# N597SW: 1999 Bombardier CL-600-2B19, registration cancelled 2015-05-15

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 15, 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: 7293
- Year built: 1999
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 25, 1999
- Certificate issued: August 8, 2014
- Last registry action: August 8, 2014
- Mode S code: A7B90D
- 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/N597SW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=597SW
- Page: https://openairdocs.org/deregistered/N597SW-2015-05-15

From the FAA registry file of October 29, 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 (80, newest 50)

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

- [SDR COMA2010032950070](https://openairdocs.org/sdr/COMA2010032950070), Mar 25, 2010: BUSHING. MIGRATED. RIGHT WING-TO-FUSELAGE ATTACH FITTING BUSHINGS MIGRATING AT FS 424.00. REMOVED AND REPLACED BUSHINGS IAW EO 57-021.
- [SDR COMA2010032950069](https://openairdocs.org/sdr/COMA2010032950069), Mar 25, 2010: BUSHING. MIGRATED. LEFT WING-TO-FUSELAGE ATTACH FITTING BUSHINGS MIGRATING AT FS 424.00. REMOVED AND REPLACED BUSHINGS IAW EO 57-021.
- [SDR COMA2010031650062](https://openairdocs.org/sdr/COMA2010031650062), Mar 16, 2010: BULKHEAD. CRACKED. FORWARD PRESSURE BULKHEAD CRACKED AROUND THE PARKING BRAKE CUTOUT, FS 202.75, LBL 23.71. CUT OUT DAMAGE AREA AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-11-563
- [SDR COMA2009082750191](https://openairdocs.org/sdr/COMA2009082750191), Aug 26, 2009: TARGET. LOOSE. ON CLIMBOUT FROM IND RECEIVED GEAR DISAGREE MSG, RT MLG INDICATED UNSAFE. FOLLOWED QRH, EMERGENCY DECLARED, A/C RETURNED TO IND LANDED SAFELY. INSPECTED A/C FOU
- [SDR COMA2009040750110](https://openairdocs.org/sdr/COMA2009040750110), Apr 3, 2009: INVERTER. INOPERATIVE. EMERGENCY EXIT LIGHT ADJACENT TO LEFT OVERWING EXIT SIGN INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT INVERTER.
- [SDR COMA2009032020100](https://openairdocs.org/sdr/COMA2009032020100), Mar 20, 2009: SKIN. CRACKED. DURING EDDY CURRENT INSPECTION OF THE AFT PRESSURE BULKHEAD FS 621.00, FOUND A CRACK ON SKIN AT LBL 27.50 ABOVE THE TOP OF CARGO DOOR TRACK. REMOVED DAMAGE AT F
- [SDR COMA2009032050099](https://openairdocs.org/sdr/COMA2009032050099), Mar 20, 2009: SKIN. CRACKED. DURING EDDY CURRENT INSPECTION OF THE AFT PRESSURE BULKHEAD FS 621.00, FOUND A CRACK ON SKIN AT CARGO DOOR TRACK / LINTEL ATTACHMENT FITTING AT WL 108.00. REMOV
- [SDR COMA2008120850022](https://openairdocs.org/sdr/COMA2008120850022), Dec 7, 2008: SECU. MALFUNCTIONED. ON APPROACH INTO CVG, RECEIVED GND SPOILER DEPLOY, FLT SPOILERS AND SPOILERONS CAUTION MSG'S. EMERGENCY DECLARED, A/C LANDED SAFELY. RESET SECU'S, OPS CHECK OF 
- [SDR COMA0860228](https://openairdocs.org/sdr/COMA0860228), Apr 17, 2008: SELECTOR VALVE. INTERMITTENT. FLIGHT 5662 - ON FINAL APPROACH INTO CVG SELECTED GEAR DOWN AND RECEIVED GEAR DISAGREE WARNING FOR THE NOSE LANDING GEAR. EMERGENCY DECLARED, RAN QRH, CYCLE GEA
- [SDR COMA0860208](https://openairdocs.org/sdr/COMA0860208), Apr 4, 2008: LIGHT. INOPERATIVE. CABIN ROW 2 EMERGENCY CEILING LIGHT FAILED TO ILLUMINATE. DEFERRED PER MEL 33-51-01-2.
- [SDR COMA0860202](https://openairdocs.org/sdr/COMA0860202), Mar 31, 2008: BPSU. FAULTY. FLIGHT 5450 - AT LEVEL OFF FROM CLIMB AT 260 KTS, HIGH SPEED CLACKER SOUNDED FOLLOWED SHORTLY BY FLAPS FAIL CAUTION MESSAGE. FLAPS WERE AT 0 DEGREES. EMERGENCY 
- [SDR COMA0860200](https://openairdocs.org/sdr/COMA0860200), Mar 30, 2008: ECU. FAULTY. FLIGHT 5301 - DURING DESCENT THROUGH 17,800FT AT 280 KTS INTO SRQ, RECEIVED FLAPS HALF SPEED MESSAGE FOLLOWED BY FLAPS FAIL CAUTION MESSAGE. FLAPS WERE AT 0 DEG
- [SDR COMA0860201](https://openairdocs.org/sdr/COMA0860201), Mar 29, 2008: FLAP. FAILED. FLIGHT 5301 - DURING DESCENT THROUGH 17,800FT AT 280 KTS INTO SRQ, RECEIVED FLAPS HALF SPEED MESSAGE FOLLOWED BY FLAPS FAIL CAUTION MESSAGE. FLAPS WERE AT 0 DEG
- [SDR COMA0860181](https://openairdocs.org/sdr/COMA0860181), Mar 19, 2008: WARNING SYSTEM. MALFUNCTIONED. FLIGHT 5539- RECEIVED APU OIL TEMP CAUTION MESSAGE. DECLARED EMERGENCY, DIVERTED TO CRW, LANDED WITHOUT INCIDENT. CHECKED APU OIL LEVEL AND PERFORMED OPS CHECK 
- [SDR COMA0760568](https://openairdocs.org/sdr/COMA0760568), Sep 13, 2007: HYDRAULIC LINE. LEAKING. FLIGHT 9456 - RECEIVED -HYD 2 LOW PRESS- CAUTION. HYD 2 QTY IS 0%. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED LEAKING HYDRAULIC LINE. NO FURTHER DEFE
- [SDR COMA0760504](https://openairdocs.org/sdr/COMA0760504), Jul 30, 2007: LIGHT. INOPERATIVE. FLIGHT 5460 - LOWER GREEN EMERGENCY EXIT LIGHT BY MAIN PAX DOOR INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT.
- [SDR COMA0760379](https://openairdocs.org/sdr/COMA0760379), May 16, 2007: PROXIMITY SWITCH. FAULTY. FLIGHT 5454 - DURING CLIMBOUT OF CVG RECEIVED A CABIN DOOR HANDLE MESSAGE, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. FLIGHT LANDED WITHOUT INCIDENT.
- [SDR COMA0760362](https://openairdocs.org/sdr/COMA0760362), May 4, 2007: RESTRICTOR VALVE. DEFECTIVE. FLIGHT 5542 - RECEIVED CABIN ALT CAUTION. CABIN PRESS RISING SLOWLY BUT STEADILY THROUGH 8000 FT. PERFORMED QRH, EMERGENCY DESCENT TO 10000. CABIN PRESS STABILI
- [SDR COMA0760361](https://openairdocs.org/sdr/COMA0760361), May 4, 2007: DRAIN LINE. DEFECTIVE. FLIGHT 5542 - RECEIVED CABIN ALT CAUTION. CABIN PRESS RISING SLOWLY BUT STEADILY THROUGH 8000 FT. PERFORMED QRH, EMERGENCY DESCENT TO 10000. CABIN PRESS STABILI
- [SDR COMA0760265](https://openairdocs.org/sdr/COMA0760265), Mar 18, 2007: DOOR. UNKNOWN. FLIGHT 5549 - PASSENGER DOOR OUTER HANDLE CAUTION MESSAGE, FOLLOWED BY A PAX DOOR WARNING MESSAGE. AIRCRAFT RETURNED BACK TO BWI AND LANDED SAFELY. DEFERRED PER
- [SDR COMA0760197](https://openairdocs.org/sdr/COMA0760197), Feb 19, 2007: CABLE. BROKEN. WHILE PERFORMING TASK CARD CRJ-2-448001, RIGHT NACELLE INSP, FOUND THE ATR CABLE TO BE BROKEN AT THE TURNBUCKLE END IN THE PYLON, MAKING THE ATR SYSTEM INOP. RE
- [SDR COMA0660438](https://openairdocs.org/sdr/COMA0660438), Jul 13, 2006: LIGHT. INOPERATIVE. FLIGHT 5188 - OVERHEAD EMERGENCY LIGHT AT ROW 12 INOPERABLE. TRANSFERRED TO DEFERRED LIST PER MEL 33-51-10-1.
- [SDR COMA0660361](https://openairdocs.org/sdr/COMA0660361), May 26, 2006: BPSU. FAULTY. FLIGHT 5489 - EN ROUTE RDU - JFK RECEIVED A FLAP FAIL CAUTION MESSAGE AT ZERO DEGREES. FLIGHT RETURNED TO THE FIELD. REPLACED THE RIGHT BRAKE POSITION SENSING U
- [SDR COMA0660360](https://openairdocs.org/sdr/COMA0660360), May 26, 2006: FLAP. MALFUNCTIONED. FLIGHT 5047 - FLAP FAIL CAUTION MESSAGE EN ROUTE TO RDU. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION PARAGRAPH (B) 1, 2, 3, 
- [SDR COMA0660298](https://openairdocs.org/sdr/COMA0660298), Apr 10, 2006: FLAP SYSTEM. MALFUNCTIONED. FLIGHT 5745 - FLAPS FAILED CAUTION MESSAGE DURING TAXI OUT. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (B) 1, 2,
- [SDR SWIA200516157](https://openairdocs.org/sdr/SWIA200516157), Nov 5, 2005: CLIP. CRACKED. CLIP ON LT SIDE FS625 CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED FS 625 LT CLIP IAW CRJ200 SRM 51-24-16 PG 1-7 51-42-06 PG 1-18.
- [SDR SWIA200516156](https://openairdocs.org/sdr/SWIA200516156), Nov 5, 2005: FLOORBEAM. CRACKED. AFT FLOOR ANGLE CRACKED FS 280 LBL 11, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED ANGLE PER REO 601R-53-11-138 AND SRM CRJ200 51-31-06 PG 1 PARA 3 PG 3.
- [SDR SWIA200515687](https://openairdocs.org/sdr/SWIA200515687), Oct 9, 2005: LAMP. BURNED OUT. EMERGENCY OVERHEAD LIGHT INOP 2ND BACK FROM FRONT. REPLACED LAMP. OPERATIONAL CHECK GOOD.
- [SDR SWIA200515565](https://openairdocs.org/sdr/SWIA200515565), Sep 18, 2005: OXYGEN MASK. DEPLOYED. PASSENGER O2 MASKS DEPLOYED WHILE SETTING FIELD ELEVATION FROM 3860' TO 4220'. REINSTALLED MASKS AND ALL DOORS RESET PER MM 35-20-00.
- [SDR SWIA200515436](https://openairdocs.org/sdr/SWIA200515436), Aug 15, 2005: BEARING. WORN. AFTER PUSHBACK FROM SLC, HEARD AUDIBLE CLICKING SOUND AS WELL AS BUMPING FEEDBACK FROM PEDALS. REPLACED LEFT RUDDER PEDAL PIVOT BEARINGS AND PEDAL ADJUSTMENT YO
- [SDR SWIA200515354](https://openairdocs.org/sdr/SWIA200515354), Jul 24, 2005: CONTROL UNIT. MALFUNCTIONED. HORIZONTAL TRIM AND MACH TRIM KICKED OFF IN FLIGHT REPEATEDLY. REMOVED AND REPLACED HSTCU. OPERATIONAL CHECK GOOD IAW CRJ MM 27-41-01.
- [SDR SWIA200515344](https://openairdocs.org/sdr/SWIA200515344), Jul 20, 2005: SWITCH. MALFUNCTIONED. STAB TRIM AND MACH TRIM CAUTION MESSAGES WILL NOT RESET. REPLACED FO'S STAB TRIM SWITCH IAW MM 27-41-05. OPERATIONAL CHECK GOOD.
- [SDR SWIA200515268](https://openairdocs.org/sdr/SWIA200515268), Jul 9, 2005: CONTROL UNIT. MALFUNCTIONED. STAB TRIM CH 1 AND CH 2 AND MACH TRIM CAUTION MESSAGES INFLIGHT. REPLACED HSTCU IAW MM 22-41-01. OPERATIONAL CHECK GOOD.
- [SDR SWIA200514788](https://openairdocs.org/sdr/SWIA200514788), Mar 22, 2005: CONTROLLER. MALFUNCTIONED. FLAP FAIL AFTER LANDING. REPLACED FECU WITH SERVICEABLE UNIT IAW CRJ MM 27-51-05.
- [SDR SWIA200414087](https://openairdocs.org/sdr/SWIA200414087), Nov 9, 2004: ENGINE. POWER LOSS. ON DESCENT RT ENGINE N1, SPOOLED DOWN, ITT INCREASED TO 800 DEGREES, AND A BANG WAS HEARD. N1 DID NOT RESPOND TO THRUST LEVER ADVANCEMENT. ENGINE WAS LEFT AT ID
- [SDR SWIA200413848](https://openairdocs.org/sdr/SWIA200413848), Sep 22, 2004: TRIM SWITCH. MALFUNCTIONED. CAPT SIDE TRIM SWITCH WILL COMMAND THE SURFACE NOSE DOWN BUT NOT NOSE UP. REMOVED AND REPLACED CAPTAINS TRIM SWITCH IAW 27-41-30. OPERATIONAL CHECK GOOD. P/N 30
- [SDR SWIA200413841](https://openairdocs.org/sdr/SWIA200413841), Sep 12, 2004: TRIM SWITCH. MALFUNCTIONED. CAPTAIN'S TRIM SWITCH WILL NOT TRIM NOSE UP, NOSE DOWN OK. REMOVED AND REPLACED CAPTAIN TRIM SWITCH ON YOKE IAW CRJ200 MM 27-00-00. OPERATIONAL CHECK GOOD.
- [SDR SWIA200413720](https://openairdocs.org/sdr/SWIA200413720), Aug 16, 2004: CONTROL UNIT. MALFUNCTIONED. FLIGHT SPLR FAULT STATUS MESSAGE FLASHES ON AND OFF DURING FLIGHT. REMOVED AND REPLACED NR 1 SECU. OPERATIONAL CHECK GOOD.
- [SDR SWIA200413681](https://openairdocs.org/sdr/SWIA200413681), Aug 8, 2004: CONTROL UNIT. MALFUNCTIONED. AFTER STARTUP A SPOILERONS FAULT MESSAGE DISPLAYED. REMOVED AND REPLACED NR 2 SECU IAW MM 27-61-05, OPERATIONAL CHECK GOOD.
- [SDR WVE2004F00018](https://openairdocs.org/sdr/WVE2004F00018), May 10, 2004: FLOOR SUPPORT. CRACKED. FLOOR SUPPORT ANGLE ON INTERCOSTAL AT FS 484, LBL 27 IS CRACKED. PROBABLE CAUSE: STRESS (EA09200402314)
- [SDR WVE2004F00017](https://openairdocs.org/sdr/WVE2004F00017), May 10, 2004: FLOOR SUPPORT. CRACKED. FLOOR SUPPORT ANGLES AT FS280, RBL9 ARE CRACKED. PROBABLE CAUSE: STRESS (EA09200402314)
- [SDR WVE2004F00016](https://openairdocs.org/sdr/WVE2004F00016), May 10, 2004: FLOOR SUPPORT. CRACKED. FLOOR SUPPORT ANGLES AT FS280, LBL9 ARE CRACKED. PROBABLE CAUSE: STRESS (EA09200402314)
- [SDR WVE2004F00015](https://openairdocs.org/sdr/WVE2004F00015), May 10, 2004: RIB. CRACKED. RT BATTERY RIB AT WS 53.60 IS CRACKED. PROBABLE CAUSE: STRESS (EA09200402314)
- [SDR WVE2004F00014](https://openairdocs.org/sdr/WVE2004F00014), May 10, 2004: RIB. CRACKED. LEFT BATTERY RIB AT WS 53.60 IS CRACKED. PROBABLE CAUSE; STRESS. RECOMMENDATION: REPAIR IAW MFG REPAIR EO. (EA09200402314)
- [SDR SWIA200413297](https://openairdocs.org/sdr/SWIA200413297), May 3, 2004: FLOOR SUPPORT. CRACKED. FLOOR SUPPORT ANGLE ON INTERCOSTAL AT FS 484 LBL 27 IS CRACKED. (FOUND DURING C-CHECK INSPECTION). REMOVED AND REPLACED CRACKED CLIP AT LBL 27 BS 484 IAW REO 60
- [SDR SWIA200413296](https://openairdocs.org/sdr/SWIA200413296), May 3, 2004: FLOOR SUPPORT. CRACKED. FLOOR SUPPORT ANGLES AT FS 280, RBL 9 ARE CRACKED. (FOUND DURING C-CHECK INSPECTION). INSTALLED NEW SUPPORT ANGLES AT FS 280 RBL 9 IB AND OB AND LBL 9 IB AND OB
- [SDR SWIA200413295](https://openairdocs.org/sdr/SWIA200413295), May 3, 2004: FLOOR SUPPORT. CRACKED. FLOOR SUPPORT ANGLES AT FS280, LBL 9 ARE CRACKED. (FOUND DURING C-CHECK INSPECTION). INSTALLED NEW SUPPORT ANGLES AT FS 280 RBL 9 INBOARD AND OUTBOARD AND LBL 9
- [SDR SWIA200413294](https://openairdocs.org/sdr/SWIA200413294), May 3, 2004: RIB. CRACKED. LT BATT RIB AT WS 53.60 IS CRACKED. (FOUND DURING C-CHECK INSPECTION). COMPLIED WITH 1 THROUGH 9 OF REO 601R-57-51-046. FAB. PARTS FROM 56144-4 ANGLE .063 AND 7
- [SDR SWIA200413293](https://openairdocs.org/sdr/SWIA200413293), May 3, 2004: RIB. CRACKED. RT BATT RIB AT WS 53.60 IS CRACKED. (FOUND DURING C-CHECK INSPECTION). REMOVED DAMAGE AND INSTALLED REPAIR PARTS DOUBLER AND FILLER IAW REO 601R-57-51-046 REPAI
- [SDR SWIA200413292](https://openairdocs.org/sdr/SWIA200413292), May 3, 2004: ANGLE. CRACKED. FS 625 LT OBLIQUE ANGLE P/N 6013501251 CRACKED IN RADIUS. (FOUND DURING C-CHECK INSPECTION). REMOVED AND REPLACED WITH NEW ANGLES IAW CRJ 200 SRM 51-21-11, 51-2

All 80: https://openairdocs.org/deregistered/N597SW-2015-05-15/reports.md

## 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 20020415006799I](https://openairdocs.org/incident/20020415006799I), Apr 15, 2002: Cndair CL6002B19 (N597SW), Casper, WY, Minor damage. (-23) Right side windshield shattered in flight. Attached service difficulty report query shows 224 incidents of this since 1993.

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.