N403SW, cancelled Jul 17, 2013

Service difficulty reports · 156

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 = 'N403SW' AND deregistration_id = 'N403SW-2013-07-17'
  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 SWIA200920924Engine · failedFLT 2878 - FLAMES FOLLOWED BY METAL OUT OF APU EXHAUST PIPE. REPLACED APU.Jan 23, 2009 · N403SW · Cndair CL6002B19 · APU Core EngineSDR SWIA200920923Warning Light · illuminatedFLT 2878 - GEAR DISAGREE WARNING FOR 10 SECONDS AFTER GEAR RETRACTED. INTERROGATED PSEU, SWUNG GEAR, UNABLE TO DUPLICATE.Jan 21, 2009 · N403SW · Cndair CL6002B19 · Landing Gear Position and WarningSDR SWIA200820650Wire Harness · shortedFLT 2670 - 'GEAR DISAGREE' DISPLAYED AFTER TAKEOFF. REMOVED AND REPLACED NLG WOW NR 2 ELECTRICAL HARNESS, PN 750006000, SN ON 1976, SN OFF 1353.Dec 11, 2008 · N403SW · Cndair CL6002B19 · Landing Gear System WiringSDR SWIA200820570Fitting · crackedWINDSHIELD CENTER POST LOWER RIGHT FITTING AT WL 110.0 IS CRACKED IN THE BEND RADIUS, AD INSP. REPLACED PER SRM.Dec 1, 2008 · N403SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA200820569Angle · crackedLEFT WINDSHIELD AFT POST LOWER AFT ANGLE IS CRACKED IN THE BEND RADIUS, AD INSP. REPLACED PER SRM.Dec 1, 2008 · N403SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200820568Angle · crackedRIGHT WINDSHIELD AFT POST LOWER AFT ANGLE IS CRACKED IN THE BEND RADIUS (AD INSP). REPLACED PER SRM.Dec 1, 2008 · N403SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200820510Actuator · sluggishFLT 2871 - RIGHT MAIN GEAR RETRACTION TIME LONGER THAN NORMAL. REPLACED RIGHT MAIN GEAR ACTUATOR, P/N: 17008-115, S/N ON, 01021 S/N OFF: 01753.Nov 26, 2008 · N403SW · Cndair CL6002B19 · Landing Gear ActuatorSDR SWIA200820016Proximity Switch · malfunctioned"NOSE GEAR DOOR" WARNING MESSAGE AFTER TAKEOFF, RETURNED TO FIELD. REPLACED PROX SWITCH PS18GA. OPS CHECK GOOD. Sep 5, 2008 · N403SW · Cndair CL6002B19 · Landing Gear Position and WarningSDR SWIA200819984Filter · dirtyADG DEPLOYED AFTER RECEIVING GENERATOR 1 OFF CAUTION MESSAGE FOLLOWED BY GENERATOR 2 OFF MESSAGE. FLIGHT 2781. SERVICED BOTH IDG'S IAW AMM 12-13-24. REPLACED NR 1 IDG FILTER IAW AMM 24-12-01. IDG'S OPS CHECK GOOD. Aug 22, 2008 · N403SW · Cndair CL6002B19 · AC Generator-AlternatorSDR SWIA200819858Actuator · faultyRECEIVED UNCOMMANDED YAW DURING FLIGHT. (FLIGHT NR 2512) REPLACED YAW DAMPER NR2 LINEAR ACTUATOR IAW AMM 22-22-01. OPS CHECK GOOD. P/N 622-9968-101, S/N OFF 714. Jul 12, 2008 · N403SW · Cndair CL6002B19 · Autopilot SystemSDR SWIA200819810Panel · unlatchedFLT 2825 - OXYGEN PANEL AT ROW 5 DROPPED OPEN IN FLIGHT. RESECURED PANEL FOR PSU IAW 25-28-01. Jun 22, 2008 · N403SW · Cndair CL6002B19 · DoorsSDR SWIA200819655Adc · malfunctionedFLT 2805 - RIGHT SIDE ALTIMETER SETTING WILL CHANGE RANDOMLY WHILE SETTING SPEEDS. REPLACED FLIGHT CONTROL PANEL IAW AMM 22-11-07 AND NR 2 ADC IAW MM 34-11-00. OPS CHECK GOOD, P/N 822-0044-001, S/N OFF 2FX8T.May 18, 2008 · N403SW · Cndair CL6002B19 · Air Data ComputerSDR SWIA200819625Lens · brokenPAX DOOR EMERGENCY FLOODLIGHT LENS COVER AND BASE IS BROKEN. REPLACED EMERGENCY LIGHT FLOODLIGHT ASSEMBLY. OPS CHECK GOOD. May 7, 2008 · N403SW · Cndair CL6002B19 · Emergency LightingSDR SWIA200819432Selector Valve · malfunctionedFLT 2555 - RECEIVED A NOSE DOOR OPEN MASTER WARNING. REPLACED NOSE DOOR SELECTOR VALVE AND CHECK VALVE PER AMM 33-22-20. OPS CHECK GOOD, P/N 750006000, S/N OFF 1640.Apr 1, 2008 · N403SW · Cndair CL6002B19 · Landing Gear Door Retract SectionSDR SWIA200819082Light · smokeFLT 6474 - SMOKE REPORTED AT SIDEWALL AREA NEAR ROW 5. REPLACED SIDEWALL LIGHTING FIXTURE. OPS CHECK GOOD. Jan 9, 2008 · N403SW · Cndair CL6002B19 · Flight Compartment LightingSDR SWIA200719000Selector Valve · malfunctionedFLT 3822 - RECEIVED A TRIPLE CHIME AND "NOSE DOOR OPEN" WARNING MESSAGE CLIMBING THRU 9,000'. REPLACED MLG SELECTOR VALVE IAW 32-32-10 AS WELL AS MANUAL BYPASS AND RUNAROUND VALVE IAW 32-32-2. OPS CHECK GOOD, PN: 750004000-003, SN OFF: 058, PN: 750005000, SNDec 26, 2007 · N403SW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA200718845Nut Plate · corrodedLAVATORY FLOOR NUTPLATES ARE CORRODED, FOUND AT C-CHECK. REPLACED NUTPLATES ON LAVATORY FLOOR. Jul 27, 2007 · N403SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA200718844Door Frame · corrodedLEFT EMERGENCY EXIT DOOR SURROUND HAS CORRODED HINGE PINS, FOUND AT C-CHECK. REPLACED PINS ON LEFT EMERGENCY EXIT DOOR SURROUND PER CRJ200 AMM 20-24-00-910-801.Jul 27, 2007 · N403SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA200718843Bolt · scoredRIGHT ENGINE FORWARD MOUNT BOLTS SHOW SIGNS OF SHANK SCORING BELOW HEAD OF BOLT, FOUND AT C-CHECK. REPLACED FORWARD ENGINE MOUNT BOLTS PER CRJ200 AMM SUBTASK 71-00-00-420-001 PARA A ITEMS 15-20. Jul 27, 2007 · N403SW · Cndair CL6002B19 · Engine Mount SectionSDR SWIA200718842Mount · corrodedLEFT ENGINE AFT MOUNT FITTING BALL BEARING IS CORRODED, FOUND AT C-CHECK. REPLACED LEFT ENGINE AFT MOUNT FITTING PER CRJ200 AMM 71-22-01-000-801.Jul 27, 2007 · N403SW · Cndair CL6002B19 · Engine Mount SectionSDR SWIA200718841Mount · corrodedRIGHT ENGINE AFT MOUNT THRUST FITTING BALL RACE IS CORRODED, DISCOVERED AT C-CHECK. REPLACED RIGHT ENGINE AFT MOUNT THRUST FITTING ASSEMBLY IAW CRJ200 AMM 71-22-01-000-801 AND 71-22-01-400-801. Jul 27, 2007 · N403SW · Cndair CL6002B19 · Engine Mount SectionSDR SWIA200718840Floorbeam · crackedCARGO FLOOR SUPPORT STRUCTURE IS CRACKED AT FS 559 + 90 AND RBL27 ON INBD SIDE, DISCOVERED AT C-CHECK. COMPLIED WITH REPAIR PER CRJ200 SRM 53-00-43. Jul 27, 2007 · N403SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200718839Door Frame · crackedPAX DOOR FRAME IS CRACKED STA 338, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS ON PAX DOOR PER REO 601R-52-11-402 REV G. Jul 27, 2007 · N403SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA200718838Stiffener · crackedCRACKED VERTICAL STIFFENER AT FS 280.0 AND LBL27, DISCOVERED AT C-CHECK. INSTALLED NEW FABRICATED ANGLE AT FS280 AND LBL 27 IAW CRJ200 SRM 51-42-06 PG 11. Jul 27, 2007 · N403SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200718837Floorbeam · crackedCRACK FOUND ON SUPPORT ANGLE UNDER FLOOR PANEL 262DRF AT FS480, DISCOVERED AT C-CHECK. INSTALLED NEW SUPPORT AT FS484 AND RBL36 PER CRJ200 SRM 51-23-00, 51-42-06 AND 51-42-21. Jul 27, 2007 · N403SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200718836Skin · crackedCRACK IN FUSELAGE SKIN AT BS 235 AND RBL6, DISCOVERED AT C-CHECK. INSTALLED REPAIR PARTS PER REO 601R 53-11-048 REV B. Jul 27, 2007 · N403SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA200718184Striker · damagedFOUND MAIN CABIN DOOR IS SQUEALING VERY LOUDLY. RETURNED TO SLC. REPAIRED DOOR SEAL STRIKER IAW CRJ REO 601R-53-22-033.Apr 27, 2007 · N403SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA200617129Lamp · failedAFT OVERHEAD EMERGENCY LIGHT INOP. RELAMPED AFT MOST OVERHEAD EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD.Aug 29, 2006 · N403SW · Cndair CL6002B19 · Emergency LightingSDR SWIA200616369Clip · crackedFS 280 - LT INBOARD CLIP IS CRACKED AT LBL 9; WL 70 - JUST BELOW FLOOR. ITEM FOUND AT C-CHECK INSPECTION. REPLACED LT INBOARD CLIP AT LBL 9 WL 70 PER CRJ200 SRM 57-42-21-PG 1 AND 2.Jan 3, 2006 · N403SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA200616368Seat Track · wornPILOTS SEAT RAILS ARE WORN. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED PILOT SEAT TRACK IAW AMM 53-01-05-400-801.Jan 3, 2006 · N403SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA200616367Bracket · crackedFS 625.30 LT AFT EQUIPMENT BAY BRACKET CRACKED BETWEEN STR 15 & STR 16. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED BRACKET PER CRJ200 51-42-21- PG 13-17 AND CRJ200 SRM 51-77-00 PG 1.Jan 3, 2006 · N403SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200616366Bracket · crackedFS 625.30 RT AFT EQUIPMENT BAY BRACKET CRACKED BETWEEN STR 15 & STR 16 FWD SIDE OF FRAME. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED BRACKET AT FS 625.30 RT BETWEEN STR 15 & STR 16 IAW CRJ200 SRM 51-42-06-21.Jan 3, 2006 · N403SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA200616365Floorbeam · crackedFS 280 - CROSSMEMBER SUPPORT ANGLE IS CRACKED AT (2) PLACES - RBL 3 & RBL 9 IN THE UPPER AFT RADIUS - WL 71. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED CLIPS AND REPAIR PARTS AT FS 280 APPROX LBL 11 - RBL 11 IAW REO 601R-53-11-136.Jan 3, 2006 · N403SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200616364Intercostal · crackedRT INTERCOSTAL AT FS 625 AND RT STRINGER IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED INTERCOSTAL AT FS 625.00 & RT STR 16 IAW CRJ200 SRM 51-42-06.Jan 3, 2006 · N403SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200616363Frame · crackedCARGO COMPARTMENT - FS 605 LT - CRACKED FRAME (605) UNDERNEATH DOOR THRESHOLD. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED DOOR THRESHOLD CLIP IAW CRJ200 SRM 51-42-06 PG 16 FIG 9.Jan 3, 2006 · N403SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA200515544Trim Switch · inoperativeCAPTAIN'S YOKE PITCH TRIM INOP. REPLACED CAPTAIN'S YOKE TRIM SWTICH IAW 27-41-05, OPERATIONAL CHECK GOOD.Sep 11, 2005 · N403SW · Cndair CL6002B19 · Stabilizer Control SystemSDR SWIA200515246Control Lever · malfunctionedFLAPS FAIL CAUTION MESSAGE. REPLACED CONTROL LEVER IAW 27-51-01. OPERATIONAL CHECK GOOD.Jul 3, 2005 · N403SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA200514615Bpsu · malfunctionedFLAPS FAIL CAUTION MESSAGE. REPLACED RIGHT BPSU IAW MM 27-51-10. OPERATIONAL CHECK GOOD.Feb 18, 2005 · N403SW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR SWIA200514525Lever · malfunctionedFLAPS FAIL CAUTION MESSAGE DURING CRUISE. REMOVED AND REPLACED FLAP HANDLE ASSY IAW MM CH 27-51-01. OPERATIONAL CHECK GOOD.Feb 6, 2005 · N403SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA200514424Position Sensor · malfunctionedINBOUND TO SLC AT 18,000 FEET FLAP FAIL CAUTION MESSAGE APPEARED. REMOVED AND REPLACED RIGHT SIDE BPSU IAW 27-51-01. OPERATIONAL CHECK GOOD.Jan 23, 2005 · N403SW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR SWIA200414244Control Unit · malfunctionedSPOILERONS FAULT STATUS MESSAGE. REPLACED RIGHT INBOARD SPOILERON PCU IAW MM 27-62-01. REPLACED NR 2 SECU IAW MM 27-61-05. OPERATIONAL CHECK GOOD, PN 27000-7, SN OFF 3779.Dec 12, 2004 · N403SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200414121Actuator · malfunctionedWHEN SELECTING FLAPS 8 FLAPS FAIL CAUTION MESSAGE. REPLACED RIGHT INBOARD FLAP ACTUATOR; RIGHT INBOARD FLAP OUTBOARD ACTUATOR; LEFT WING INBOARD FLAP INBOARD ACTUATOR; LEFT WING INBOARD FLAP OUTBOARD ACTUATOR IAW SB 601R27-120 AND MM 27-53-01, 27-53-05. OPERNov 20, 2004 · N403SW · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR SWIA200414069Control Unit · malfunctionedINFLIGHT THE FLIGHT/GROUND SPOILERS FAULT AND THE INBOARD GROUND SPOILER FAULT MESSAGE CAME ON. REMOVED AND REPLACED NR 2 SECU PER CRJ MM 27-61-05. OPERATIONAL CHECK GOOD.Nov 8, 2004 · N403SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200413799Frame · crackedLT FS 718 BETWEEN STRINGERS 10L AND 12L IS CRACKED 1INCH LONG IN RADIUS OF FRAME FLANGE. (ITEM FOUND AT C-CHECK INSPECTION.) SB 601R-53-055 REVISION A, STRUCTURAL REPAIR AT FUSELAGE STATION (FS) 718.00 BETWEEN STRINGERS 10 AND 12, PART B INCORPORATED.Jun 12, 2004 · N403SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA200413798Frame · crackedRT FS 718 BETWEEN STRINGERS 10R AND 12R IS CRACKED 1INCH LONG IN RADIUS OF FRAME FLANGE. (ITEM FOUND AT C-CHECK INSPECTION.) SB 601R-53-055, REV-A STRUCTURAL REPAIR AT F.S. 718.00 RT BETWEEN STRINGERS 10 AND 12, PART-E INCORPORATED.Jun 12, 2004 · N403SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA200413743Floor Support · corrodedPAX DOOR LOWER THRESHOLD FLOOR SUPPORT ANGLE CORRODED. ( ITEM FOUND AT C-CHECK INSPECTION.) INSTALLED FLOOR SUPPORT ANGLE IAW CRJ 200 SRM CHAP. 51-42-01, 51-42-13, AND 51-42-21.Jun 12, 2004 · N403SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200413742Threshold · corrodedSERVICE DOOR THRESHOLD (SILL) CORRODED BEYOND LIMITS. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW SERVICEABLE SERVICE DOOR THRESHOLD IAW CRJ SRM 51-41-02.Jun 12, 2004 · N403SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200413741Angle · crackedFS 484.00 ANGLE CRACKED AT RBL 27 OUTBOARD SIDE. ITEM FOUND AT C-CHECK INSPECTION. REMOVED AND REPLACED FS 484 RBL 27 OUTBOARD INTERCOSTAL ANGLE IAW BOMBARDIER INC REO 601R-53-41-059 REV A.Jun 12, 2004 · N403SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200413740Seat Track · corrodedAREAS OF CORROSION BELOW LEFTHAND EMERGENCY EXIT ON SIDE SEAT RAIL. ITEM FOUND AT C-CHECK INSPECTION. REMOVED SIDE SEAT RAIL AND INSTALLED NEW SEAT RAIL SECTION IAW REO 601R-53-00-055.Jun 12, 2004 · N403SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA200413739Angle · crackedLEFTHAND 621.00 ANGLE CRACKED OUTBOARD END. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR PARTS IAW BOMBARDIER REO 601R-53-61-004.Jun 12, 2004 · N403SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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