N938SW

Service difficulty reports · 128

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 = 'N938SW' 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 SWIA200820366Window · crackedFLT 5836 - CAPTAIN'S SIDE WINDOW CRACKED. REPLACED WINDOW.Nov 14, 2008 · N938SW · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA200820205Lens · missingFLT 6014 - OVERHEAD EXIT SIGN IN CABIN MISSING RED/LENS COVER. REPLACED RED/LENS COVER. Oct 17, 2008 · N938SW · Cndair CL6002B19 · Emergency LightingSDR SWIA200819145Connector · disconnectedOVERWING EMERGENCY EXIT SIGN DOES NOT ILLUMINATE, FLIGHT NR 6369. INSPECTED AND SECURED CONNECTOR ON ELBP 2 CHARGER IAW CRJ 200 MM 33-51-05.Jan 28, 2008 · N938SW · Cndair CL6002B19 · Light System WiringSDR SWIA200719164Structure · crackedLEFT OUTBOARD FLAP IS CRACKED ALONG TRAILING EDGE, FOUND AT C-CHECK. REPLACED FLAP ASSEMBLY PER CRJ200 AMM 27-54-05-400-801.Oct 19, 2007 · N938SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA200719163Floorbeam · crackedLBL9 AT FS 280 IS CRACKED AT LOWER RADIUS, FOUND AT C-CHECK. COMPLIED WITH FLOORBEAM REPAIR IAW CRJ200 REO 601R-53-11-171 REV C.Oct 19, 2007 · N938SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200719162Floorbeam · crackedLBL 9 AT FS 280 SHOWS SIGNS OF CRACKING, FOUND AT C-CHECK. COMPLIED WITH REPAIR OF CRACKED ANGLE AT FS 280 AND LBL 9 FLOORBEAM IAW CRJ200 REO 601R-53-11-138 REV NC.Oct 19, 2007 · N938SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200718712Inverter · inoperativeFLT 6445 - EMERGENCY LIGHTING ALONG FLOOR STRIP IS INOP. REPLACED NR 2 EMERGENCY LIGHT INVERTER IAW 33-51-07. OPS CHECK GOOD.Sep 24, 2007 · N938SW · Cndair CL6002B19 · Emergency LightingSDR SWIA200718703Connector · disconnectedFLT 5967 - THE EMERGENCY FLOOR LIGHTING BETWEEN ROWS 2 AND 5 DOES NOT WORK. ALSO, THE EMERGENCY EXIT SIGN BELOW THE LEFT WING EMERGENCY EXIT DOES NOT WORK. SECURED PLUG AT LIGHT STRIP. OPS CHECK GOOD FOR ALL LIGHTS IAW AMM 33-25-00.Sep 17, 2007 · N938SW · Cndair CL6002B19 · Emergency LightingSDR SWIA200718552Structure · crackedAFT PORTION OF PAX DOOR IS CRACKED UNDERNEATH TOP STEP. REPAIRED CRACK IAW REO 601R-52-11-279.Jul 31, 2007 · N938SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA200718551Structure · crackedFORWARD PORTION OF PAX DOOR IS CRACKED UNDERNEATH TOP STEP. REPAIRED CRACK IAW AMM REO 601R-52-11-279.Jul 31, 2007 · N938SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA200617146Window · crackedON DESCENT THROUGH 8000' FIRST OFFICER'S SIDE WINDOW CRACKED. REPLACED FIRST OFFICER'S SIDE WINDOW IAW 56-12-01 AND RII 56-220-1000. OPERATIONAL CHECKS GOOD, SN OFF: 02196H1120.Sep 9, 2006 · N938SW · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA200616934B-Nut · looseFUEL ODOR IN COCKPIT DURING APU USEAGE. SECURED LOOSE (B) NUT ON APU FUEL SHUTOFF VALVE. OPERATIONAL CHECKS GOOD.Aug 3, 2006 · N938SW · Cndair CL6002B19 · APU Engine Fuel and ControlSDR SWIA200616879Angle · crackedPAX DOOR; AFT DRAG ANGLE CRACKED BELOW POWER ASSIST MOTOR, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED MADE REPAIR PARTS ON PAX DOOR AFT DRAG ANGLE IAW AREO 601R 52-11-513 REV 'A'. A.INFANTI 03-26-06.Mar 17, 2006 · N938SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA200616878Fitting · crackedMAIN FWD AVIONICS COMPARTMENT FS 280 LBL9 FRAME CLIP CRACKED INBD, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP PN 601R31113-57 PO#58390 IAW CRJ200 REO 601R-53-11-136.Mar 17, 2006 · N938SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200616877Fitting · crackedMAIN FWD AVIONICS COMPARTMENT FS 280.00 RBL9 FRAME CLIP CRACKED INBD AND OTBD, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED (2 EA) PN 601R31113-58 CLIPS AT FS 280 RBL9 INBD AND OTBD PER CRJ200 SRM 51-42-21 AND BOMBARDIER REO 601R-53-11-136.Mar 17, 2006 · N938SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200616876Floor Support · crackedCRACK IN FLOOR SUPPORT FS 621 WL73.5 RBL44, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REO 601R 53-117-4. REPAIR ANGLE AND REO 601R 53-61-117-6 STRAP IAW REO 601R 53-61-117 REV 'C'.Mar 17, 2006 · N938SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200616875Floor Support · crackedCRACK IN FLOOR SUPPORT FS 621 WL73.5 LBL44, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PIECES IAW CRJ200 REO 601R-53-61-117 REV 'C'.Mar 17, 2006 · N938SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200515472Control Unit · malfunctionedSTAB CHANNEL ONE WILL NOT ENGAGE. REPLACED MOTOR CONTROL UNIT IAW MM27-42-05. OPERATIONAL CHECK GOOD.Aug 26, 2005 · N938SW · Cndair CL6002B19 · Stabilizer Position IndicatingSDR SWIA200514860Switch · malfunctionedF/O'S TRIM SWITCH IS STICKY. REPLACED F/O'S TRIM SWITCH IAW MM 27-41-05. OPERATIONAL CHECK GOOD.Apr 8, 2005 · N938SW · Cndair CL6002B19 · Stabilizer Control SystemSDR SWIA200514643Control Panel · malfunctionedON CLIMB, RIGHT RUDDER TRIM WAS USED MOMENTARILY, FOLLOWED BY UNCOMMANDED FULL RIGHT RUDDER TRIM ACTIVATION, AIRCRAFT WAS RETURNED TO TRIMMED CONDITION EASILY OPPOSITE RUDDER AND CORRECTED ALL TOGETHER WITH TRIM SWITCH. NORMAL FOR REMAINDER OF FLIGHT. REPLACFeb 23, 2005 · N938SW · Cndair CL6002B19 · Stabilizer Position IndicatingSDR SWIA200413981Window · failedLEFT SIDE WINDOW SHATTERED. REMOVED AND REPLACED LEFT SIDE WINDOW REF MM 56-12-01. P/N OFF 601R33033-11, S/N OFF 02201H1672.Oct 17, 2004 · N938SW · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA200413903Position Sensor · malfunctionedFLAP FAIL MESSAGE ON TAXI OUT AT 13 DEGREES. REMOVED AND REPLACED RIGHT BPSU PER CRJ MM 27-51-10. REMOVED AND REPLACED NR 2 INBOARD FLAP ACTUATOR AND NR 1 RIGHT INBOARD FLAP ACTUATOR IAW CRJ MM 27-53-01. OPERATIONAL CHECK GOOD. NR 1 P/N 852D100-19, S/N OFFOct 9, 2004 · N938SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA200413886Control Unit · malfunctionedFLAPS FAIL MESSAGE APPEARED WHEN FLAPS SELECTED TO 45 DEGREES. REMOVED AND REPLACED FECU IAW CRJ MM 27-51-05. OPERATIONAL CHECK GOOD.Oct 2, 2004 · N938SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA200413752Angle · crackedAPU COMPARTMENT FS 625.00 STR 14R HAS A CRACKED ATTACH ANGLE. ITEM FOUND AT C-CHECK INSPECTION. REPLACED IAW CRJ SRM 51-40-11, 51-42-06 AND 51-25-16.Aug 21, 2004 · N938SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200413751Angle · crackedAPU COMPARTMENT FS 625.00 STR 14L HAS A CRACKED ATTACH ANGLE. ITEM FOUND AT C-CHECK INSPECTION. REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-25-16.Aug 21, 2004 · N938SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200413750Beam · crackedFUSELAGE TRANSVERSE BEAM LOWER FLANGE IS CRACKED; FS 280.00 RBL 12.0. ITEM FOUND AT C-CHECK INSPECTION. LOWER FLANGE REPAIRED IAW CRJ REO #601R-53-11-171 REV A.Aug 21, 2004 · N938SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA200413749Attach Fitting · crackedFUSELAGE FLOORBEAM TO TRANSVERSE BEAM ATTACH CLIP IS CRACKED FS 280.00 LBL 9.0 O/B CLIP. ITEM FOUND AT C-CHECK INSPECTION. CLIP REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-01, 51-42-13, 51-21-11, 51-25-16.Aug 21, 2004 · N938SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA200413016Connector · damagedEMERGENCY LIGHTS STRIP INSIDE CABIN HAS APPROX 12 FEET OF LIGHTS NOT WORKING BETWEEN ROW 2 AND ROW 5. INSTALLED SERVICEABLE CONNECTOR P38LZ AT ROW 5. OPS CHECKS GOOD.Mar 12, 2004 · N938SW · Cndair CL6002B19 · Light System Wiring
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