IAW SRM.Jun 20, 2017 · N920SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA201743489Door Sill · corrodedLEFT DOOR SILL BS 310 - 349 HAS CORROSION. REMOVED AND INSTALLED A NEW DOOR SILL ANGLE IAW AMM.Jun 19, 2017 · N920SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201743488Door Sill · corrodedRIGHT DOOR SILL BS 319.7 - 349 HAS CORROSION. REMOVED DOOR SILL LOWER ANGLE AND INSTALLED A NEW ANGLE IAW SRM.Jun 19, 2017 · N920SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201743487Intercostal · corrodedPASSENGER DOOR INTERCOSTAL (HINGE SIDE OF DOOR) UNDER PANEL 832ER HAS CORROSION. INSTALLED A NEW INTERCOSTAL IAW SRM.Jun 16, 2017 · N920SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA201743486Skin · chafedRIGHT AILERON LOWER INBOARD FIXED LEADING EDGE SKIN CHAFED. REPAIRED IAW REO.Jun 16, 2017 · N920SW · Cndair CL6002B19 · AileronsSDR SWIA201743485Skin · chafedRH AILERON LOWER OUTBOARD FIXED LEADING EDGE CHAFED. REPAIRED IAW REO.Jun 16, 2017 · N920SW · Cndair CL6002B19 · AileronsSDR SWIA201541315Floor Panel · crackedFLOOR PANEL 222FLW CRACKED AT SCREW HOLE. REPAIRED THE COCKPIT FLOOR PANEL IAW EA.May 29, 2015 · N920SW · Cndair CL6002B19 · Fuselage Floor PanelSDR SWIA201541317Bulkhead Web · damagedBS 621 AFT PRESSURE BULKHEAD FWD SIDE, DEFECTS NOTED AT RBL 27.50, RBL 18.00, RBL 9.50, LBL 18.00, LBL 27.50, LBL 36.20 BETWEEN WL 120.43 AND WL 73.50. REPAIRED THE PRESSURE BULKHEAD IAW REO.May 24, 2015 · N920SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA201541314Skin · gougedSERVICE DOOR OUTER SKIN GOUGED AT EXTERNAL HANDLE CUT OUT. REPAIRED SERVICE DOOR OUTER SKIN GOUGES AT EXTENAL HANDLE CUT OUT IAW EA.May 24, 2015 · N920SW · Cndair CL6002B19 · Service DoorsSDR SWIA201541312Door Sill · crackedFOUND CRACK ON CARGO DOOR SILL AT FS 589. REPAIRED THE DOOR SILL IAW REO.May 24, 2015 · N920SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201541313Skin · dentedLEFT INBD FLAP LOWER SKIN HAS A DENT INBD SIDE. DAMAGE WAS REMOVED, REPAIR DOUBLER AND FILLER WERE INSTALLED IAW SRM.May 23, 2015 · N920SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201541311Skin · damagedLIGHTNING STRIKE FOUND ON RT ELEVATOR T/E INBD SIDE. REPAIRED THE RT ELEVATOR T/E SKIN IAW REO.May 23, 2015 · N920SW · Cndair CL6002B19 · Elevator, Plate/SkinSDR SWIA201541310Door Frame · dentedPAX DOOR FRAME DENTED AT FS 349, BY THE CAM FITTING. REPAIRED THE DOOR FRAME IAW REO.May 23, 2015 · N920SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA201541316Handle · gougedSERVICE DOOR INNER DOOR HANDLE HAS SEVERAL AREAS THAT CONTAIN CHAFED AND GOUGED. REPAIRED THE SERVICE DOOR INNER HANDLE IAW STS EA.May 22, 2015 · N920SW · Cndair CL6002B19 · Service DoorsSDR SWIA201541308Rib · corrodedLT SPOILERON INBD RIB HAS CORRODED HARDWARE. R & R CORRODED HARDWARE IAW SRM.May 22, 2015 · N920SW · Cndair CL6002B19 · SpoilersSDR SWIA201541307Pcu · corrodedRT FLIGHT SPOILER OTBD PCU HAS CORRODED HARDWARE. REMOVED CORROSION FROM THE RT FLIGHT SPOILER OTBD PCU ATTACH HARDWARE IAW SRM.May 22, 2015 · N920SW · Cndair CL6002B19 · SpoilersSDR SWIA201541306Attach Fitting · corrodedRT SPOILERON OTBD FITTING ATTACH RIB HAS CORRODED HARDWARE. REMOVED CORROSION FROM THE RT SPOILERON OTBD FITTING ATTACH RIB IAW SRM.May 22, 2015 · N920SW · Cndair CL6002B19 · SpoilersSDR SWIA201541305Bolt · corrodedRT SPOILERON PCU'S HAVE CORRODED HARDWARE. REMOVED CORROSION FROM THE RT SPOILERON PCU CONNECTING HARDWARE IAW SRM.May 22, 2015 · N920SW · Cndair CL6002B19 · SpoilersSDR SWIA201541304Fitting · corrodedRT WING T/E FITTING, OTBD OF SPOILERON, HAS CORRODED HARDWARE. REMOVED CORROSION FROM THE CONNECTING HARDWARE ON THE RT WING T/E FITTING OTBD OF THE SPOILERON IAW SRM.May 22, 2015 · N920SW · Cndair CL6002B19 · Wing, Attach FittingsSDR SWIA201541303Attach Fitting · corrodedRT AILERON INBD AND OTBD ATTACH FITTING BOLT RETAINERS HAVE CORRODED HARDWARE. REMOVED CORROSION FROM THE RT AILERON INBD AND OTBD ATTACH FITTING BOLT RETAINERS HARDWARE IAW SRM.May 22, 2015 · N920SW · Cndair CL6002B19 · AileronsSDR SWIA201541309Floor Panel · crackedFLOOR PANEL 222WZ CRACKED. REPAIRED THE FLOOR PANEL IAW EA.May 21, 2015 · N920SW · Cndair CL6002B19 · Fuselage Floor PanelSDR SWIA201440241Wire · chafedLEFT JET OVERHEAT FAIL. REPAIRED CHAFED WIRES TO LT ENGINE LOOP A & LOOP B IAW ESPM. OPS CHECKED FIRE DETECTION SYSTEM - GOOD IAW AMM.Nov 30, 2014 · N920SW · Cndair CL6002B19 · Fire Protection System WiringSDR SWIA201438712Battery Pack · inoperativeF/A FLASHLIGHT INOPERATIVE. INSTALLED NEW BATTERIES.Jul 13, 2014 · N920SW · Cndair CL6002B19 · Emergency EquipmentSDR SWIA201438621Line · failedACFT LOST ALL FLUID IN NR 1 HYDRAULIC SYSTEM. REPLACED HYDRAULIC LINE AND NR 1 EDP IAW AMM.Jul 8, 2014 · N920SW · Cndair CL6002B19 · Hydraulic System, MainSDR SWIA201437260Lamp · burned outNR 2 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. REPLACED LAMP.Apr 24, 2014 · N920SW · Cndair CL6002B19 · Emergency LightingSDR SWIA2014032836852Bulb · burned outEMERGENCY LIGHT EXIT SIGN FORWARD OF GALLEY SERVICE DOOR HAS 1 LIGHT BULB BURNED OUT. REPLACED BULB.Mar 26, 2014 · N920SW · Cndair CL6002B19 · Emergency LightingSDR SWIA201436826Lamp · burned outTWO EMERGENCY EXIT LIGHTS BURNED OUT IN GALLEY, REPLACED LAMPS.Mar 20, 2014 · N920SW · Cndair CL6002B19 · Emergency LightingSDR SWIA201436762Door · bindingTHE GALLEY SERVICE DOOR IS DIFFICULT TO OPEN AND CLOSE. REPLACED THE GALLEY SERVICE DOOR LIFT DEVICE IAW AMM.Mar 17, 2014 · N920SW · Cndair CL6002B19 · Service DoorsSDR SWIA201436227Light · inoperativeONE OF THE LIGHT BULBS ON THE EMERGENCY EXIT SIGN NEXT TO SERVICE DOOR IS BURNED OUT. FLT 6415 RELAMPED.Feb 2, 2014 · N920SW · Cndair CL6002B19 · Emergency LightingSDR SWIA201335535Relay · faultyAC ESS BUS CAUTION MESSAGE ON & EMERGENCY LIGHT ON STATUS MESSAGE. FLT 5549 REPLACED THE AC ESS TRANSFER RELAY K1X10.Dec 9, 2013 · N920SW · Cndair CL6002B19 · AC Power Distribution SystemSDR SWIA201335297Post · crackedCRACK ON FS 409+128 VERTICAL POST OTBD AFT RADIUS AT RBL18.00 WL71.00. C-CHECK REPLACED CRACKED POST AT 409+128 RBL 18 IAW REO.Nov 1, 2013 · N920SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201335296Drag Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED. C-CHECK REPAIRED PAX DOOR AFT DRAG ANGLE IAW REO.Nov 1, 2013 · N920SW · Cndair CL6002B19 · Passenger/Crew Doors
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