N445SW

Service difficulty reports · 275

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 = 'N445SW' 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 SWIA200515735Floorbeam · crackedRIGHT FLOORBEAM ANGLE AT FS 621.00 BETWEEN RBL 27 AND RBL 45. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR PARTS PER REO 601R-53-61-117 AND CRJ200 SRM 51-42-06 AND SRM 51-42-21.May 6, 2005 · N445SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200515734Floorbeam · crackedLEFT FLOORBEAM ANGLE AT FS 621 BETWEEN LBL 27 AND LBL 45. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR PARTS PER REO 601R-53-61-117 AND CRJ200 SRM 51-42-06 AND 51-42-21.May 6, 2005 · N445SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200515733Clip · crackedFS 280 LBL 9, 2 EA CLIPS CRACKED I/B & O/B. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED CLIPS IAW ENG DWG 601R31113 AND CRJ200 SRM CG 51-42-06 & 51-42-20.May 6, 2005 · N445SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA200515732Clip · crackedFS 280 RBL 9 (2 EA) CLIPS CRACKED I/B & O/B. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED RIGHT O/B CLIP PER CRJ200 SRM 51-42-06 & 51-40-20. INSTALLED RIGHT I/B CLIP PER CRJ200 SRM 51-42-06.May 6, 2005 · N445SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA200514811Oxygen Mask · deployedAFTER OPENING MAIN CABIN DOOR, ALL O2 MASKS DEPLOYED. RE-PACKED PASSENGER O2 MASKS IAW AMM 35-21-09.Mar 29, 2005 · N445SW · Cndair CL6002B19 · Passenger Oxygen SystemSDR SWIA200514340Pcu · inoperativeRIGHT SPOILERON NR 3 PCU INOPERATIVE. REMOVED AND REPLACED RIGHT OUTBOARD SPOILER ON PCU WITH SERVICEABLE UNIT IAW MM 27-62-01. REPLACED RIGHT SECU WITH SERVICEABLE UNIT, MM 27-60-00. OPERATIONAL CHECK GOOD. P/N 49-164-06, S/N OFF: 01624.Jan 3, 2005 · N445SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200414268Control Unit · malfunctionedINBOARD GROUND SPOILERS STATUS ON AFTER 2ND ENGINE START. REMOVED AND REPLACED NR 1 SECU IAW MM CH 27-61-05, OPERATIONAL CHECK GOOD.Dec 14, 2004 · N445SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200414163Light · inoperativeFIRST GREEN SECTION OF THE EMERGENCY FLOOR PATH LIGHTS IS OUT. REPLACED FORWARD GREEN EMERGENCY FLOOR LIGHTING STRIP IAW CRJ MM 33-51-01, OPERATIONAL CHECK GOOD.Nov 27, 2004 · N445SW · Cndair CL6002B19 · Emergency LightingSDR SWIA200413916Switch · dirtyMACH TRIM AND STAB TRIM CAUTION MESSAGES INFLIGHT AT CRUISE ALTITUDE. CLEANED PILOTS SIDE SWITCH. PERFORMED TEST OF HSTCU, OPERATIONAL CHECK GOOD.Oct 10, 2004 · N445SW · Cndair CL6002B19 · Stabilizer Position IndicatingSDR SWIA200413390Pcu · malfunctionedSPOILERON FAULT MESSAGE. REPLACED HYDRAULIC NR 1 PRESSURE SWITCH, LEFT SPOILERON PCU AND NR 2 SECU. OPS CHECK GOOD IAW MM CH 27-62-01. P/N 49-164-06, S/N OFF 01598.Jun 4, 2004 · N445SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200413259Actuator · malfunctionedNR 2 STAB TRIM WOULD NOT ENGAGE. REMOVED AND REPLACED HSTA IAW MM 27-42-05, 27-42-01 & 27-40-00. REPLACED MCU P/N: 7062-3, S/N OFF: 904. REPLACED STAB ENGAGE PANEL. P/N: 601R51706-3. OPS CHECK GOOD.May 4, 2004 · N445SW · Cndair CL6002B19 · Stabilizer Control SystemSDR SWIA200412883Pcu · malfunctionedON TAXI OUT, SPOILERONS FAULT STATUS MESSAGE. REMOVED AND REPLACED RIGHT SPOILERON OUTBOARD PCU AND SECU NR 1. OPS CHECK SATISFACTORY. LEAK CHECK SATISFACTORY IAW MM 27-60-03. PCU P/N: 49-164-06, S/N OFF: 01389.Feb 8, 2004 · N445SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200412773Control Unit · malfunctionedCREW REPORTS GROUND SPOILER FAULTS. REMOVED & REPLACED NR 1 SECU, REF MM 27-61-05. OPS CHECKS GOOD.Jan 14, 2004 · N445SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200312729Angle · crackedFS 625 RIGHT INTERCOSTAL ANGLE STR 14R CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11. P/N: 601-35012-52Dec 24, 2003 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200312728Angle · crackedFS 625 LT INTERCOSTAL ANGLE STR 14L CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11. P/N: 601-35012-51Dec 24, 2003 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200312727Clip · crackedFS 484 RT INTERCOSTAL I/B CLIP RBL 27 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. CLIP REPLACED IAW REO 601R-53-41-059 REV ''A''.Dec 24, 2003 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200312726Handle · crackedPAX DOOR OUTER HANDLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. PAX DOOR OUTER HANDLE INSTALLED IAW CRJ MM 52-11-03-400-802.Dec 24, 2003 · N445SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA200312725Floorbeam · crackedFS 280 RT FLOORBEAM RBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. DISCOVERED DURING C-CHECK INSPECTION. ANGLES REPLACED IAW CRJ SRM 51-40-11 AND RII 53-401.Dec 24, 2003 · N445SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200312446Ecu · malfunctioned''FLAPS FAIL'' CAUTION DURING CRUISE FLIGHT. NO FLAP LANDING IAW QRH. REMOVED AND REPLACED FECU IAW CL 600 MM 27-51-05. OPS CHECKS GOOD.Sep 20, 2003 · N445SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA200312387Wire · broken(STALL FAIL) MESSAGE WHILE ENROUTE COMPLIED WITH THE APPROPRIATE QRH PROCEDURE. REPAIRED BROKEN WIRE AT CONNECTOR FOR CAPT STICK SHAKER.Sep 2, 2003 · N445SW · Cndair CL6002B19 · Flight Control System WiringSDR SWIA200312175Bpsu · malfunctionedFLAP FAIL CAUTION MESSAGE APPEARED 20 MIN AFTER DEPARTURE. REMOVED AND REPLACED LT BPSU. RIGGED LEFT AND RIGHT BPSU IAW MM 27-51-10. FOUND FECU POTENTIOMETER OUTSIDE LIMIT. ADJUSTED FECU POTENTIOMETERS. REMOVED AND REPLACED FLAP CONTROL LEVER PER CRJ MM 2Jul 12, 2003 · N445SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA200312013Control Unit · malfunctionedFLT SPOILER AND O/B GROUND SPOILER STATUS MESSAGES ILLUMINATED. REMOVED AND REPLACED LEFT SECU. MESSAGES NO LONGER DISPLAYED. OPS CHECK GOOD AT THIS TIME. S/N OFF 01600.May 26, 2003 · N445SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200311867Structure · burnedLEFT OUTBOARD FLAP TRAILING EDGE HAS SEVERAL BURNED AREAS AS A RESULT OF A LIGHTNING STRIKE. INSTALLED SERVICEABLE FLAP ON LEFT OUTBOARD POSITION IAW 27-54-01 AND 27-54-05. S/N OFF: SB/RJ/731.Mar 31, 2003 · N445SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA200211069Wire · shortedAT ROTATION, WINDSHEAR FAIL STATUS MESSAGE AND STICK SHAKER ACTUATION UP TO 180 KNTS. RETURNED FOR LANDING AT SLC. FOUND WIRE CG51C22 SHORTING AT FLAP POSITION TRANSMITTER CANNON PLUG P1CF. REMOVED DAMAGED WIRE LENGTH AND REPLACED SOCKETS ON ALL WIRES TOJul 17, 2002 · N445SW · Cndair CL6002B19 · Flight Control System WiringSDR SWIA200211054Wire · shortedUPON ROTATION IN OKC, THROUGH 10 DEGREE PITCH UP, STICK SHAKER ACTIVATED. WINDSHEAR FAIL STATUS MESSAGE AND CONTINUOUS IGNITION, AIRSPEED WAS ROUGHLY 165 KTS. THEN ON FINAL IN SLC, GEAR WAS COMING DOWN, WINDSHEAR FAIL MESSGE APPEARED AGAIN, CONTINUOUS IGNITIJul 14, 2002 · N445SW · Cndair CL6002B19 · Flight Control System Wiring
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