N595SW, cancelled Nov 16, 2015

Service difficulty reports · 53

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 = 'N595SW' AND deregistration_id = 'N595SW-2015-11-16'
  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 COMA2010121350258Engine · vibrationON CLIMBOUT FROM DTW RECEIVED RIGHT ENGINE N2 AMBER VIB MSG. EMERGENCY DECLARED, A/C RETURNED TO DTW LANDED SAFELY. REMOVED AND REPLACED RIGHT ENGINE.Dec 9, 2010 · N595SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR COMA0860233Computer · failedFLIGHT 5624 - EN ROUTE TO CVG RECEIVED STALL FAIL CAUTION MESSAGE. FOLLOWED QRH, EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY IN CVG. REMOVED AND REPLACED STALL PROTECTION COMPUTER.Apr 27, 2008 · N595SW · Cndair CL6002B19 · Stall Warning SystemSDR COMA0860207Tube · crackedFLIGHT 5451 - EN ROUTE FROM YYZ TO CVG, NR 2 ENGINE LOW FUEL PRESSURE CAUTION MESSAGE. ENGINE REMAINED AT 56%, 70 DEG OIL TEMP, 50 PSI OIL PRESS, AND NO RESPONSE FROM THRUST LEVER. PERFORMED IFSD ON NR 2 ENGINE, EMERGENCY DECLARED AND A/C DIVERTED TO CMH ANDApr 2, 2008 · N595SW · Cndair CL6002B19 · Fuel Controlling SystemSDR COMA0760520Pin · damagedFLIGHT 5255 - OVERWING FLOOR EXIT LIGHTS (ORANGE BAR) ARE INOP. FOUND PIN ON ORANGE BAR DAMAGED. REMOVED DAMAGED STRIP AND INSTALLED SERVICEABLE STRIP.Aug 6, 2007 · N595SW · Cndair CL6002B19 · Emergency LightingSDR COMA0760304Panel · warpedYAW MOTION NOTED DURING CLIMB, AUTOPILOT ON AND OFF. RETURNED TO CMH. FOUND THE RIGHT LOWER VISOR PANEL BOWED OUT, REPLACED THE VISOR PANEL.Apr 8, 2007 · N595SW · Cndair CL6002B19 · Vertical Stabilizer, Plate/SkinSDR COMA0760296Wire Harness · faultyFLIGHT 5347 - UPON GEAR RETRACTION RECEIVED A GEAR DISAGREE MOMENTARILY BEFORE THE GEAR SHOWED UP AND LOCKED. REMOVED AND REPLACED NLG WOW NR 1 WIRE HARNESS.Mar 30, 2007 · N595SW · Cndair CL6002B19 · Landing Gear System WiringSDR COMA0760157Actuator · bindingFLIGHT 5075 - FLAP FAIL MESSAGE ON DESCENT, DECLARED EMERGENCY, ABORTED APPROACH, THEN LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RT OUTBOARD FLAP OUTBOARD ACTUATOR.Feb 5, 2007 · N595SW · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR COMA0760156Actuator · bindingFLIGHT 5075 - FLAP FAIL MESSAGE ON DESCENT, DECLARED EMERGENCY, ABORTED APPROACH, THEN LANDED WITHOUT INCIDENT. REMOVED AND REPLACED OUTBOARD FLAP INBOARD ACTUATOR.Feb 5, 2007 · N595SW · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR COMA0760155Actuator · bindingFLIGHT 5075 - FLAP FAIL MESSAGE ON DESCENT, DECLARED EMERGENCY, ABORTED APPROACH, THEN LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RIGHT INBOARD FLAP OUTBOARD ACTUATOR.Feb 5, 2007 · N595SW · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR COMA0760154Actuator · bindingFLIGHT 5075 - FLAP FAIL MESSAGE ON DESCENT, DECLARED EMERGENCY, ABORTED APPROACH, THEN LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RIGHT INBOARD FLAP INBOARD ACTUATOR.Feb 5, 2007 · N595SW · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR COMA0660617Valve · faultyFLIGHT 5027 - DURING CLIMB EN ROUTE LEX-ATL RECEIVED A STEERING INOPERATIVE MESSAGE, CREW DECLARED AN EMERGENCY AND DIVERTED TO CVG. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE ELECTRO-HYDRAULIC SERVO VALVE.Nov 4, 2006 · N595SW · Cndair CL6002B19 · Landing Gear Steering SystemSDR COMA0660415Uplock Sensor · out of adjustFLIGHT 5740 - AFTER TAKEOFF FROM PIT RECEIVED GEAR UP DISAGREE WARNING MESSAGE AND LEFT MAIN GEAR IN RED. PERFORMED QRH AND RETURNED TO PIT. LANDED WITHOUT INCIDENT. FOUND LEFT MAIN LANDING GEAR UPLOCK SENSOR OUT OF ADJUSTMENT. RE-ADJUSTED UP LOCK SENSOR.Jun 30, 2006 · N595SW · Cndair CL6002B19 · Landing Gear Position and WarningSDR COMA0660312Brake Cable · dirtyFLIGHT 5799 - DURING TAKEOFF ROLL, THE TAKEOFF CONFIGURATION OK ADVISORY MESSAGE WAS INTERMITTENT. CLEANED PARK BRAKE CABLE AND PERFORMED ENGINE RUNS AT TAKEOFF POWER, NO DISCREPANCIES NOTED.Apr 23, 2006 · N595SW · Cndair CL6002B19 · Landing Gear Brake SystemSDR COMA0660246Csd · warning lightFLIGHT 5209 - NR 1 GEN CAUTION MESSAGE ON TAKEOFF. SERVICED NR 1 GEN CSD.Mar 13, 2006 · N595SW · Cndair CL6002B19 · AC Generation SystemSDR COMA0660174Extinguisher · lowFLIGHT 5883 - DURING CLIMBOUT OF FSD RECEIVED A CARGO BOTTLE LOW CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT RETURNED TO THE FIELD. REPLACED THE CARGO BOTTLE FIRE EXTINGUISHER.Feb 21, 2006 · N595SW · Cndair CL6002B19 · Extinguishing SystemSDR COMA0660173Fire Bottle · lowFLIGHT 5883 - DURING CLIMBOUT OF FSD RECEIVED A CARGO BOTTLE LOW CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT RETURNED TO THE FIELD. REPLACED THE CARGO BOTTLE FIRE EXTINGUISHER.Feb 21, 2006 · N595SW · Cndair CL6002B19 · Fire Bottle, FixedSDR SWIA200616169Yoke · lack of lubeAILERON ROLL CONTROL VERY STIFF IN BOTH CAPTAIN'S AND FIRST OFFICER'S YOKE. CLEANED AND LUBED RT TRIM CENTERING AND FEEL MECHANISM, OPERATIONAL CHECKS GOOD REF CL600 MM 27-12-10.Jan 21, 2006 · N595SW · Cndair CL6002B19 · Control Column SectionSDR SWIA200515949Switch · inoperativeEMERGENCY LIGHT INDICATION PUSH SWITCH INOP. REPLACED EMERGENCY LIGHT INDICATOR PUSH SWITCH AS REQUIRED. OPERATIONAL CHECK GOOD.Dec 2, 2005 · N595SW · Cndair CL6002B19 · Emergency LightingSDR SWIA200516155Angle · crackedLEFT WHEEL WELL BAT ANGLE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED ANGLE DOUBLER PER REO 601R-57-51-046 STEP 5-8 REV B.Oct 22, 2005 · N595SW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR SWIA200516154Angle · crackedAFT PRESSURE BULKHEAD AFT SIDE; 2 ANGLES ARE CRACKED; 1 AT LBL40 AND 1 AT 4BL40 WL90 FS 625, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED LEFT HAND AFT PRESSURE BULKHEAD ANGLE PER 601R-35012 AND REO 601R-53-61-422. INSTALLED RIGHT HAND AFT PRESSURE BULKHEAD AOct 22, 2005 · N595SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA200515223Control Unit · malfunctionedFLT SPLRS AND OB GND SPLR FAULT STATUS MSG ON ED2 SELECTION TO FLAPS 8. REPLACED BOTH SECUS IAW MM 27-61-05, PN OFF 49164-06 SN 01562 AND SN 01544Jun 30, 2005 · N595SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200515174Control Handle · malfunctionedON APPROACH, FLAPS FAILED AT 20 DEGREES. REPLACED FLAP CONTROL HANDLE IAW CL 600 MM 27-51-01. OPERATIONAL CHECK GOOD.Jun 17, 2005 · N595SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA200515122Trim Switch · inoperativeSTAB CH 1WILL NOT MOVE STAB TRIM. REPLACED CAPTIANS STAB TRIM SWITCH ON YOKE, OPERATIONAL CHECK GOOD IAW 27-41-00.Jun 6, 2005 · N595SW · Cndair CL6002B19 · Stabilizer Control SystemSDR SWIA200514358Pcu · malfunctionedSPOILERONS FAULT MESSAGE. REPLACED RIGHT INBOARD AND OUTBOARD SPOILERON PCU IAW CRJ MM 27-62-01. OPERATIONAL CHECK GOOD. P/N 27000-7, S/N MAL-0989, S/N OFF 3287.Jan 7, 2005 · N595SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200414231Control Unit · malfunctionedSPOILERONS FAULT STATUS MESSAGE JUST AFTER TAKEOFF. REMOVE AND REPLACE NR 2 SECU IAW MM 27-61-05. OPERATIONAL CHECK GOOD.Dec 7, 2004 · N595SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200414164Light · brokenEMERGENCY EXIT FLOOD LIGHT BY PASSENGER DOOR BROKE. REMOVED AND REPLACED EMERGENCY EXIT FLOODLIGHT IAW MM 33-51-19, OPERATIONAL CHECK GOOD.Nov 22, 2004 · N595SW · Cndair CL6002B19 · Emergency LightingSDR SWIA200413854Actuator · malfunctionedDURING TAKEOFF FROM ABQ, AT AN ALTITUDE OF 450 FT AGL THE STAB TRIM AND MACH TRIM DISCONNECTED AS SOON AS THE FLAPS WERE MOVED FROM 20 DEGREES TO 8 DEGREES. REMOVED AND REPLACED HORIZONTAL STAB ACTUATOR, MCU AND STAB TRIM SWITCH IAW 27-46-00, 27-42-61, 27-42-Sep 23, 2004 · N595SW · Cndair CL6002B19 · Stabilizer Position IndicatingSDR SWIA200413570Clip · crackedINTERCOSTAL CLIP ON LEFT HAND SIDE AT FS 484 LBL 27 CRACKED. LOCATED UNDER FLOOR PANEL 261DLF. REMOVED CRACKED CLIP. INSTALLED NEW CLIP 601R31171-17 IAW CRJ 200 REO 601R-53-41-059.May 19, 2004 · N595SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200413569Angle · crackedRIGHT SIDE 625 OBLIQUE ANGLE CRACKED RBL 14. REMOVED AND INSTALLED A NEW OBLIQUE ANGLE P/N 600-35012-52 IAW CRJ 200 SRM 51-42-21.May 19, 2004 · N595SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200413568Clip · crackedINTERCOSTAL CLIP ON RT SIDE AT FS 484 RBL 29 CRACKED. LOCATED UNDER FLOOR PANEL 262DRF. REMOVED CRACKED CLIP, INSTALLED NEW CLIP 601R31171-9 IAW CRJ 200 REO 6501R-53-41-059.May 19, 2004 · N595SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200413123Trunnion · damagedHARD LANDING AFTER ILS APPROACH. AIRCRAFT BOUNCED AND, PRIOR TO SUBSEQUENT LANDING, THE LT WING TIP MADE CONTACT WITH RUNWAY.HARD OVERWEIGHT LANDING INSPECTION COMPLIED WITH IAW ST 12-407 ST 12-407. (AIRCRAFT CURRENTLY UNDERGOING LANDING GEAR REPLACEMENT) UJan 17, 2004 · N595SW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA200312718Trim Panel · damagedRUDDER TRIM SPORATIC TO LT SIDE, HARD TO USE. REMOVED AND REPLACED RUDDER/AILERON TRIM PANEL IAW CRJ MM 27-12-10. OPS. CHECK GOOD.Dec 23, 2003 · N595SW · Cndair CL6002B19 · Rudder Tab Control SystemSDR SWIA200312527Pcu · malfunctionedDURING DESCENT WITH FLIGHT SPOILERS DEPLOYED, STATUS MESSAGE FLT SPOILER FAULT APPEARED. REPLACED OUTBOARD RIGHT FLIGHT SPOILER PCU PER MM 27-62-01. SYS OPS CHECK AND LEAK CHECK OKAY.Oct 21, 2003 · N595SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200312462Seal · failedNOSE GEAR DID NOT RETRACT W/FOLLOWING MESSAGE: NOSE DOOR OPEN, GEAR DISAGREE, WOW INPUT, WOW OUTPUT, STEER INOPERATIVE. RETURNED TO CYVR. REMOVED AND REPLACED THE NLG LOWER BEARING TEE SEAL IAW MM 32-21-20. OPS AND LEAKS CHECKS GOOD.Sep 26, 2003 · N595SW · Cndair CL6002B19 · Nose/Tail Landing GearSDR SWIA200312195Axle · malfunctionedNOSE LANDING GEAR AXLE ASSY CORRODED. INSTALLED NEW AXLE ASSEMBLY IAW CRJ MM 32-21-15.Jul 16, 2003 · N595SW · Cndair CL6002B19 · Main Landing Gear Strut/Axle/TruckSDR SWIA200312037Line · leakingON A 10 MILE FINAL TO RUNWAY 26 - HYD 2B LOW PRESS MESSAGE APPEARED. HYD 2B RESERVOIR APPEARS TO BE EMPTY. REMOVED AND REPLACED HYDRAULIC LINE ON NR 2 HYDRAULIC SYSTEM SERVICE PORT IAW CL600 20-22-00. OPS CHECK GOOD. RESERVICED HYDRAULIC SYSTEM RESERVOIR IMay 25, 2003 · N595SW · Cndair CL6002B19 · Hydraulic System, MainSDR SWIA200311922Lever · failedFLAPS FAIL CAME ON FINAL, 7 MILES OUT. WHEN FLAPS WERE AT 20 DEGREES, SELECTED 30 DEGREES AND FLAPS FAIL MESSAGE ILLUMINATED. INTERROGATED FECU. FECU INDICATED FLAP HANDLE FAILURE. REMOVED AND REPLACED FLAP HANDLE. FLAPS OPS CHECK GOOD.Apr 28, 2003 · N595SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA200311849Bpsu · malfunctionedDURING APPROACH INTO SLC RECEIVED A FLAPS FAIL MESSAGE WITH FLAPS AT 20 DEGREES. RAN QRH PROCEDURE AND LANDED WITHOUT INCIDENT. FOUND LEFT BPSU TO BE JUMPY (TURNED SEVERAL TIMES WITH NO CHANGE IN POSITION). REMOVED AND REPLACED LEFT BPSU IAW 27-51-10 AND CHMar 22, 2003 · N595SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA200311766Control Unit · malfunctionedFLAPS FAIL CAUTION MESSAGE AFTER TAKEOFF. FLAPS WOULD NOT GO UP OR DOWN. RETURNED TO DFW. INSPECTED CANNON PLUGS AT SELECTOR LEVER. INSPECTED PINS AT FECU. INTERROGATED FECU, NO FAULTS FOUND. RESET SYSTEM. SYSTEM OPS CHECK GOOD IAW CL-600 MM 27-51-00. Jan 31, 2003 · N595SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA200211607Control Handle · malfunctionedFLAP FAIL MESSAGE AFTER LANDING WHEN RAISING FLAPS FROM 45 TO 30 DEGREES. REMOVED AND REPLACED FLAP CONTROL LEVER PER MM 27-51-01. OPS CHECKED GOOD. NO SKEWING OR DEFORMATION NOTED ON FLAPS.Dec 20, 2002 · N595SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA200211573Trim Switch · malfunctionedSHORTLY AFTER TAKEOFF, STAB TRIM DISENGAGED AND WOULD NOT REENGAGE (FLAPS & GEAR WERE UP). REPLACED COPILOT TRIM DISCONNECT SWITCH IAW MM 27-41-05. OPS CHECKS GOOD IAW MM 27-40-00 AND 27-41-00. SYSTEM OPS CHECKS GOOD.Dec 14, 2002 · N595SW · Cndair CL6002B19 · Stabilizer Control SystemSDR SWIA200211274Carbon Seal · leakingSMOKE IN COCKPIT IMMEDIATELTY AFTER TAKEOFF. MOSTLY COMING FROM CAPTAINS'S VENT. DONNED O2 MASKS. SMOKE LAV MESSAGE FOLLOWED. PERFORMED EMERGENCY PROCEDURE. FA NOTICED SMOKE IN CABIN AS WELL. NO FIRE IN LAVATORY. PERFORMED EVAC AT GATE. LOGGED OVERWEISep 29, 2002 · N595SW · Cndair CL6002B19 · Turbine Engine Oil SystemSDR SWIA200211273Seal · dirtyHIGH PITCHED WHINING NOISE REPORTED BY PASSENGERS AT ROW 7A&B. CLEANED DOOR SEAL AT LEFT OVER WING EXIT.Sep 29, 2002 · N595SW · Cndair CL6002B19 · Emergency ExitsSDR SWIA200211256Smoke Detector · failedCARGO BOTTLE TEST NR 2 INOP. NO RED LIGHTS ON THE TEST. REMOVED AND REPLACED AFT CARGO SMOKE DETECTOR WITH NEW SERVICEABLE DETECTOR IAW 26-15-00 CRJ MM. OPS CHECK GOOD.Sep 20, 2002 · N595SW · Cndair CL6002B19 · Smoke DetectionSDR SWIA200211320Angle · crackedFOUND INTERCOSTAL ATTACH ANGLE AT FS 484 RBL 27.00 CRACKED. FOUND DURING C CHECK INSPECTION. NEW ANGLE FITTED AND INSTALLED IAW REO 601R-53-41-059 REV ''A''.P/N: 601R31171-9.Aug 21, 2002 · N595SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200211319Angle · crackedFOUND ANGLES CRACKED AT FS 280.0 LBL AND RBL 90 INBOARD AND OUTBOARD. NEW ANGLES FIT AND INSTALLED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-42-21.Aug 21, 2002 · N595SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200211318Floor Support · crackedRIGHT AND LEFT FLOOR SUPPORT ANGLES AT FS 621.00 ARE CRACKED. FOUND DURING C-CHECK INSPECTION. REPAIRED DAMAGED ANGLES IAW CRJ REO 601R-53-61-117 REV A.Aug 21, 2002 · N595SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200211317Frame · crackedAT LEFT AND RIGHT FS 718.00 THE FRAME IS CRACKED AT THE PYLON FITTING. FOUND DURING C CHECK INSPECTION. REPAIRED CRACKED FRAME IAW CRJ REO 601R-53-61-193. ANGLE P/N: 600-36030-31, 2024T3-040.Aug 21, 2002 · N595SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200211123Control Unit · malfunctionedSTAB TRIM CH 2 WILL NOT ENGAGE. REPLACED HSTA AND MOTOR CONTROL UNIT. STAB TRIM OPS CHECKS GOOD.Aug 13, 2002 · N595SW · Cndair CL6002B19 · Stabilizer ActuatorSDR SWIA200210617Engine · vibratesNR 1 ENGINE FAN VIB IN YELLOW ARC SHORTLY AFTER TAKEOFF. ON ENGINE RUN UP, COULDN'T DUPLICATE PROBLEM. AT HIGH POWER SETTINGS, VIB NEVER GOT ABOVE .3. INSPECTED FAN BLADES VISUALLY AND INSPECTION GOOD.Jan 30, 2002 · N595SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
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