N433SW

Service difficulty reports · 140

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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 = 'N433SW'
  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 SWIA202266590None · failedAPU FIREX BOTTLE TEST CAUSES EMERGENCY APU SHUTDOWN WITH CODE 227 ON APU ECU (FILED CLOSED) REMOVED AND REPLACED PBA SWITCH FOR APU FIRE IN REFERENCE TO CRJ200 ESPM 20-24-00. NO FIX. REMOVED AND REPLACED FIRE DETECTION PANEL IN REFERENCE TO CRJ200 AMM 26Oct 4, 2022 · N433SW · Cndair CL6002B19 · Fire Bottle, PortableSDR SWIA202264221None · crackedUPON INSPECTION FOUND RH ENGINE LOWER I/B THRUST REVERSER MAIN TRACK CRACKED. (FILED - CLOSED) REMOVED AND REPLACED RH ENGINE LOWER I/B THRUST REVERSER MAIN TRACK IN REFERENCE WITH CRJ200 AMM 78-34-11. OPS CHECK GOOD AT THIS TIME.Feb 13, 2022 · N433SW · Cndair CL6002B19 · Engine Exhaust SystemSDR SWIA202161788Stringer · damagedSTRINGER 26L REQUIRES REPLACEMENT BETWEEN FRAME FS364.00 AND APPROX. FS341. (FILED CLOSED) REPLACED DAMAGED SECTION OF STR26L FROM FS364.00 TO SPLICE REPAIR BETWEEN FS333.00 - FS 349.00. SPLICE PERFORMED IN REF TO SRM 53-00-03, FIG 202, SHEET 1 (REPAIR FOct 4, 2021 · N433SW · Cndair CL6002B19 · Fuselage Main, KeelSDR SWIA202161784Rail · corrodedSEAT TRACK HAS CORROSION BELOW WINDOW 3AB. (FILED CLOSED) REMOVED AND REPLACED LH SIDEWALL SEAT TRACK FROM FS409.00+18.02 - FS409.00+111.02 IN REF TO REO 601R-53-00-055, REV C, DATED 2017-03-21, REPAIR B USING MCFARLANE P/N 6656 SEAT TRACK IN REF TO REO 6Sep 20, 2021 · N433SW · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202161787None · corrodedFRAME 394, FWD LOWER DOUBLER BETWEEN STR 26L AND 27 HAS CORROSION. (FILED CLOSED) REMOVED AND REPLACED SKIN SUPPORT ON FWD SIDE OF FRAME 394.00 BETWEEN STR25L-STR25R IN REF TO SRM 51-42-06 AND REO 601R-53-21-3502, REV--, DATED 2021-09-28. COMPLIED WITH TSep 17, 2021 · N433SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202161786Bracket · crackedCARGO DOOR AFT COUNTERBALANCE SPRING ATTACHMENT BRACKET IS CRACKED. (FILED CLOSED) REMOVED AND REPLACED CARGO DOOR AFT COUNTERBALANCE SPRING ATTACHMENT BRACKET USING ALTERNATE FASTENERS IN REF TO REO 601R-53-61-7721, REV--, DATED 2021-09-19. COMPLIED WITHSep 17, 2021 · N433SW · Cndair CL6002B19 · DoorsSDR SWIA202161783Rail · corrodedSEAT TRACK HAS CORROSION DIRECTLY BELOW WINDOW 4AB. (FILED CLOSED) REMOVED AND REPLACED LH SIDEWALL SEAT TRACK FROM FS409.00+18.02 - FS409.00+111.02 IN REF TO REO 601R-53-00-055, REV C, DATED 2017-03-21, REPAIR B USING MCFARLANE P/N 6656 SEAT TRACK IN REFSep 17, 2021 · N433SW · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202161785Track · gougedCARGO DOOR AFT ROLLER GUIDE TRACK IS GOUGED NEAR THE UPPER STOP. (FILED CLOSED) REMOVED AND REPLACED CARGO DOOR AFT ROLLER GUIDE TRACK IN REF TO SRM 51-21-06 AND 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED M-337.Sep 15, 2021 · N433SW · Cndair CL6002B19 · DoorsSDR SWIA2019101646469Vane · out of limitsRIGHT INBD FLAP VANE L/E OUTBOARD PANEL IS FOUND TO BE OUT OF LIMITS. (C-CHECK) RO: 10/13/2019 REMOVED AND REPLACED RH INBD FLAP VANE LE OTBD PANEL IAW SRM.Oct 2, 2019 · N433SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2019101646468Vane · damagedRIGHT INBD FLAP VANE L/E CENTER PANEL IS FOUND TO BE OUT OF LIMITS. (C-CHECK) RO: 10/13/2019 REMOVED AND REPLACED RH INBD FLAP VANE LE (CENTER OTBD PANEL) IAW SRM.Oct 2, 2019 · N433SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2019101646467Vane · damagedLEFT INBD FLAP VANE OTBD L/E IS CHAFED OUT OF LIMITS. (CHECK) RO: 10/13/2019 LOCATED, DRILLED, AND INSTALLED REPLACEMENT FLAP OTBD L/E VANE PANEL IAW SRM.Sep 17, 2019 · N433SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2019101646466Vane · damagedLEFT INBD FLAP VANE CNTER L/E IS CHAFED OUT OF LIMITS. (C-CHECK) RO: 10/13/2019 LOCATED, DRILLED, AND INSTALLED REPLACEMENT FLAP CENTER VANE PANEL IAW SRM.Sep 17, 2019 · N433SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2019101646465Floor Support · out of limitsREPLACE RH FLOOR SILL FS 310.00 TO FS 319.70 DUE TO OUT OF LIMITS (C-CHECK) RO: 10/13/2019 R/H FLOOR SILL FS310 TO FS319 REPLACED IAW SRM.Sep 13, 2019 · N433SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019101646483Retainer · gougedAFT CARGO DOOR SEAL RETAINER GOUGED UPPER AFT CORNER MARKED (C-CHECK) RO: 10/13/2019 REMOVED CARGO DOOR (UPPER ,AFT ) SEAL RETAINER, AND INSTALLED NEW CARGO DOOR (UPPER ,AFT) SEAL RETAINER IAW SRM.Sep 11, 2019 · N433SW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR SWIA2019101646470Door Frame · corrodedPAX DOOR CUT OUT FRAME AT STR 16 1/2 L FROM FS 295.0 TO FS 310.0 HAS CORROSION (C-CHECK) RO: 10/13/2019 REMOVED AND REPLACED INTERCOSTAL ON PAX DOOR CUT OUT FRAME AT STGR 16 1/2 L FROM FS295.00 TO FS310.00 IAW SRM.Sep 11, 2019 · N433SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2019101646482Door Sill · corrodedSERVICE DOOR SILL ANGLE HAS CORROSION (C-CHECK) RO: 10/13/2019 SERVICE DOOR SILL ANGLE IS CORRODED AND REPLACED WITH NEW SILL ANGLE IAW SRM.Sep 10, 2019 · N433SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019101646481Door Sill · corrodedRH SILL JUST FWD OF SERVICE DOOR CUTOUT AND BACK TO FS 409.0 HAS CORROSION (C-CHECK) RO: 10/13/2019 BLENDED OUT CORROSION ON RH FLOOR SILL FROM FS 310.00 TO FS 319.70 & FROM FS349.00 TO FS409.00 +5 IAW SRM.Sep 10, 2019 · N433SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019101646480Web · corrodedPAX DOOR AFT WEB CORRODED AT ACCESS PNL CUTOUTS AND STAIR LANDINGS (C-CHECK) RO: 10/13/2019 REMOVED CORROSION ON PAX DOOR AFT WEB STEP LANDINGS IAW SRM. REMOVED AND REPLACED PAX DOOR AFT WEB IAW SRM.Sep 9, 2019 · N433SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2019101646479Web · corrodedPAX DOOR FWD WEB CORRODED AT STEP LANDINGS AND ACCESS PNL CUTOUTS (C-CHECK) RO: 10/13/2019 REMOVED CORROSION ON PAX DOOR FWD WEB STEP LANDINGS IAW SRM. REMOVED REPLACED PAX DOOR FWD WEB IAW SRM.Sep 9, 2019 · N433SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2019101646478Vane · chafedRIGHT INBD FLAP VANE L/E HAS THREE CHAFFS ( OUTBD, MIDDLE, INBD). (C-CHECK) RO: 10/13/2019 BLENDED RIGHT INBD FLAP VANE L/E IN THREE SPOTS ( OUTBD, MIDDLE, INBD). RIGHT INBD FLAP VANE L/E CENTER PANEL IS FOUND TO BE OUT OF LIMITS AND REPLACED. RIGHT INBD FLAP Sep 4, 2019 · N433SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2019101646477Vane · chafedLEFT INBD FLAP VANE L/E HAS THREE CHAFFS ( OUTBD, MIDDLE, INBD). (C-CHECK) RO: 10/13/2019 BLENDED OUTAND REPAIRED CHAFFING MARKS ON THE LEFT HAND I/B FLAP VANE L/E AT THE 3EA. LOCATION I/B, O/B AND MIDDLE. REPLACED LEFT INBD FLAP (CENTER ) VANE L/E PANEL, AND Sep 4, 2019 · N433SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2019101646476Panel · corrodedPAX DOOR PANEL 832AT HAS CORROSION AROUND FASTENER HOLES AND CHAFING DAMAGE ALONG LOWER FASTENER HOLES. (C-CHECK) RO: 10/13/2019 REMOVED CORROSION & CHAFING DAMAGES ON PANEL 832AT AROUND SCREW HOLES IAW SRM.Sep 4, 2019 · N433SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2019101646475Panel · corrodedPAX DOOR PANEL 832BR HAS CORROSION AROUND FASTENER HOLES. (C-CHECK) RO: 10/13/2019 REMOVED AND REPLACED CORROSION ON PASSENGER DOOR PANEL 832BR IAW SRM.Sep 4, 2019 · N433SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2019101646474Panel · corrodedPAX DOOR PANEL 832CR HAS CORROSION AROUND FASTENER HOLES. (C-CHECK) RO: 10/13/2019 REMOVED CORROSION ON PASSENGER DOOR PANEL 832CR IAW SRM.Sep 4, 2019 · N433SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2019101646473Panel · corrodedPAX DOOR PANEL 832EL HAS CORROSION AROUND FASTENER HOLES. (C-CHECK) RO: 10/13/2019 REMOVED CORROSION ON PASSENGER DOOR PANEL 832EL IAW SRM.Sep 4, 2019 · N433SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2019101646472Panel · corrodedPAX DOOR PANEL 832ER HAS CORROSION AROUND FASTENER HOLES. (C-CHECK) RO: 10/13/2019 REMOVED CORROSION ON PASSENGER DOOR PANEL 832ER IAW SRM.Sep 4, 2019 · N433SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2019101646471Panel · corrodedPAX DOOR PANEL 832GR HAS CORROSION AROUND FASTENER HOLES. (C-CHECK) RO: 10/13/2019 REMOVED CORROSION ON PASSENGER DOOR PANEL 832GR, FOUND TO BE OUT OF LIMITS IAW SRM.Sep 4, 2019 · N433SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2019082746230Proximity Sensor · failedCREW REPORTS "GEAR DISAGREE" AFTER TAKEOFF. CREW REPORTED NOSE GEAR WOULD NOT RETRACT AFTER ROTATION. RETURNED TO FIELD. REMOVED AND REPLACED THE NLG STRUT-CENTERED PROXIMITY SENSOR HARNESS ASSY IAW AMM. PERFORMED OPS CHECK OF EXTENSION AND RETRACTION SYSTEM IAug 26, 2019 · N433SW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA2019022145534Selector Valve · leakingGEAR DISAGREE ON TAKEOFF WHEN TRYING TO RETRACT THE GEAR. BOTH MAINS RETRACTED FULLY BUT THE NOSE GEAR STAYED DOWN. COMPLIED WITH QRH AND ALL GEAR INDICATED DOWN AND 3 GREEN. RETURNED TO FIELD. (FLT#4105) REMOVED AND REPLACED NLG SELECTOR VALVE IAW AMM. HYD SYFeb 21, 2019 · N433SW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA2019021945528Selector Valve · failedFLT#3703, UPON GEAR RETRACTION, NOSE GEAR DID NOT SHOW AN UP INDICATION. GEAR DISAGREE WARNING MESSAGE APPEARED.FOLLOWED QRH PROCEDURE AND GEAR EXTENDED TO DOWN POSITION CORRECTLY. NO GEAR SPEED LIMITS WERE EXCEEDED. INSTALLED NLG SELECTOR VALVE IAW AMM. BLEDFeb 18, 2019 · N433SW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA2019011545442Bracket · bentGEAR DISAGREE ON T/O. NOSE WHEEL DID NOT RETRACT. FOLLOWED QRH. RTF. (FLT#4106) CLOSED REMOVED AND REPLACED NLG OLEO BRACKET AND ADJUSTED PROXIMITY SENSOR. PERFORMED OPS CHECK IAW AMM. OPS CHECK GOOD, SWUNG GEAR MULTIPLE TIMES.Jan 11, 2019 · N433SW · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/AxleSDR SWIA2018111645188Uplock · failedAS WE PUT DOWN THE LANDING GEAR, WE WOULD GET A MOMENTARY GEAR DISAGREE CAUTION MESSAGE. (FLT# 7413) FO: 10/29/2018. CLOSED REMOVED AND REPLACED LEFT MLG UPLOCK ASSY IAW AMM. LEAK AND OPS CHECKS GOOD.Oct 25, 2018 · N433SW · Cndair CL6002B19 · Landing Gear Position and WarningSDR SWIA2017091943771Unknown · crackedFOUR HOLES WITH DEFECTS. ALL HOLES COLD WORKED AND REPAIRED IAW REO.Aug 29, 2017 · N433SW · Cndair CL6002B19 · Wing StructureSDR SWIA2017091943770Unknown · crackedFOUR HOLES WITH DEFECTS. ALL HOLES COLD WORKED AND REPAIRED IAW REO.Aug 29, 2017 · N433SW · Cndair CL6002B19 · Wing StructureSDR SWIA2017091943775Floor Support · corrodedCARGO FLOOR SUPPORT JUST INSIDE CARGO DOOR HAS CORROSION AROUND NUTPLATE HOLES. INSTALLED NEW CARGO FLOOR SUPPORT IAW REO.Aug 28, 2017 · N433SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201743774Skin · dentedRT WING LEADING EDGE WING STATION 166. HAD A SMALL DENT .009 INCH DEEP X 3/4 INCH WIDE AND 1/2 INCH LONG. HAND DRESSED THE SKIN BACK TO ORIGINAL CONTOUR IAW REO.CHECKED GOOD.Aug 25, 2017 · N433SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2017091943773Structure · dentedLEFT WING LEADING EDGE LWS 185. HAD A SMALL DENT THAT MEASURES .019 INCH IN DEPTH, X .75 INCH IN LENGTH, AND .5 INCH IN WIDTH. COMPLIED WITH DRESS BACK REPAIR TO DENT ON THE LH WING LEADING EDGE IAW REO. LEAK CHECKED GOOD.Aug 25, 2017 · N433SW · Cndair CL6002B19 · Wing StructureSDR SWIA201743772Structure · dentedWING STATION 139. HAS A DENT 3/4 INCH WIDE AND .010 INCH DEEP. HAND FORMED THE DENT BACK TO ORIGINAL CONTOUR IAW REO. CHECKED GOOD..Aug 25, 2017 · N433SW · Cndair CL6002B19 · Wing StructureSDR SWIA201743085Priority Valve · failedPILOT REPORTED NOSE GEAR WOULD NOT RETRACT WITH GEAR DISAGREE. REPLACED THE NOSE LANDING GEAR PRIORITY VALVE. SWUNG GEAR, OPS CHECKED GOOD.Mar 1, 2017 · N433SW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA201541642Strut · overservicedNOSE GEAR FAILED TO RETRACT. RETURNED TO FIELD. FOUND NOSE STRUT OVER SERVICED CORRECTED, OPS CHECKS GOOD, GEAR SWING ACCOMPLISHED.Nov 25, 2015 · N433SW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA201439964Bracket · bentON DEPARTURE, NOSE GEAR FAILED TO RETRACT. RETURNED TO FIELD. MAIN GEAR EXTENDED NORMALLY. DUE TO IMPROPER PLACEMENT OF TOW STRAP, R & R BENT AND MISALIGNED NLG CENTERED PROX SENSOR BRACKET IAW AMM, PN: 16215-105.Nov 16, 2014 · N433SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201438417Lamp · inoperativeLEFT MIDDLE OVERWING EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP.Jun 26, 2014 · N433SW · Cndair CL6002B19 · Emergency LightingSDR SWIA201437681Light · burned outEXTERIOR EMERGENCY LIGHT NR 7 IS BURNED OUT. R & R EXTERIOR EMERGENCY LIGHT IAW AMM.May 21, 2014 · N433SW · Cndair CL6002B19 · Emergency LightingSDR SWIA201437133Actuator · failedYAW DAMPER NR 2 KEEPS DISCONNECTING AND WHEN ENGAGED CAUSES UNCOMMANDED RUDDER MOVEMENT. R & R YAW DAMPER NR 2 LINEAR ACTUATOR IAW AMM, PN ON/OFF: 622-9968-001, SN ON: 2497, SN OFF: 2561.Apr 14, 2014 · N433SW · Cndair CL6002B19 · Autopilot SystemSDR SWIA201436645Light · inoperativeEMERGENCY LIGHT NEXT TO MAIN CABIN DOOR IS BURNED OUT. FLT 4699 RELAMPED.Mar 6, 2014 · N433SW · Cndair CL6002B19 · Emergency LightingSDR SWIA201436082Computer · faultyAIRCRAFT INITIATED A SEVERE CLIMB TO CAPTURE GLIDE SLOPE, DISCONNECTED THE AUTO PILOT, GOT THE AIRCRAFT STABLE & RESUMED THE APPROACH. WHEN THE AUTO PILOT WAS RECONNECTED, AT APPROXIMATELY 3500 ', THE FLIGHT DIRECTOR COMMANDED A 15 DEGREE NOSE DOWN PITCH. DIJan 21, 2014 · N433SW · Cndair CL6002B19 · Autopilot ComputerSDR SWIA201335354Floor Support · corrodedCABIN FLOOR SUPPORT BEAM FS 349.00 AT PAX DOOR HAS CORROSION ON UNDERSIDE & CORRODED FASTENERS. C-CHECK REPAIRED CABIN FLOOR SUPPORT BEAM AT FS 349 LBL 40.00 IAW STS EA.Nov 10, 2013 · N433SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201335355Stiffener · chafedINTERNAL LT SIDE OF CTR WING FUEL TANK, FUEL PANEL 510BB. FUEL TUBE ASSEMBLY IN FWD PORTION OF TANK, CHECK VLV IS CHAFING ON THE STIFFENER. C-CHECK BLENDED CHAFED AREA ON STRINGER 23 JUST OTBD OF WS 29.4 IAW SRM.Nov 8, 2013 · N433SW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR SWIA201335357Angle · crackedAFT PRESSURE BULKHEAD, AFT SIDE, FRAME JUST AFT OF BULKHEAD HAS 2 EA CRACKED "L" ANGLES, 1 AT LT SIDE, 1 AT RT SIDE. C-CHECK R & R 2 EA "L" ANGLES AT FS 625 STRINGER 14 IAW SRM & REO.Nov 7, 2013 · N433SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201335356Skin · chafedRT AILERON UPPER LE SKIN IS CHAFED. C-CHECK REPLACED RT AILERON UPPER LE SKIN PN 601R13031-166 IAW SRM.Nov 7, 2013 · N433SW · Cndair CL6002B19 · Ailerons
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