# N595SW: 1999 Bombardier CL-600-2B19, registration cancelled 2015-11-16

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 16, 2015
- Exported to: South Africa
- Status when cancelled: Valid registration
- Airframe: [Bombardier CL-600-2B19](https://openairdocs.org/model/bombardier-cl-600-2b19) (registry code 1390008)
- Engine: [GE CF34 series](https://openairdocs.org/engine/ge-cf34-series) (registry code 30015)
- Data sheets: [TCDS A21EA-1](https://openairdocs.org/tcds/A21EA-1) (OpenAirDocs)
- Serial number: 7292
- Year built: 1999
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 12, 1999
- Certificate issued: August 8, 2014
- Last registry action: August 8, 2014
- Mode S code: A7B19F
- Owner when cancelled: [Golden Mile Aircraft Leasing Inc](https://openairdocs.org/faa-owner/GOLDEN%20MILE%20AIRCRAFT%20LEASING%20INC)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.7236° N, 75.5412° W: Placed by OpenAirDocs at the center of ZIP code 19801, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N595SW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=595SW
- Page: https://openairdocs.org/deregistered/N595SW-2015-11-16

From the FAA registry file of October 28, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Bombardier CL-600-2B19: https://openairdocs.org/model/bombardier-cl-600-2b19.md

## Service difficulty reports (53, newest 50)

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

- [SDR COMA2010121350258](https://openairdocs.org/sdr/COMA2010121350258), Dec 9, 2010: ENGINE. VIBRATION. 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), Apr 27, 2008: COMPUTER. FAILED. FLIGHT 5624 - EN ROUTE TO CVG RECEIVED STALL FAIL CAUTION MESSAGE. FOLLOWED QRH, EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY IN CVG. REMOVED AND REPLACED STALL P
- [SDR COMA0860207](https://openairdocs.org/sdr/COMA0860207), Apr 2, 2008: TUBE. CRACKED. 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 RESPONS
- [SDR COMA0760520](https://openairdocs.org/sdr/COMA0760520), Aug 6, 2007: PIN. DAMAGED. 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), Apr 8, 2007: PANEL. WARPED. 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), Mar 30, 2007: WIRE HARNESS. FAULTY. 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), Feb 5, 2007: ACTUATOR. BINDING. FLIGHT 5075 - FLAP FAIL MESSAGE ON DESCENT, DECLARED EMERGENCY, ABORTED APPROACH, THEN LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RT OUTBOARD FLAP OUTBOARD A
- [SDR COMA0760156](https://openairdocs.org/sdr/COMA0760156), Feb 5, 2007: ACTUATOR. BINDING. FLIGHT 5075 - FLAP FAIL MESSAGE ON DESCENT, DECLARED EMERGENCY, ABORTED APPROACH, THEN LANDED WITHOUT INCIDENT. REMOVED AND REPLACED OUTBOARD FLAP INBOARD ACTUA
- [SDR COMA0760155](https://openairdocs.org/sdr/COMA0760155), Feb 5, 2007: ACTUATOR. BINDING. FLIGHT 5075 - FLAP FAIL MESSAGE ON DESCENT, DECLARED EMERGENCY, ABORTED APPROACH, THEN LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RIGHT INBOARD FLAP OUTBOARD
- [SDR COMA0760154](https://openairdocs.org/sdr/COMA0760154), Feb 5, 2007: ACTUATOR. BINDING. FLIGHT 5075 - FLAP FAIL MESSAGE ON DESCENT, DECLARED EMERGENCY, ABORTED APPROACH, THEN LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RIGHT INBOARD FLAP INBOARD 
- [SDR COMA0660617](https://openairdocs.org/sdr/COMA0660617), Nov 4, 2006: VALVE. FAULTY. FLIGHT 5027 - DURING CLIMB EN ROUTE LEX-ATL RECEIVED A STEERING INOPERATIVE MESSAGE, CREW DECLARED AN EMERGENCY AND DIVERTED TO CVG. FLIGHT LANDED WITHOUT INCID
- [SDR COMA0660415](https://openairdocs.org/sdr/COMA0660415), Jun 30, 2006: UPLOCK SENSOR. OUT OF ADJUST. 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 INCI
- [SDR COMA0660312](https://openairdocs.org/sdr/COMA0660312), Apr 23, 2006: BRAKE CABLE. DIRTY. FLIGHT 5799 - DURING TAKEOFF ROLL, THE TAKEOFF CONFIGURATION OK ADVISORY MESSAGE WAS INTERMITTENT. CLEANED PARK BRAKE CABLE AND PERFORMED ENGINE RUNS AT TAKEOFF
- [SDR COMA0660246](https://openairdocs.org/sdr/COMA0660246), Mar 13, 2006: CSD. WARNING LIGHT. FLIGHT 5209 - NR 1 GEN CAUTION MESSAGE ON TAKEOFF. SERVICED NR 1 GEN CSD.
- [SDR COMA0660174](https://openairdocs.org/sdr/COMA0660174), Feb 21, 2006: EXTINGUISHER. LOW. 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 CARG
- [SDR COMA0660173](https://openairdocs.org/sdr/COMA0660173), Feb 21, 2006: FIRE BOTTLE. LOW. 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 CARG
- [SDR SWIA200616169](https://openairdocs.org/sdr/SWIA200616169), Jan 21, 2006: YOKE. LACK OF LUBE. 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 
- [SDR SWIA200515949](https://openairdocs.org/sdr/SWIA200515949), Dec 2, 2005: SWITCH. INOPERATIVE. EMERGENCY LIGHT INDICATION PUSH SWITCH INOP. REPLACED EMERGENCY LIGHT INDICATOR PUSH SWITCH AS REQUIRED. OPERATIONAL CHECK GOOD.
- [SDR SWIA200516155](https://openairdocs.org/sdr/SWIA200516155), Oct 22, 2005: ANGLE. CRACKED. 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), Oct 22, 2005: ANGLE. CRACKED. 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 
- [SDR SWIA200515223](https://openairdocs.org/sdr/SWIA200515223), Jun 30, 2005: CONTROL UNIT. MALFUNCTIONED. 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), Jun 17, 2005: CONTROL HANDLE. MALFUNCTIONED. 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), Jun 6, 2005: TRIM SWITCH. INOPERATIVE. 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), Jan 7, 2005: PCU. MALFUNCTIONED. 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), Dec 7, 2004: CONTROL UNIT. MALFUNCTIONED. 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), Nov 22, 2004: LIGHT. BROKEN. 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), Sep 23, 2004: ACTUATOR. MALFUNCTIONED. 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. REM
- [SDR SWIA200413570](https://openairdocs.org/sdr/SWIA200413570), May 19, 2004: CLIP. CRACKED. 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
- [SDR SWIA200413569](https://openairdocs.org/sdr/SWIA200413569), May 19, 2004: ANGLE. CRACKED. 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), May 19, 2004: CLIP. CRACKED. 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 650
- [SDR SWIA200413123](https://openairdocs.org/sdr/SWIA200413123), Jan 17, 2004: TRUNNION. DAMAGED. HARD LANDING AFTER ILS APPROACH. AIRCRAFT BOUNCED AND, PRIOR TO SUBSEQUENT LANDING, THE LT WING TIP MADE CONTACT WITH RUNWAY.HARD OVERWEIGHT LANDING INSPECTION 
- [SDR SWIA200312718](https://openairdocs.org/sdr/SWIA200312718), Dec 23, 2003: TRIM PANEL. DAMAGED. 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), Oct 21, 2003: PCU. MALFUNCTIONED. 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 CHE
- [SDR SWIA200312462](https://openairdocs.org/sdr/SWIA200312462), Sep 26, 2003: SEAL. FAILED. 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 T
- [SDR SWIA200312195](https://openairdocs.org/sdr/SWIA200312195), Jul 16, 2003: AXLE. MALFUNCTIONED. NOSE LANDING GEAR AXLE ASSY CORRODED. INSTALLED NEW AXLE ASSEMBLY IAW CRJ MM 32-21-15.
- [SDR SWIA200312037](https://openairdocs.org/sdr/SWIA200312037), May 25, 2003: LINE. LEAKING. 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
- [SDR SWIA200311922](https://openairdocs.org/sdr/SWIA200311922), Apr 28, 2003: LEVER. FAILED. 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 
- [SDR SWIA200311849](https://openairdocs.org/sdr/SWIA200311849), Mar 22, 2003: BPSU. MALFUNCTIONED. 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 (TUR
- [SDR SWIA200311766](https://openairdocs.org/sdr/SWIA200311766), Jan 31, 2003: CONTROL UNIT. MALFUNCTIONED. 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. INTE
- [SDR SWIA200211607](https://openairdocs.org/sdr/SWIA200211607), Dec 20, 2002: CONTROL HANDLE. MALFUNCTIONED. 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 
- [SDR SWIA200211573](https://openairdocs.org/sdr/SWIA200211573), Dec 14, 2002: TRIM SWITCH. MALFUNCTIONED. 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 G
- [SDR SWIA200211274](https://openairdocs.org/sdr/SWIA200211274), Sep 29, 2002: CARBON SEAL. LEAKING. SMOKE IN COCKPIT IMMEDIATELTY AFTER TAKEOFF. MOSTLY COMING FROM CAPTAINS'S VENT. DONNED O2 MASKS. SMOKE LAV MESSAGE FOLLOWED. PERFORMED EMERGENCY PROCEDURE. FA 
- [SDR SWIA200211273](https://openairdocs.org/sdr/SWIA200211273), Sep 29, 2002: SEAL. DIRTY. 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), Sep 20, 2002: SMOKE DETECTOR. FAILED. 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 CHE
- [SDR SWIA200211320](https://openairdocs.org/sdr/SWIA200211320), Aug 21, 2002: ANGLE. CRACKED. 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
- [SDR SWIA200211319](https://openairdocs.org/sdr/SWIA200211319), Aug 21, 2002: ANGLE. CRACKED. 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), Aug 21, 2002: FLOOR SUPPORT. CRACKED. 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), Aug 21, 2002: FRAME. CRACKED. 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
- [SDR SWIA200211123](https://openairdocs.org/sdr/SWIA200211123), Aug 13, 2002: CONTROL UNIT. MALFUNCTIONED. 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), Jan 30, 2002: ENGINE. VIBRATES. 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

All 53: https://openairdocs.org/deregistered/N595SW-2015-11-16/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB CHI04IA056](https://openairdocs.org/ntsb/CHI04IA056), Jan 18, 2004: Bombardier CL-600-2B19 (N595SW), Rapid City, SD, incident, minor damage. Probable cause: The copilot's failure to maintain control of the airplane during the landing and the captain's delay in initiating remedial action. Factors contributing to the accident were the low ceiling and low…

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20040117002589I](https://openairdocs.org/incident/20040117002589I), Jan 17, 2004: Cndair CL6002B19 (N595SW), Rapid City, SD, Minor damage. (-23) Ellsworth app gave sky west flt 3855 the wx - indefinite ceiling at one hundred, vis one quarter mile and freezing fog at 04:54 zulu. Flt 3855 entered…

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