N961SW

Service difficulty reports · 174

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 = 'N961SW' 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 SWIA202266167None · dentedLH OB FLAP LOWER SKIN IS DENTED AT FLS268 10IN FWD OF TE. (C-CHECK RO 7/26/2022) LH OB FLAP LOWER SKIN DENT AT FLS268 10IN FWD OF TE WAS FOUND OUT OF LIMITS IAW CRJ 200 SRM 57-53-00. COMPLIED WITH CRJ 200 SRM 57-53-00 REPAIR NO.3 REV.38 B DATED 25 NOV 2Jun 9, 2022 · N961SW · Cndair CL6002B19 · Aileron TabsSDR SWIA202266166None · failedFOUND FS409+128 VERTICAL POSTS BL0.0 LEFT HAND SIDE WL 69.0 HAS INDICATION NOTED .400 LONG 80%FSH AT AFT FLANGE RADIUS FAILED NDT INSPECTION (C-CHECK RO 7/26/2022) COMPLIED WITH REO 601R-53-41-889. COMPLETED SKYCARD 51-900-1003-SKY AND COMPLETED M-337 Jun 6, 2022 · N961SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202266165None · crackedPAX DOOR AFT FORMER IS CRACKED JUST BELOW THE POWER ASSIST MOTOR PULLEY (C-CHECK RO 7/26/2022) REMOVED AND REPLACED PAX DOOR AFT FORMER IAW CRJ 200 SRM 51-42-06 AND 51-42-21 REV. 38B DATED 25 NOV 2020. MAJOR REPAIR TASK CARD 51-900-1003-SKY AND FORM M-3Jun 5, 2022 · N961SW · Cndair CL6002B19 · DoorsSDR SWIA202266164None · damagedTHE ADF ANTENNA HAS ONE NUTPLATE SPINNING WITH THE SCREW STILL INSTALLED AND REQUIRES REPLACEMENT.THE LH MIDDLE NUTPLATE. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED 1EA NUTPLATE ON HAT CHANNEL AND RE-INSTALLED HAT CHANEEL IAW CRJ 200 SRM 51-42-06. MAJOJun 4, 2022 · N961SW · Cndair CL6002B19 · Omega Navigation SystemSDR SWIA202266163None · dentedWHILE REMOVING STABILIZER VERTICAL LEADING EDGE FOUND PROTRUDING DENT APROX 12" ABOVE T/E OF THE L/H PYLON (C-CHECK RO 7/26/2022) REPAIRED DENT IAW REO 601R-53-61-7844 REV. - - DATED 6/15/22. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED. FORM 3Jun 3, 2022 · N961SW · Cndair CL6002B19 · Ventral StructureSDR SWIA202266162None · chafedR/H INBOARD FLAP, FLAP VANE IS CHAFED AT (3) LOCATIONS ALONG THE LEADING EDGE FROM CONTACT WITH FLAP VANE STOPS. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED R/H INBOARD FLAP VANE MID. LEADING EDGE CAP I.A.W. BOMBARDIER CRJ200 SRM 51-42-13 REV.38B, DATEMay 31, 2022 · N961SW · Cndair CL6002B19 · AileronsSDR SWIA202266161None · crackedL/H FORWARD FUSELAGE SKIN IS CRACKED AT THE L/H TRU DOOR AFT LATCH CUTOUT IN THE FORWARD LOWER RADIUS OF THE LATCH CUTOUT. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED L/H FWD FUSE SKIN IAW SRM 51-42-13, 51-42-06 AND REO 601R-53-11-3775 REV-- DATED:2022-May 31, 2022 · N961SW · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202266160None · dentedPAX DOOR HAS DENT ON OUTER SKIN ( MARKED) (C-CHECK RO 7/26/2022) REPAIRED PAX DOOR OUTER SKIN DENT IAW MHIRJ REO 601R-52-11-2925 REV. -- DATED 2022-06-14. MAJOR REPAIR TASK CARD 51-900-1003-SKY AND FORM M-337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE NOTMay 29, 2022 · N961SW · Cndair CL6002B19 · DoorsSDR SWIA2019111846765Proximity Sensor · out of adjustATTEMPTED TO RETRACT GEAR ON DEPARTURE, GEAR DISAGREE WARNING WITH NOSE DOOR OPEN WARNING FLIGHT 5493 CLOSEDTHIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 19896892 WITH THE FOLLOWING CORRECTIVE ACTION: "PERFORMED ADJUSTMENT OF THE NOSE LANDING GEAR CENTERED/ENov 14, 2019 · N961SW · Cndair CL6002B19 · Landing Gear Position and WarningSDR SWIA2019071246035Actuator · failedRECEIVED €ŒGEAR DISAGREE€? ON THE RIGHT MAIN ON TAKEOFF. MESSAGE CLEARED BEFORE QRH COMPLETED. (FLT#5803) FO: 07/05/2019 CLOSED REMOVED AND REPLACED RT MLG SIDE STAY ACTUATOR IAW AMM.Jul 5, 2019 · N961SW · Cndair CL6002B19 · Landing Gear ActuatorSDR SWIA2019051045870Strut · lowGEAR DISAGREE WARNING MESSAGE AFTER TAKEOFF WITH THE NOSE GEAR REMAINING DOWN AND LOCKED. BOTH MAIN GEAR INDICATED €ŒUP€?. HAD ASSOCIATED €ŒNOSE DOOR OPEN€? WARNING MESSAGE AS WELL AS TWO CAUTION MESSAGES, €ŒSTEERING INOP€? AND €ŒWOW INPUT.€? RAN QRMay 10, 2019 · N961SW · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/AxleSDR SWIA2019050845868Doubler · corrodedDRAIN MAST INTERNAL DOUBLER AT FS 605 HAS CORROSION. (C-CHECK) RO: 05/07/2019 REMOVED AND REPLACED DRAIN MAST INTERNAL DOUBLER P/N 301R43216-11 AT FS 605 IAW SRM. LEAK AND OPS CHECKS SATISFACTORY IAW AMM.Apr 12, 2019 · N961SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2019050845863Hinge · damagedPAX DOOR HINGE ( FUSELAGE SIDE) DAMAGED. (C-CHECK) RO: 05/07/2019 REMOVED AND REPLACED PAX DOOR HINGE ( FUSELAGE SIDE) IAW SRM. LEAK CHECK SATISFACTORY.Apr 6, 2019 · N961SW · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA2019050845850Trunnion · damagedFOUND 2EA OVERSIZE FASTENERS IN LT TRUNNION IN HOLES 14, 19. (C-CHECK) RO: 05/07/2019 REAMED OVERSIZE HOLES IN LT TRUNNION LOWER PLANK AND INSTALLED NEW FASTENERS IAW REO.Apr 5, 2019 · N961SW · Cndair CL6002B19 · Wing, Landing Gear Attach FittingsSDR SWIA2019050845867Door Sill · corrodedSERVICE DOOR SILL ANGLE PN 601R38303-225 HAS SPOTS OF CORROSION. (C-CHECK) RO: 05/07/2019 REMOVED AND REPLACED NEW SILL ANGLE IAW SRM.Apr 3, 2019 · N961SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019050845865Door Sill · corrodedSEVERAL AREAS OF CORROSION ON LT PRESSURE FLOOR SILL SKIN. (C-CHECK) RO: 05/07/2019 REMOVED CORROSION IN 12 AREAS ON LT PRESSURE FLOOR SILL PANEL BETWEEN FS 409+128 AND FS559, IAW REO ALL CHECKS OKAY.Apr 3, 2019 · N961SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019050845849Door Sill · corrodedSEVERAL AREAS OF CORROSION ON RT PRESSURE FLOOR SILL SKIN. (C-CHECK) RO: 05/07/2019 BLENDED OUT CORROSION ON RT PRESSURE FLOOR SILL PANEL FROM FS 409+128 TO FS 559 AT VARIOUS LOCATIONS IAW REO.Apr 3, 2019 · N961SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019050845866Frame · corrodedFRAME FS605 CORRODED STR26L €“ STR26R. (C-CHECK) RO: 05/07/2019 REMOVED AND REPLACED FRAME AT FS605 STR26L - STR26R IAW SRM. LEAK CHECK GOOD.Apr 2, 2019 · N961SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2019050845862Floorbeam · corrodedFLOORBEAM FS409+10 €“ FS409+40 RBL9 CORRODED AT FASTENER HOLE LOCATIONS. (C-CHECK) RO: 05/07/2019 REMOVED AND REPLACED FLOORBEAM CAP AT FS409.00+5 - FS409.00+42 IAW SRM AND REO.Apr 2, 2019 · N961SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2019050845860Floor Support · corrodedFLOOR SUPPORT ANGLE CORRODED FS621 LBL9 €“ LBL27. (C-CHECK) RO: 05/07/2019 REMOVED CORROSION FROM FLOOR SUPPORT ANGLE FS621 LBL9-LBL27 COMPLIED WITH AL STEPS OF REO.Apr 2, 2019 · N961SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019050845864Floorbeam · corrodedFLOORBEAM CORRODED AROUND NUT PLATE LOCATIONS FS610 €“ FS620 LBL27. (C-CHECK) RO: 05/07/2019 COMPLIED WITH PERMANENT REPAIR FLOORBEAM CORROSION AROUND NUT PLATE LOCATIONS FS610 €“ FS620 LBL27 IAW REO.Apr 1, 2019 · N961SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2019050845861Floorbeam · corrodedFLOORBEAM CORRODED AROUND NUT PLATE LOCATIONS FS569 €“ FS610 LBL27. (C-CHECK) RO: 05/07/2019 REPLACED FLOORBEAM FS569 - FS610 LBL27 WITH NEW P/N 601R35031-263 IAW REO.Apr 1, 2019 · N961SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2019050845857Skin · chafedRIGHT HAND SIDE AFT EXTERIOR SKIN HAS CHAFING AND CORROSION WHERE APU EXHAUST SHEILD ATTACHES TO AIRCRAFT. (C-CHECK) RO: 05/07/2019 BLENDED CHAFING AND CORROSION WHERE APU EXHAUST SHEILD ATTACHES TO AIRCRAFT IAW SRM AND REO.Apr 1, 2019 · N961SW · Cndair CL6002B19 · Empennage StructureSDR SWIA2019050845856Door Sill · corrodedCARGO DOOR SILL CORRODED FS562 €“ FS621 LBL43. (C-CHECK) RO: 05/07/2019 REMOVED AND REPLACED CARGO DOOR SILL FROM FS589.00 - 621.00 IAW SRM.Apr 1, 2019 · N961SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019050845854Floorbeam · corrodedFLOORBEAM CORRODED AROUND NUT PLATE LOCATIONS FS561 €“ FS569 LBL27. (C-CHECK) RO: 05/07/2019 REMOVED AND REPLACED NEW FLOORBEAM LBL 27 FROM FS 574 TO FS 559+24 IAW REO.Apr 1, 2019 · N961SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2019050845859Fairing · damagedFAIRING 326CL IS CHAFED/GOUGED WHERE IT INTERFACES WITH THE VISOR PANEL. (C-CHECK) RO: 05/07/2019 REMOVED DAMAGE ON PANEL 326CL AND COMPLIED WITH ALL STEPS OF REO.Mar 29, 2019 · N961SW · Cndair CL6002B19 · Empennage StructureSDR SWIA2019050845855Door · chafedLT MLG DOOR FORWARD SIDE HAS CHAFING 2 LOCATIONS. (C-CHECK) RO: 05/07/2019 BLENDED LT MLG DOOR FWD SIDE CHAFES 2 LOCATIONS IAW SRM.Mar 21, 2019 · N961SW · Cndair CL6002B19 · Landing Gear DoorsSDR SWIA201945853Pan · corrodedSERVICE DOOR AFT PAN HAS CORROSION AT LOWER CORNER. (C-CHECK) RO: 05/07/2019 BLENDED SERVICE DOOR AFT PAN AT LOWER CORNER IAW SRM AND REO.Mar 21, 2019 · N961SW · Cndair CL6002B19 · Service DoorsSDR SWIA2019050845852Structure · gougedSERVICE DOOR OUTER HANDLE CUT-OUT HAS SEVERAL GOUGES. (C-CHECK) RO: 05/07/2019 BLENDED OUT DAMAGE AREAS 5 EA ON SERVICE DOOR OUTER HANDLE CUT OUT, COMPLIED WITH ALL STEPS OF REO.Mar 21, 2019 · N961SW · Cndair CL6002B19 · Service DoorsSDR SWIA2019050845858Panel · dentedDENTS ON RT WING MIDDLE LEADING EDGE (C-CHECK) RO: 05/07/2019 REPLACED RT WING CENTER LEADING EDGE WITH NEW LEADING EDGE PANEL P/N 601R12044-8S IAW SRM.Mar 20, 2019 · N961SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2019050845851Access Door · dentedSEVERAL DENTS FOUND BELOW GROUND AIR CONNECTION DOOR AT APPROXIMATELY FS559 TO FS579. (C-CHECK) RO: 05/07/2019 COMPLIED WITH PERMANENT REPAIR GRD AIR DOOR DENTS, IAW REO, ALL CHECKS OKAY.Mar 20, 2019 · N961SW · Cndair CL6002B19 · Service DoorsSDR SWIA201743191Skin · dentedFWD FUSELAGE BELLY AT FS 250.0 HAS A DENT. C-CHECK, ALL STEPS COMPLETED FOR PERMANENT REPAIR TO DENT LOCATED AT FS 250 IAW REO.Mar 30, 2017 · N961SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201743190Skin · chafedRIGHT INBOARD FLAP VANE L/E SKIN IS CHAFED AT CENTER SECTION. C-CHECK, REMOVED AND REPLACED RT INBD FLAP CENTER FLAP VANE LEADING EDGE CAP IAW SRM.Mar 21, 2017 · N961SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201743189Skin · chafedRIGHT INBOARD FLAP VANE L/E SKIN IS CHAFED AT LEFT SECTION. C-CHECK, REMOVED AND REPLACED THE RIGHT INBOARD FLAP VANE L/E SKIN IAW SRM.Mar 21, 2017 · N961SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201743188Skin · chafedLEFT INBOARD FLAP VANE SKIN L/E, RT SECTION IS CHAFED. C-CHECK, REMOVED AND REPLACED LEFT INBD FLAP VANE L/E RT SECTION IAW SRM.Mar 21, 2017 · N961SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201743187Flap · chafedLEFT INBOARD FLAP CENTER SECTION OF L/E IS CHAFED. C-CHECK, REMOVED AND REPLACED LEFT INBD FLAP CENTER L/E SECTION IAW SRM.Mar 21, 2017 · N961SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201743186Skin · chafedLEFT INBOARD VANE SKIN INBOARD L/E SECTION CHAFED. REMOVED AND REPLACED LEFT INBD VANE SKIN INBD L/E SECTION IAW SRM.Mar 21, 2017 · N961SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201641864Seal · leakingWHILE CLIMBING, ACFT WAS PRESSURIZING NORMAL AND AT 32,000 FT CREW REPORTED VERY LOUD NOISE COMING FROM SERVICE DOOR. THEN CABIN PRESSURE STARTED TO CLIMB UNTIL IT REACH 8000. CREW STARTED TO DESCEND AND CABIN ALT KEPT CLIMBING UNTIL REACHED 11,000 FT THEN CRFeb 5, 2016 · N961SW · Cndair CL6002B19 · Service DoorsSDR SWIA201541552Control Handle · failedAFTER TAKEOFF, CREW RECEIVED A GEAR DISAGREE, NOSE GEAR DID NOT RETRACT, C/W QRH, RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. R & R LANDING GEAR CONTROL HANDLE ASSY IAW AMM. C/W GEAR EXTENSION, RETRACT CYCLES AND EMERGENCY EXTENSION IAW AMM OPS CHECK Nov 10, 2015 · N961SW · Cndair CL6002B19 · Landing Gear SelectorSDR SWIA201541430Proximity Sensor · failedAFTER TAKEOFF, THE CREW RECEIVED A NOSE WHEEL STEERING INOPERATIVE INDICATION, FOLLOWED BY A GEAR DISAGREE. NOSE GEAR DID NOT RETRACT. NO EMERGENCY DECLARED. VERIFIED NOSE WHEEL STEERING OPS WITH GEAR DOWN. R & R WOW 1 PROXIMITY SENSOR ON NOSE GEAR IAW ASep 8, 2015 · N961SW · Cndair CL6002B19 · Landing Gear Position and WarningSDR SWIA201540933Skin · damagedLEFT SIDE EXTERNAL FUSELAGE SKIN HAS A CREASE AT BS 605 BETWEEN STR 21 - 22L. REPAIRED IAW EA.Mar 16, 2015 · N961SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201540935Vane · chafedRIGHT INBD FLAP, OTBD VANE CAP HAS A CHAFE. BLENDED CHAFE ON INBD FLAP VANE CAP, FOUND TO BE BEYOND LIMITS OF REO. R & R VANE CAP ON RT INBD FLAP, OTBD END. RESTORED FINISH AND IDENTIFIED VANE CAP IAW EA.Mar 15, 2015 · N961SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201540937Skin · chafedRIGHT AILERON CHAFED ALONG UPPER L/E. RT AILERON UPPER L/E SKIN REPAIRED IAW REO.Mar 12, 2015 · N961SW · Cndair CL6002B19 · AileronsSDR SWIA201540929Skin · corrodedEXTERNAL FUSELAGE SKIN HAS CORROSION AT 2 EA FAIRING MOUNT HOLES, AT BS 559+33, BETWEEN STRINGERS 22 - 23R. SKIN REPAIRED IAW EA.Mar 12, 2015 · N961SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201540932Skin · dentedDENT AFT OF BS 589 BELOW STRINGER 21 MEASURES 1.5 X 1.5 X .06 DEEP. REPAIRED DENT IAW EA.Mar 11, 2015 · N961SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201439566Warning Message · false activationDURING DESCENT AT 24,000 FT, RECEIVED LT FUEL LOW PRESSURE MESSAGE, NO SECONDARY INDICATIONS, FUEL WAS 310 PPH, OCCURED WHEN THROTTLE WAS BROUGHT BACK TO FLIGHT IDLE. PERFORMED OPS CHECK OF FUEL LOW PRESSURE SWITCH IAW AMM, AND RAN ENGINES WITH CREW AS REQUIROct 19, 2014 · N961SW · Cndair CL6002B19 · Engine Fuel Indicating SystemSDR SWIA201438818Amplifier · fluctuatesRETURNED TO DEPARTURE DUE TO RT ENGINE N1, N2, OIL PRESSURE, AND FUEL FLUCTUATIONS. REPLACED AMPLIFIER. OPS CHECKED GOOD.Jul 19, 2014 · N961SW · Cndair CL6002B19 · Engine Indicating SystemSDR SWIA201437851Engine · overtempREJECTED TAKEOFF DUE TO ITT EXCEEDENCE ON LT ENGINE DURING T/O ROLL. COMPLIED WITH OVER TEMP INSPECTION IAW CARD.May 24, 2014 · N961SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA201437565Lamp · inoperativeEMERGENCY EXIT SIGN, LOWER, NEXT TO GALLEY SERVICE DOOR, LAMPS INOPERATIVE, REPLACED LAMPS.May 13, 2014 · N961SW · Cndair CL6002B19 · Emergency LightingSDR SWIA201437245Controller · faultyRECEIVED CABIN AFT CAUTION. AUTO 1 AND AUTO 2 WOULD NOT CONTROL CABIN. MANUAL MODE WOULD CONTROL CABIN. PERFORMED OPS TEST OF THE PRESSURIZATION CONTROLS IAW AMM. OPS CHECKED GOOD AT THIS TIME.Apr 21, 2014 · N961SW · Cndair CL6002B19 · Cabin Pressure Control System
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