N423SW, cancelled Mar 6, 2023

Service difficulty reports · 130

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 = 'N423SW' AND deregistration_id = 'N423SW-2023-03-06'
  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 SWIA2020061847643Fitting · damagedPER CUSTOMER REQUEST, REMOVE HORIZONTAL STAB STATIONARY FITTING HARDWARE TO VERIFY HOLE DIAMETER. (C-CHECK) RO 7/27/2018 VERIFIED HOLES DIAMETER ON HORIZONTAL STAB STATIONARY FITTING AND REAMED AND UP SIZE HOLES AND INSTALLED NEW HARDWARE PER REO AND COMPLIEDJul 3, 2018 · N423SW · Cndair CL6002B19 · Horizontal Stabilizer Miscellaneous StructureSDR SWIA2018073144929Vane · chafedLT INBOARD FLAP - FLAP VANE CHAFED AT 2 LOCATIONS ON TOP TRAILING EDGE (CHAFES LOCATED AT 49" AND 54" FROM INBOARD SIDE OF VANE). (C-CHECK) RO: 07/28/2018 BLENDED OUT DAMAGE IAW REO AND SRM.Jun 22, 2018 · N423SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2018073144928Coaming · chafedCARGO DOOR COAMING IS CHAFED AT LOWER FWD END. (C-CHECK) RO: 07/28/2018 INSTALLED 2 EA CARGO DOOR COAMING IAW SRM AND REO. OPS TEST AND LEAK CHECK GOOD AT THIS TIME. NO DEFECTS NOTED.Jun 16, 2018 · N423SW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR SWIA2018073144921Hinge · damagedREPLACE PAX DOOR HINGE FUSELAGE SIDE DUE TO OUT OF LIMITS ELONGATED HOLES. (C-CHECK) RO: 07/28/2018 INSTALLED NEW/SERVICEABLE PASSENGER DOOR HINGE FUSELAGE SIDE IAW REO. LEAK CHECK GOOD AT THIS TIME.Jun 14, 2018 · N423SW · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA2018073144927Frame · corrodedFS 605.00 FRAME HAS 2 AREAS OF CORROSION ON FWD SIDE OF FRAME BETWEEN STR 27 AND 23L. (C-CHECK) RO: 07/28/2018 REMOVED AND INSTALLED A NEW FS 605.00 FRAME BETWEEN STRINGER 27 AND STRINGER 23L IAW REO. COMPLIED WITH PRESSURIZATION LEAK CHECK, GOOD.Jun 12, 2018 · N423SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2018073144926Aileron · chafedRT AILERON ALONG LOWER LEADING EDGE IS CHAFED. (C-CHECK) RO: 07/28/2018 REMOVED DAMAGE ON RT AILERON ALONG LOWER LEADING EDGE IAW REO.Jun 9, 2018 · N423SW · Cndair CL6002B19 · AileronsSDR SWIA2018073144925Aileron · chafedRT AILERON ALONG UPPER LEADING EDGE IS CHAFED. (C-CHECK) RO: 07/28/2018 REMOVED AND REPLACED R/H AILERON UPPER LEADING EDGE IAW REO.Jun 9, 2018 · N423SW · Cndair CL6002B19 · AileronsSDR SWIA2018073144924Vane · chafedRIGHT WING INBOARD FLAP VANE LEADING EDGE CHAFED INBOARD OF THE INBOARD SLIDING VANE ACTUATOR ATTACHMENT. (C-CHECK) RO: 07/28/2018. REPLACED RT INBD FLAP VANE CAP IAW SRM.Jun 9, 2018 · N423SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2018073144923Vane · chafedLEFT WING INBOARD FLAP VANE LEADING EDGE CHAFED OUTBOARD OF THE OUTBOARD SLIDING VANE ACTUATOR ATTACHMENT. (C-CHECK) RO: 07/28/2018 REMOVED CHAFE DAMAGE IAW REO AND SRM.Jun 9, 2018 · N423SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2018073144922Vane · chafedLEFT WING INBOARD FLAP VANE LEADING EDGE CHAFED OUTBOARD OF THE MIDDLE SLIDING VANE ACTUATOR ATTACHMENT. (C-CHECK) RO: 07/28/2018 REMOVED CHAFE DAMAGE IAW REO AND SRM.Jun 9, 2018 · N423SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2017101743746Warning Message · false activationGEAR DISAGREE. WOW INPUT CAUTION MESSAGE, STEERING INOPERATIVE, WOW OUTPUT FAIL STATUS MESSAGES POSTED. MESSAGES CLEARED AND OPS CHECKED GOOD.Sep 11, 2017 · N423SW · Cndair CL6002B19 · Landing Gear Position and WarningSDR SWIA201642287Strut · chafedLEFT MLG DOOR LOWER CONTROL ARM CHAFED AT INBD END. REMOVED AND INSTALLED NEW SERVICEABLE LT MLG DOOR STRUT, IAW AMM. OPS CKS GOOD.Jun 13, 2016 · N423SW · Cndair CL6002B19 · Landing Gear Door Retract SectionSDR SWIA201642286Panel · corrodedPANEL 832CR HAS CORROSION AROUND THE FASTENER HOLES. R & R WITH NEW PANEL 832CR, PN: 600-31902-295 IAW SRM.Jun 11, 2016 · N423SW · Cndair CL6002B19 · DoorsSDR SWIA201642285Panel · corrodedPANEL 832CL HAS CORROSION AROUND THE FASTENER HOLES. R & R PANEL 832CL, PN: 600-31902-295 IAW SRM.Jun 11, 2016 · N423SW · Cndair CL6002B19 · DoorsSDR SWIA201642096A/C Pack · leakingLEFT 14TH DUCT WARNING WITH SYS OFF, RED FLOW BAR ON LT COWL/PYLON. FOLLOWED QRH AND MSG DID NOT EXTINGUISH. DIVERTED, DECLARED EMERGENCY. HOT AIR LEAK COMING FROM FWD OF THE LT PACK. THE HOT AIR IS BLOWING ON THE 14TH STAGE LOOP CAUSING WARNING MESSAGE. RMay 3, 2016 · N423SW · Cndair CL6002B19 · Cabin Cooling SystemSDR SWIA201541136Battery Pack · dischargedEMERGENCY LIGHTS ARE INOPERATIVE. CHARGED EMERGENCY LIGHT BATTERIES. ALL LIGHTS OPS CHECKED GOOD IAW AMM.Apr 17, 2015 · N423SW · Cndair CL6002B19 · Emergency LightingSDR SWIA201439496Proximity Sensor · damagedGEAR DISAGREE. NOSE GEAR DOORS. RETURNED TO FIELD. NOSE GEAR PROXIMITY SWITCH HAD BEEN DAMAGED.Oct 14, 2014 · N423SW · Cndair CL6002B19 · Landing Gear Position and WarningSDR SWIA201439261Bracket · bentAFTER TAKE OFF WHEN RETRACTING THE LANDING GEAR THE NOSE GEAR DID NOT RETRACT. RECEIVED A GEAR DISAGREE WARNING MESSAGE AND NOSE DOOR OPEN WARNING MESSAGE. FOLLOWED QRH AND LANDED. R & R THE BENT NLG OLEO CENTERED/EXTENDED PROXIMITY SENSOR, PSI4GA, BRACKET Sep 8, 2014 · N423SW · Cndair CL6002B19 · Main Landing Gear Attach SectionSDR SWIA201439206Acm · overtempRETURNED TO DEPARTURE DUE TO A RT PACK HIGH TEMP. R & R RIGHT ACM.Aug 24, 2014 · N423SW · Cndair CL6002B19 · Cabin Cooling SystemSDR SWIA201439150Bracket · brokenGEAR DISAGREE. RETURNED TO THE FIELD. CLOSED, R & R NLG WOW SENSOR BRACKET IAW CMM. ADJUSTED NLG WOW SENSOR IAW CMM. OPS CHECKED GOOD. PERFORMED LANDING GEAR EXTENSION/RETRACTION OPERATIONAL CHECK IAW AMM. NO DEFECTS NOTED.Aug 18, 2014 · N423SW · Cndair CL6002B19 · Main Landing GearSDR SWIA201438914Structure · damagedMULTIPLE DENTS FOUND ON FUSELAGE SKIN AT BS 654.5 - 682 BETWEEN STRINGERS 16 -18L. ACFT OUT OF SERVICE, REPAIRED FRAME, INSTALLED DOUBLER AND REPAIRED STRINGERS 17L AND 18L IAW REO.Jul 8, 2014 · N423SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA201438134Bulb · inoperativeSERVICE DOOR FLOOR LEVEL LIGHTED EMERGENCY EXIT SIGN HAS AN INOPERATIVE BULB. REPLACED THE BULB IAW AMM.Jun 10, 2014 · N423SW · Cndair CL6002B19 · Emergency LightingSDR SWIA201437822Connector · brokenEMERGENCY EXIT LIGHT FOR WARDROBE HAS A BROKEN WIRE CONNECTOR. REPLACED WIRE CONNECTOR IAW ESPM AND AMM.May 21, 2014 · N423SW · Cndair CL6002B19 · Light System WiringSDR SWIA201437823Structure · crackedAPU ENCLOSURE HAS SEVERAL CRACKS AT SPOT WELDS. CLEAN AND WELDED CRACKS IN APU ENCLOSURE IAW EA.May 16, 2014 · N423SW · Cndair CL6002B19 · APU Cowling/ContainmentSDR SWIA201437835Floorbeam · crackedANGLE UNDER FLOORBOARD AT BS 484, LBL 36, CRACKED. C-CHECK, REPAIRED ANGLE IAW REO.May 15, 2014 · N423SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA201437834Floorbeam · crackedANGLE UNDER FLOORBOARD AT BS 484, RBL 27, CRACKED, C-CHECK, REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE IAW STANDARD REPAIR.May 15, 2014 · N423SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA201437833Floor Panel · corrodedLEFT PRESSURE FLOOR DOUBLER BS 409+128 - 473.15 HAS FOUR AREAS OF CORROSION. C-CHECK, REMOVED CORROSION IAW REO.May 15, 2014 · N423SW · Cndair CL6002B19 · Fuselage Floor PanelSDR SWIA201437832Floor Panel · corrodedLEFT PRESSURE FLOOR DOUBLER BS 473.15 - 513 HAS THREE AREAS OF CORROSION. C-CHECK, REMOVED CORROSION IAW REO.May 15, 2014 · N423SW · Cndair CL6002B19 · Fuselage Floor PanelSDR SWIA201437831Floor Panel · corrodedLEFT PRESSURE FLOOR DOUBLER BS 513-559 HAS FIVE AREAS OF CORROSION. C-CHECK, REMOVED CORROSION IAW REO.May 15, 2014 · N423SW · Cndair CL6002B19 · Fuselage Floor PanelSDR SWIA201437830Web · corrodedLEFT PRESSURE FLOOR WEB, BS 441, CORRODED AT NUTPLATE. C-CHECK, REMOVED CORROSION IAW REO.May 15, 2014 · N423SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201437829Web · corrodedLT PRESSURE FLOOR WEB BS 460 CORRODED AT NUTPLATE. C-CHECK, REMOVED CORROSION IAW REO.May 15, 2014 · N423SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201437828Web · corrodedLEFT PRESSURE FLOOR WEB BS 540 CORRODED AT NUTPLATE. C-CHECK, REMOVED CORROSION IAW REO.May 15, 2014 · N423SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201437827Web · corrodedLEFT PRESSURE FLOOR WEB, BS 548, CORRODED AT NUTPLATE, C-CHECK, REMOVED CORROSION IAW REO.May 15, 2014 · N423SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201437826Floor Panel · corrodedRT PRESSURE FLOOR DOUBLER BS 409+128-473.15 HAS FOUR AREAS OF CORROSION. C-CHECK REMOVED CORROSION IAW REO.May 15, 2014 · N423SW · Cndair CL6002B19 · Fuselage Floor PanelSDR SWIA201437825Floor Panel · corrodedRIGHT PRESSURE FLOOR DOUBLER BS 473.15-513 HAS THREE AREAS OF CORROSION. C-CHECK REMOVED CORROSION IAW REO.May 15, 2014 · N423SW · Cndair CL6002B19 · Fuselage Floor PanelSDR SWIA201437824Floor Panel · corrodedRIGHT PRESSURE FLOOR DOUBLER BS 513-559 HAS FOUR AREAS OF CORROSION. C-CHECK, REMOVED CORROSION IAW REO.May 15, 2014 · N423SW · Cndair CL6002B19 · Fuselage Floor PanelSDR SWIA201437840Frame · corrodedLOWER FRAME SECTION AT BS 333 IS CORRODED BEYOND LIMITS. C-CHECK, REPLACED LOWER FRAME SECTION IAW SRM.May 13, 2014 · N423SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA201437839Frame · failedLOWER FRAME SECTION AT BS 349 IS BEYOND LIMITS. C-CHECK, INSTALLED NEW LOWER FRAME SECTION IAW SRM.May 13, 2014 · N423SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA201437838Frame · failedLOWER FRAME SECTION AT BS 319.7 IS BEYOND LIMITS. C-CHECK, INSTALLED NEW LOWER FRAME SECTION IAW SRM.May 13, 2014 · N423SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA201437837Window Frame · crackedPOSSIBLE CRACK ON WINDSHIELD CENTER POST LEFT LOWER ANGLE FITTING. C-CHECK, REPLACED POST IAW SRM.May 13, 2014 · N423SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA201437836Angle · crackedBS 625, ANGLE IS CRACKED S14L. C-CHECK, REPLACED ANGLE IAW SRM.May 13, 2014 · N423SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201437846Skin · corrodedLOWER AFT FUSELAGE SKIN HAS CORROSION AT SEVERAL FASTENERS FROM BS 559+88 - 559 +112 AT LOWER CENTERLINE. C-CHECK, REMOVED CORROSION IAW EA.May 11, 2014 · N423SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201437845Skin · gougedAFT FUSELAGE SKIN HAS A GOUGE AT BS 691, S20L. C-CHECK, REPAIRED SKIN IAW EA.May 11, 2014 · N423SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201437844Hinge Fitting · gougedNR 6 LUG IS GOUGED ON PASSENGER DOOR PIANO HINGE. C-CHECK, BLENDED OUT GOUGE DAMAGE IAW REO.May 11, 2014 · N423SW · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA201437843Vane · chafedRIGHT INBD FLAP VANE INBD L/E IS CHAFED. C-CHECK, BLENDED OUT CHAFE IAW REO.May 11, 2014 · N423SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201437842Vane · chafedRIGHT INBD FLAP VANE CENTER L/E IS CHAFED. C-CHECK, SKIN CAP REPLACED IAW REO.May 11, 2014 · N423SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201437841Vane · chafedRIGHT INBD FLAP VANE OTBD L/E IS CHAFED. C-CHECK, BLENDED OUT DAMAGED AREA IAW REO.May 11, 2014 · N423SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201437850Skin · gougedCARGO DOOR SKIN AROUND HANDLE, HAS THREE GOUGES. TWO AT FWD AREA OF HANDLE AND ONE AT AFT END. C-CHECK, REPAIRED GOUGES IAW GREO.May 9, 2014 · N423SW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR SWIA201437849Vane · chafedLEFT WING INBD FLAP VANE UPPER L/E OF VANE CHAFED, JUST INBD OF FLAP VANE, INBD SLIDING ACTUATOR. C-CHECK, REPLACED LEFT WING INBD FLAP VANE INBD L/E IAW SRM.May 9, 2014 · N423SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201437848Vane · chafedLEFT WING INBD FLAP VANE-UPPER L/E OF VANE CHAFED JUST OTBD OF FLAP VANE OTBD SLIDING ACTUATOR, C-CHECK, BLENDED OUT DAMAGED AREA IAW REO.May 9, 2014 · N423SW · Cndair CL6002B19 · Trailing Edge Flaps
Back to N423SW, cancelled Mar 6, 2023