# Service difficulty reports: N595SW, cancelled Nov 16, 2015

A list on [N595SW, cancelled Nov 16, 2015](https://openairdocs.org/deregistered/N595SW-2015-11-16.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 53 reports

- [SDR COMA2010121350258](https://openairdocs.org/sdr/COMA2010121350258.md): Engine · vibration · Dec 9, 2010 · N595SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > ON CLIMBOUT FROM DTW RECEIVED RIGHT ENGINE N2 AMBER VIB MSG. EMERGENCY DECLARED, A/C RETURNED TO DTW LANDED SAFELY. REMOVED AND REPLACED RIGHT ENGINE.
- [SDR COMA0860233](https://openairdocs.org/sdr/COMA0860233.md): Computer · failed · Apr 27, 2008 · N595SW · Cndair CL6002B19 · Stall Warning System
  > FLIGHT 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.
- [SDR COMA0860207](https://openairdocs.org/sdr/COMA0860207.md): Tube · cracked · Apr 2, 2008 · N595SW · Cndair CL6002B19 · Fuel Controlling System
  > FLIGHT 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 AND
- [SDR COMA0760520](https://openairdocs.org/sdr/COMA0760520.md): Pin · damaged · Aug 6, 2007 · N595SW · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT 5255 - OVERWING FLOOR EXIT LIGHTS (ORANGE BAR) ARE INOP. FOUND PIN ON ORANGE BAR DAMAGED. REMOVED DAMAGED STRIP AND INSTALLED SERVICEABLE STRIP.
- [SDR COMA0760304](https://openairdocs.org/sdr/COMA0760304.md): Panel · warped · Apr 8, 2007 · N595SW · Cndair CL6002B19 · Vertical Stabilizer, Plate/Skin
  > YAW MOTION NOTED DURING CLIMB, AUTOPILOT ON AND OFF. RETURNED TO CMH. FOUND THE RIGHT LOWER VISOR PANEL BOWED OUT, REPLACED THE VISOR PANEL.
- [SDR COMA0760296](https://openairdocs.org/sdr/COMA0760296.md): Wire Harness · faulty · Mar 30, 2007 · N595SW · Cndair CL6002B19 · Landing Gear System Wiring
  > FLIGHT 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.
- [SDR COMA0760157](https://openairdocs.org/sdr/COMA0760157.md): Actuator · binding · Feb 5, 2007 · N595SW · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLIGHT 5075 - FLAP FAIL MESSAGE ON DESCENT, DECLARED EMERGENCY, ABORTED APPROACH, THEN LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RT OUTBOARD FLAP OUTBOARD ACTUATOR.
- [SDR COMA0760156](https://openairdocs.org/sdr/COMA0760156.md): Actuator · binding · Feb 5, 2007 · N595SW · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLIGHT 5075 - FLAP FAIL MESSAGE ON DESCENT, DECLARED EMERGENCY, ABORTED APPROACH, THEN LANDED WITHOUT INCIDENT. REMOVED AND REPLACED OUTBOARD FLAP INBOARD ACTUATOR.
- [SDR COMA0760155](https://openairdocs.org/sdr/COMA0760155.md): Actuator · binding · Feb 5, 2007 · N595SW · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLIGHT 5075 - FLAP FAIL MESSAGE ON DESCENT, DECLARED EMERGENCY, ABORTED APPROACH, THEN LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RIGHT INBOARD FLAP OUTBOARD ACTUATOR.
- [SDR COMA0760154](https://openairdocs.org/sdr/COMA0760154.md): Actuator · binding · Feb 5, 2007 · N595SW · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLIGHT 5075 - FLAP FAIL MESSAGE ON DESCENT, DECLARED EMERGENCY, ABORTED APPROACH, THEN LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RIGHT INBOARD FLAP INBOARD ACTUATOR.
- [SDR COMA0660617](https://openairdocs.org/sdr/COMA0660617.md): Valve · faulty · Nov 4, 2006 · N595SW · Cndair CL6002B19 · Landing Gear Steering System
  > FLIGHT 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.
- [SDR COMA0660415](https://openairdocs.org/sdr/COMA0660415.md): Uplock Sensor · out of adjust · Jun 30, 2006 · N595SW · Cndair CL6002B19 · Landing Gear Position and Warning
  > FLIGHT 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.
- [SDR COMA0660312](https://openairdocs.org/sdr/COMA0660312.md): Brake Cable · dirty · Apr 23, 2006 · N595SW · Cndair CL6002B19 · Landing Gear Brake System
  > FLIGHT 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.
- [SDR COMA0660246](https://openairdocs.org/sdr/COMA0660246.md): Csd · warning light · Mar 13, 2006 · N595SW · Cndair CL6002B19 · AC Generation System
  > FLIGHT 5209 - NR 1 GEN CAUTION MESSAGE ON TAKEOFF. SERVICED NR 1 GEN CSD.
- [SDR COMA0660174](https://openairdocs.org/sdr/COMA0660174.md): Extinguisher · low · Feb 21, 2006 · N595SW · Cndair CL6002B19 · Extinguishing System
  > FLIGHT 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.
- [SDR COMA0660173](https://openairdocs.org/sdr/COMA0660173.md): Fire Bottle · low · Feb 21, 2006 · N595SW · Cndair CL6002B19 · Fire Bottle, Fixed
  > FLIGHT 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.
- [SDR SWIA200616169](https://openairdocs.org/sdr/SWIA200616169.md): Yoke · lack of lube · Jan 21, 2006 · N595SW · Cndair CL6002B19 · Control Column Section
  > AILERON 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.
- [SDR SWIA200515949](https://openairdocs.org/sdr/SWIA200515949.md): Switch · inoperative · Dec 2, 2005 · N595SW · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT INDICATION PUSH SWITCH INOP. REPLACED EMERGENCY LIGHT INDICATOR PUSH SWITCH AS REQUIRED. OPERATIONAL CHECK GOOD.
- [SDR SWIA200516155](https://openairdocs.org/sdr/SWIA200516155.md): Angle · cracked · Oct 22, 2005 · N595SW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > LEFT 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.
- [SDR SWIA200516154](https://openairdocs.org/sdr/SWIA200516154.md): Angle · cracked · Oct 22, 2005 · N595SW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT 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 A
- [SDR SWIA200515223](https://openairdocs.org/sdr/SWIA200515223.md): Control Unit · malfunctioned · Jun 30, 2005 · N595SW · Cndair CL6002B19 · Drag Control System
  > FLT 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 01544
- [SDR SWIA200515174](https://openairdocs.org/sdr/SWIA200515174.md): Control Handle · malfunctioned · Jun 17, 2005 · N595SW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > ON APPROACH, FLAPS FAILED AT 20 DEGREES. REPLACED FLAP CONTROL HANDLE IAW CL 600 MM 27-51-01. OPERATIONAL CHECK GOOD.
- [SDR SWIA200515122](https://openairdocs.org/sdr/SWIA200515122.md): Trim Switch · inoperative · Jun 6, 2005 · N595SW · Cndair CL6002B19 · Stabilizer Control System
  > STAB CH 1WILL NOT MOVE STAB TRIM. REPLACED CAPTIANS STAB TRIM SWITCH ON YOKE, OPERATIONAL CHECK GOOD IAW 27-41-00.
- [SDR SWIA200514358](https://openairdocs.org/sdr/SWIA200514358.md): Pcu · malfunctioned · Jan 7, 2005 · N595SW · Cndair CL6002B19 · Drag Control System
  > SPOILERONS 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.
- [SDR SWIA200414231](https://openairdocs.org/sdr/SWIA200414231.md): Control Unit · malfunctioned · Dec 7, 2004 · N595SW · Cndair CL6002B19 · Drag Control System
  > SPOILERONS FAULT STATUS MESSAGE JUST AFTER TAKEOFF. REMOVE AND REPLACE NR 2 SECU IAW MM 27-61-05. OPERATIONAL CHECK GOOD.
- [SDR SWIA200414164](https://openairdocs.org/sdr/SWIA200414164.md): Light · broken · Nov 22, 2004 · N595SW · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY EXIT FLOOD LIGHT BY PASSENGER DOOR BROKE. REMOVED AND REPLACED EMERGENCY EXIT FLOODLIGHT IAW MM 33-51-19, OPERATIONAL CHECK GOOD.
- [SDR SWIA200413854](https://openairdocs.org/sdr/SWIA200413854.md): Actuator · malfunctioned · Sep 23, 2004 · N595SW · Cndair CL6002B19 · Stabilizer Position Indicating
  > DURING 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-
- [SDR SWIA200413570](https://openairdocs.org/sdr/SWIA200413570.md): Clip · cracked · May 19, 2004 · N595SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL 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.
- [SDR SWIA200413569](https://openairdocs.org/sdr/SWIA200413569.md): Angle · cracked · May 19, 2004 · N595SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT 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.
- [SDR SWIA200413568](https://openairdocs.org/sdr/SWIA200413568.md): Clip · cracked · May 19, 2004 · N595SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL 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.
- [SDR SWIA200413123](https://openairdocs.org/sdr/SWIA200413123.md): Trunnion · damaged · Jan 17, 2004 · N595SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > HARD 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) U
- [SDR SWIA200312718](https://openairdocs.org/sdr/SWIA200312718.md): Trim Panel · damaged · Dec 23, 2003 · N595SW · Cndair CL6002B19 · Rudder Tab Control System
  > RUDDER TRIM SPORATIC TO LT SIDE, HARD TO USE. REMOVED AND REPLACED RUDDER/AILERON TRIM PANEL IAW CRJ MM 27-12-10. OPS. CHECK GOOD.
- [SDR SWIA200312527](https://openairdocs.org/sdr/SWIA200312527.md): Pcu · malfunctioned · Oct 21, 2003 · N595SW · Cndair CL6002B19 · Drag Control System
  > DURING 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.
- [SDR SWIA200312462](https://openairdocs.org/sdr/SWIA200312462.md): Seal · failed · Sep 26, 2003 · N595SW · Cndair CL6002B19 · Nose/Tail Landing Gear
  > NOSE 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.
- [SDR SWIA200312195](https://openairdocs.org/sdr/SWIA200312195.md): Axle · malfunctioned · Jul 16, 2003 · N595SW · Cndair CL6002B19 · Main Landing Gear Strut/Axle/Truck
  > NOSE LANDING GEAR AXLE ASSY CORRODED. INSTALLED NEW AXLE ASSEMBLY IAW CRJ MM 32-21-15.
- [SDR SWIA200312037](https://openairdocs.org/sdr/SWIA200312037.md): Line · leaking · May 25, 2003 · N595SW · Cndair CL6002B19 · Hydraulic System, Main
  > ON 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 I
- [SDR SWIA200311922](https://openairdocs.org/sdr/SWIA200311922.md): Lever · failed · Apr 28, 2003 · N595SW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS 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.
- [SDR SWIA200311849](https://openairdocs.org/sdr/SWIA200311849.md): Bpsu · malfunctioned · Mar 22, 2003 · N595SW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > DURING 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 CH
- [SDR SWIA200311766](https://openairdocs.org/sdr/SWIA200311766.md): Control Unit · malfunctioned · Jan 31, 2003 · N595SW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS 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.
- [SDR SWIA200211607](https://openairdocs.org/sdr/SWIA200211607.md): Control Handle · malfunctioned · Dec 20, 2002 · N595SW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP 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.
- [SDR SWIA200211573](https://openairdocs.org/sdr/SWIA200211573.md): Trim Switch · malfunctioned · Dec 14, 2002 · N595SW · Cndair CL6002B19 · Stabilizer Control System
  > SHORTLY 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.
- [SDR SWIA200211274](https://openairdocs.org/sdr/SWIA200211274.md): Carbon Seal · leaking · Sep 29, 2002 · N595SW · Cndair CL6002B19 · Turbine Engine Oil System
  > SMOKE 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 OVERWEI
- [SDR SWIA200211273](https://openairdocs.org/sdr/SWIA200211273.md): Seal · dirty · Sep 29, 2002 · N595SW · Cndair CL6002B19 · Emergency Exits
  > HIGH PITCHED WHINING NOISE REPORTED BY PASSENGERS AT ROW 7A&B. CLEANED DOOR SEAL AT LEFT OVER WING EXIT.
- [SDR SWIA200211256](https://openairdocs.org/sdr/SWIA200211256.md): Smoke Detector · failed · Sep 20, 2002 · N595SW · Cndair CL6002B19 · Smoke Detection
  > CARGO 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.
- [SDR SWIA200211320](https://openairdocs.org/sdr/SWIA200211320.md): Angle · cracked · Aug 21, 2002 · N595SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND 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.
- [SDR SWIA200211319](https://openairdocs.org/sdr/SWIA200211319.md): Angle · cracked · Aug 21, 2002 · N595SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND 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.
- [SDR SWIA200211318](https://openairdocs.org/sdr/SWIA200211318.md): Floor Support · cracked · Aug 21, 2002 · N595SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT 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.
- [SDR SWIA200211317](https://openairdocs.org/sdr/SWIA200211317.md): Frame · cracked · Aug 21, 2002 · N595SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > AT 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.
- [SDR SWIA200211123](https://openairdocs.org/sdr/SWIA200211123.md): Control Unit · malfunctioned · Aug 13, 2002 · N595SW · Cndair CL6002B19 · Stabilizer Actuator
  > STAB TRIM CH 2 WILL NOT ENGAGE. REPLACED HSTA AND MOTOR CONTROL UNIT. STAB TRIM OPS CHECKS GOOD.
- [SDR SWIA200210617](https://openairdocs.org/sdr/SWIA200210617.md): Engine · vibrates · Jan 30, 2002 · N595SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > NR 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.

Next page: https://openairdocs.org/deregistered/N595SW-2015-11-16/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/deregistered/N595SW-2015-11-16/reports

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