N916SW

Service difficulty reports · 286

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 = 'N916SW' 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 SWIA200515321Roller · out of adjustMAIN CABIN DOOR STICKS. MOVED FWD SPIGOT ON PAX DOOR AFT .032". ADJUSTED AS NECESSARY TOP FWD SPIGOT AND FWD TEFLON ROLLER ON PAX DOOR. ALSO, REMOVED AND REPLACED BOTH PAX DOOR GAS SPRING IAW AMM 92-11-17, OPS CHECK GOOD AT THIS TIME.Jul 22, 2005 · N916SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA200515322Pcu · malfunctionedFLT SPLRS FAULT STATUS MESSAGE ON ED2 UPON TOUCHDOWN. FLT CONTROL PAGE VERIFIED THE LEFT FLT SPOILER WAS AT FAULT. REMOVED AND REPLACED LEFT FLIGHT SPOILER INBOARD PCU PER 27-62-01. PERFORMED OPS CHECK PER 27-64-00-710-801. OPS CHECK GOOD, NO LEAKS NOTED.Jul 20, 2005 · N916SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200515311Handle · out of adjustFA REPORTS THAT MCD HANDLE WAS VERY HARD TO OPEN. ADJUSTED LOWER TENSION TIES IAW MM 52-11-49. OPERATIONAL CHECK GOOD.Jul 20, 2005 · N916SW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR SWIA200515289Lock · crackedMAIN CABIN DOOR WILL NOT OPEN FROM INSIDE CABIN. REPLACED LATCH LOCK ASSY IAW MM 52-11-25. OPERATIONAL CHECK GOOD.Jul 15, 2005 · N916SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA200515258Fitting · out of adjustMAIN CABIN DOOR WOULD NOT CLOSE. ADJUSTED SPIGOT FITTING IAW AMM TASK 52-11-00-730-801. OPERATIONAL CHECK GOOD.Jul 11, 2005 · N916SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA200515180Fitting · lack of lubeMAIN CABIN DOOR WILL NOT CLOSE. LUBRICATED ALL PAX DOOR FITTINGS AND PINS PER CRJ 200 MM 12-20-52. OPERATIONAL CHECK GOOD.Jun 23, 2005 · N916SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA200515102Smoke Detector · malfunctionedPRIOR TO FINAL APPROACH RECEIVED SMOKE TOILET CAUTION. FOUND NO EVIDENCE OF BURNING OR COMPONENT OVERHEATING IN LAV. PERFORMED LAV SMOKE DETECTOR SELF TEST. SELF TEST GOOD.Jun 4, 2005 · N916SW · Cndair CL6002B19 · Smoke DetectionSDR SWIA200515089Control Unit · malfunctioned"STAB CH 1 INOP" STATUS MSG IN FLIGHT. REPLACED HSTCU IAW CRJ 200 MM CHAPTER 27-41-01. OPERATIONAL CHECK GOOD.Jun 2, 2005 · N916SW · Cndair CL6002B19 · Stabilizer Position IndicatingSDR SWIA200515706Bracket · crackedSTA 621 LT LOWER ANGLE BRACKET (AFT BULKHEAD) CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED LT FLOOR SUPPORT IN ACCORDANCE WITH REO NR 601R-53-61-117Mar 26, 2005 · N916SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA200515705Drag Angle · crackedPAX DOOR AFT DRAG ANGLE IS CRACKED BY DOOR ASSIST PULLEY BRACKET, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR ANGLE SECTION AND SPLICE ANGLES IAW REO 601R-52-11-513 CRJ200 SRM 51-42-06 PG 1-15.Mar 26, 2005 · N916SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA200515704Clip · crackedFS280; CLIPS AT LBL9.0 AND RBL9.0 ARE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. CLIP AT LBL 9.0 INBOARD AND CLIP AT RBL 9.0 INBOARD REPLACED AS REQUIRED IAW SRM 51-42-06 AND 51-42-21.Mar 26, 2005 · N916SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200514361Control Unit · malfunctionedSTAB CHANNEL 2 WOULD NOT ENGAGE. REMOVED AND REPLACED HSTCU PER CRJ 200 MM 27-41-01. OPERATIONAL CHECK GOOD.Jan 9, 2005 · N916SW · Cndair CL6002B19 · Stabilizer Position IndicatingSDR SWIA200514345Actuator · malfunctionedEN ROUTE STAB TRIM CH 2 AND MACH TRIM CAME ON. REMOVED AND REPLACED HSTA IAW CRJ 200 MM 27-42-01 AND HSTCU IAW CRJ 200 MM 27-42-05. OPERATIONAL CHECK GOOD. P/N 7062-3, S/N OFF 1104.Jan 4, 2005 · N916SW · Cndair CL6002B19 · Stabilizer Control SystemSDR SWIA200414174Light · inoperativeCABIN EMERGENCY FLOODLIGHT AT ROW 10 IS INOPERATIVE. RELAMPED EMERGENCY LIGHT IAW CRJ 200 MM 33-51-00, OPERATIONAL CHECK GOOD.Nov 29, 2004 · N916SW · Cndair CL6002B19 · Emergency LightingSDR SWIA200414009Control Unit · malfunctionedDURING DESCENT AP PITCH TRIM CAUTION ILLUMINATED. REPLACE HORIZONTAL STAB ACTUATOR AND MOTOR CONTROL UNIT IAW CRJ MM 27-40-00, 27-42-01, AND 27-42-05. OPERATIONAL CHECK GOOD. P/N 8316-3, S/N OFF 1080.Oct 26, 2004 · N916SW · Cndair CL6002B19 · Stabilizer Position IndicatingSDR SWIA200413845Actuator · malfunctionedSTAB TRIM CHANNEL 1 WILL NOT ENGAGE. REMOVED AND REPLACED HSTA AND MOTOR CONTROL UNIT IAW CRJ 200 MM 27-40-00, 27-42-01, 27-42-05. OPERATIONAL CHECK GOOD. P/N 7062-3, S/N OFF 884.Sep 24, 2004 · N916SW · Cndair CL6002B19 · Stabilizer Control SystemSDR SWIA200413356Panel · malfunctionedSTAB CHANNEL 1 WILL NOT ENGAGE. REMOVED AND REPLACED STAB TRIM ENGAGE PANEL. OPS CHECKS GOOD.May 25, 2004 · N916SW · Cndair CL6002B19 · Stabilizer Position IndicatingSDR SWIA200412998Trim Switch · failedSTAB TRIM CH 1 FAIL TO SET. DEPOWERED AND REPOWER AIRCRAFT. STAB TRIM RESET. REPLACED F/O'S PITCH TRIM DISCONNECT SWITCH WITH SERVICEABLE UNIT IAW CRJ MM 27-41-30.Mar 7, 2004 · N916SW · Cndair CL6002B19 · Stabilizer Position IndicatingSDR SWIA200412874Bulb · burned outRIGHT WING FORWARD EMERGENCY EXIT LIGHT INOP. RELAMPED BULBS. OPS CHECK GOOD.Feb 5, 2004 · N916SW · Cndair CL6002B19 · Emergency LightingSDR SWIA200412792Control Panel · malfunctionedSTAB TRIM CH1 INOP STATUS MESSAGE ON TAXI WOULD NOT RE-ENGAGE. REPLACED STAB TRIM CONTROL PANEL WITH A SERVICEABLE UNIT. OPS CHECK GOOD. P/N 601R51706-3.Jan 19, 2004 · N916SW · Cndair CL6002B19 · Stabilizer Control SystemSDR SWIA200412750Control Unit · malfunctionedON DESCENT INTO DEN, RECEIVED A FLAPS FAIL MESSAGE WHEN MOVING FLAPS FROM 0 DEGREES TO 8 DEGREES. REMOVED AND REPLACED FECU IAW CRJ MM 27-50-00. OPS CHECK GOOD.Jan 4, 2004 · N916SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA200312455Intercostal · crackedFS 484 RT INTERCOSTAL O/B FLANGE RBL 36 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. DAMAGED FLANGE REPAIRED IAW CRJ REO 601R-53-41-059 REV A AND RII 53-401.Sep 3, 2003 · N916SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200312454Handle · crackedPAX DOOR OUTER HANDLE IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. PAX DOOR OUTER HANDLE REMOVED AND REPLACED. P/N: 601R31763-1.Sep 3, 2003 · N916SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA200312453Floorbeam · crackedFS 280 RT FLOORBEAM RBL 9.0 I/B & O/B ATTACH ANGLES CRACKED. DISCOVERED DURING C-CHECK INSPECTION. ANGLES REPLACED IAW CRJ SRM 51-40-11.Sep 3, 2003 · N916SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200312452Plate · crackedFS 589.0; LBL 38; FLOOR LANDING PLATE HAS A CRACK EXTENDING FROM RIVET. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED DAMAGE IAW CRJ REO 601R-53-61-433 REV NC.Sep 3, 2003 · N916SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA200312249Control Panel · faultyYD2 INOPERATIVE, CAME ON DURING TAXI OUT, WAS UNABLE TO RE-ENGAGE. INSTALLED SERVICEABLE YAW DAMPER CONTROL PANEL. OPS CHECK GOOD.Aug 8, 2003 · N916SW · Cndair CL6002B19 · Autopilot SystemSDR SWIA200312102Bulb · burned outLEFT REAR AFT EMERGENCY LIGHT (EXTERIOR) INOP. REPLACED BAD BULB ON LEFT REAR AFT EMERGENCY LIGHT OVERWING. OPS CHECK GOOD.Jun 12, 2003 · N916SW · Cndair CL6002B19 · Emergency LightingSDR SWIA200312051Bulb · inoperativeEMERGENCY LIGHT INOP IN CEILING OF PAX CABIN. INSTALLED NEW BULB, OPS CHECK GOOD.May 26, 2003 · N916SW · Cndair CL6002B19 · Emergency LightingSDR SWIA200311885Bulb · burned outOVERHEAD EMERGENCY LIGHT IN CABIN (SECOND ONE) IS OUT. REMOVED AND REPLACED LIGHT BULB AS INDICATED PER MM 33-51-16. OPS CHECK GOOD.Apr 13, 2003 · N916SW · Cndair CL6002B19 · Emergency LightingSDR SWIA200211670Control Unit · malfunctionedFLAPS FAILED AT -0- WHEN SELECTED TO 8 DEGREES ON DESCENT. CLEARED FAULTS FROM FECU. CYCLED FLAPS SEVERAL TIMES. NO FAULTS FOUND. OPS CHECK GOOD.Dec 26, 2002 · N916SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA200211522Overheat Sensor · malfunctionedABORTED THE TAKEOFF DUE TO AN ''ANTI-ICE DUCT'' WARNING MESSAGE. THE SYNOPTIC PAGE WARNING WAS FOR THE RT WING LEADING EDGE. REPLACED ALL 21 RT WING OVERHEAT SENSORS IAW CRJ MM 30-12-12. OPS CHECK GOOD.Nov 24, 2002 · N916SW · Cndair CL6002B19 · Pneumatic Indicating SystemSDR SWIA200211469Fairing · damagedFLAPS FAIL AT ''0'' DURING APPROACH TO LANDING. REMOVED AND REPLACED LT INBOARD FLAP TO FUSELAGE FAIRING IAW SRM 51-71-00.Nov 11, 2002 · N916SW · Cndair CL6002B19 · Aerodynamic FairingsSDR SWIA200211420Actuator · malfunctionedYAW DAMPER NR 2 FAILED IN FLIGHT. MESSAGE ON EICAS. REMOVED AND REPLACED NR 2 YAW DAMP LINEAR ACTUATOR IAW CRJ MM 22-22-01. OPS CHECK GOOD.Nov 1, 2002 · N916SW · Cndair CL6002B19 · Autopilot SystemSDR SWIA200211190Ecu · malfunctionedAFTER STARTING ENGINES, NOTED FLT SPOILERS, GROUND SPOILERS, CAUTION MSGS & SPOILERONS. INSTALLED SERVICEABLE SECU. OPS CHECK GOOD.Sep 2, 2002 · N916SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200211079Proximity Sensor · dirtyDESCENDING THROUGH 12,000 FT, RECEIVED A RIGHT EMERGENCY DOOR CAUTION MESSAGE. CAUTION SELF CLEARED AT ABOUT 7000 FT (NO CABIN PRESSURE LOSS). CLEANED AND INSPECTED RIGHT EMERGENCY EXIT DOOR PROXIMITY SENSOR. RESECURED DOOR. OPS CHECK GOOD.Jul 27, 2002 · N916SW · Cndair CL6002B19 · Door Warning SystemSDR SWIA200211050Tire · blownAC RETURNED TO PHX DUE TO HIGH ENGINE VIBRATION ON LEFT ENGINE. VIBRATION CAUSED BY FOD INGESTION DURING GROUND OPERATION OR TAKEOFF. A LEFT MAIN TIRE BLEW ON ROTATION. ON LANDING THE OTHER LEFT MAIN TIRE FAILED. REPLACED BOTH LEFT MAIN WHEEL ASSYS IAW 32-Jul 16, 2002 · N916SW · Cndair CL6002B19 · Tire
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