# N592SW: 1998 Bombardier CL-600-2B19, registration cancelled 2012-02-03

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 3, 2012
- 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: 7279
- Year built: 1998
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 23, 1998
- Certificate issued: January 14, 2008
- Last registry action: June 19, 2008
- Mode S code: A7A67A
- Owner when cancelled: [Bombardier Services Corp](https://openairdocs.org/faa-owner/BOMBARDIER%20SERVICES%20CORP)
- Location: [Colchester, VT](https://openairdocs.org/faa-place/VT/Colchester)
- Owner type: Non-citizen corporation
- Owner's area on the map: 44.5541° N, 73.2255° W: Placed by OpenAirDocs at the center of ZIP code 05446, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N592SW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=592SW
- Page: https://openairdocs.org/deregistered/N592SW-2012-02-03

From the FAA registry file of October 27, 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 (58, newest 50)

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

- [SDR COMA0760631](https://openairdocs.org/sdr/COMA0760631), Nov 8, 2007: FLAP SYSTEM. MALFUNCTIONED. FLIGHT 5308 - EN ROUTE CVG-LGA RECEIVED FLAP FAIL MESSAGE. DIVERTED TO JFK, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. COMPLIED WITH AD 2006-12-21 FLAP CAUTIO
- [SDR COMA0760432](https://openairdocs.org/sdr/COMA0760432), Jun 11, 2007: CONTROL HANDLE. FAULTY. AT 4000FT AND 210KTS RECEIVED GEAR HORN, TERRAIN WARNING AND GEAR DOWN AMBER. CLEARED AFTER 45 SECONDS. GEAR IND TURNED WHITE AFTER 10 SECONDS. 2ND INCIDENT, FI
- [SDR COMA0760389](https://openairdocs.org/sdr/COMA0760389), May 20, 2007: FLAP SYSTEM. FAILED. FLIGHT 5067 - FLAP FAIL AT GATE. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM
- [SDR COMA0760313](https://openairdocs.org/sdr/COMA0760313), Apr 11, 2007: FLAP. MALFUNCTIONED. AFTER LANDING DURING FLAP RETRACTION RECEIVED A FLAP FAIL MESSAGE AT 27 DEGREES. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTI
- [SDR COMA0760229](https://openairdocs.org/sdr/COMA0760229), Mar 6, 2007: WINDOW. CRACKED. FLIGHT 9438 - F/O'S SIDE WINDOW CRACKED PASSING THROUGH 26,000 FT. REPLACED WINDOW.
- [SDR COMA0660408](https://openairdocs.org/sdr/COMA0660408), Jun 27, 2006: SENSOR. FAULTY. FLIGHT 5480 - AFTER TAKEOFF RECEIVED A RIGHT PACK OVERPRESSURE WARNING, FLIGHT RETURNED TO THE FIELD. REPLACED THE DUCT TEMPERATURE SENSOR.
- [SDR COMA0660400](https://openairdocs.org/sdr/COMA0660400), Jun 22, 2006: CONNECTOR. DIRTY. FLIGHT 5506 - RECEIVED APU TEMP MASTER CAUTION IN FLIGHT/ DIVERTED TO ORF AND LANDED WITHOUT INCIDENT. FOUND APU OIL SERVICED PROPERLY. CLEANED CONNECTOR ON OIL
- [SDR SWIA200516048](https://openairdocs.org/sdr/SWIA200516048), Dec 27, 2005: PIN. LOOSE. STAB TRIM CH 1 STATUS MESSAGE OCCURRED TWICE, ONCE ON CLIMB-OUT, ONCE ON TAXI IN. REPLACED HSTA AND MCU IAW AMM 27-40-00, 27-42-05 AND RECONNECTED LOOSE PINS AT
- [SDR SWIA200516002](https://openairdocs.org/sdr/SWIA200516002), Dec 16, 2005: TRIM SWITCH. MALFUNCTIONED. CA STAB TRIM INTERMITTENT, BOTH DIRECTIONS. REPLACED CAPTIANS TRIM SWITCH. IAW 27-41-05. OPERATIONAL CHECK GOOD IAW 27-41-01.
- [SDR SWIA200515884](https://openairdocs.org/sdr/SWIA200515884), Nov 22, 2005: LAMP. BURNED OUT. NR 2 CEILING EMERGENCY FLOODLIGHT INOP. RELAMPED NR 2 CEILING EMERGENCY FLOODLIGHT. OPERATIONAL CHECK GOOD.
- [SDR SWIA200515668](https://openairdocs.org/sdr/SWIA200515668), Oct 11, 2005: BOLT. LOOSE. ABORTED T/O DUE TO "CONFIG SPOILERS" WARNING MSG. REPLACED BOLT AND BUSHINGS AT ROD END ATTACH POINT RIGHT FLIGHT SPOILER OB PCU AND ADJUSTED PCU IAW MM 27-62-0
- [SDR SWIA200515470](https://openairdocs.org/sdr/SWIA200515470), Aug 26, 2005: PCU. MALFUNCTIONED. FLIGHT SPOILERS FAULT STATUS MSG ON ED2. REPLACED RIGHT NR 2 OUTBOARD FLIGHT SPOILER PCU IAW MM 29-62-01. OPERATIONAL CHECK GOOD.
- [SDR SWIA200515100](https://openairdocs.org/sdr/SWIA200515100), Jun 4, 2005: CONNECTOR. LOOSE. OVERHEAD EMERGENCY EXIT SIGN AT OVERWING EXITS INOP. RESECURED LOOSE CONNECTOR. OPERATIONAL CHECK GOOD IAW AMM SUBTASK 33-51-00-720-801.
- [SDR SWIA200515553](https://openairdocs.org/sdr/SWIA200515553), May 16, 2005: ANGLE. CRACKED. FS 625 LT ANGLE STR 14L CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06.
- [SDR SWIA200515112](https://openairdocs.org/sdr/SWIA200515112), May 15, 2005: FLOORBEAM. CRACKED. FS 280 BELOW FLOOR RBL 9.0 OUTBOARD ANGLE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-13, 51-42-21, 51-23-00, 51-25-00
- [SDR SWIA200515111](https://openairdocs.org/sdr/SWIA200515111), May 15, 2005: FLOOR SUPPORT. CORRODED. FLOOR ANGLE CORRODED IN NUMEROUS LOCATIONS FROM FS 409 +128 TO FS 559 AND LBL 36 TO 47, ITEM FOUND AT C-CHECK INSPECTION. BLENDED OUT DAMAGE IAW CRJ SRM 53-41-4
- [SDR SWIA200515110](https://openairdocs.org/sdr/SWIA200515110), May 15, 2005: FLOOR SUPPORT. CORRODED. FLOOR ANGLE CORRODED IN NUMEROUS LOCATIONS FROM FS 409 +128 TO FS 559 AND RBL 36 TO 47, ITEM FOUND AT C-CHECK INSPECTION. BLENDED OUT DAMAGE IAW CRJ SRM 53-41-4
- [SDR SWIA200515109](https://openairdocs.org/sdr/SWIA200515109), May 15, 2005: STEP. CORRODED. PAX DOOR TOP STEP HAS CORROSION ON HINGE, ITEM FOUND AT C-CHECK INSPECTION. HINGE REPLACED IAW CRJ SRM 51-41-02.
- [SDR SWIA200515108](https://openairdocs.org/sdr/SWIA200515108), May 15, 2005: FLOOR PANEL. CRACKED. FS 193 - LEFT SIDE ELECTRICAL BAY FLOOR CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED CRACK IAW CRJ REO 601R-53-11-001 REV NC.
- [SDR SWIA200514664](https://openairdocs.org/sdr/SWIA200514664), Mar 2, 2005: LIGHT. BURNED OUT. ONE CEILING LEVEL EMERGENCY FLOODLIGHT INOPERATIVE. RELAMPED, OPERATIONAL CHECKS GOOD.
- [SDR SWIA200514653](https://openairdocs.org/sdr/SWIA200514653), Feb 28, 2005: PCU. MALFUNCTIONED. SPOILERON FAULT STATUS MESSAGE UPON LANDING. REPLACED RIGHT OUTBOARD PCU IAW 22-61-05, OPERATIONAL CHECK GOOD.
- [SDR SWIA200414062](https://openairdocs.org/sdr/SWIA200414062), Nov 4, 2004: CONVERTER. INOPERATIVE. EMERGENCY TRACK LIGHTING AT SEAT 12AB IS NOT ILLUMINATING. REMOVED AND REPLACED CONVERTER IAW 33-00-00. OPERATIONAL CHECK GOOD.
- [SDR SWIA200413847](https://openairdocs.org/sdr/SWIA200413847), Sep 25, 2004: ACTUATOR. MALFUNCTIONED. COULD NOT GET STAB CHANNEL NR 2 TO ENGAGE. REMOVED AND REPLACED THE HORIZONTAL STAB TRIM ACTUATOR AND THE MOTOR CONTROL UNIT. OPERATIONAL CHECK GOOD. P/N 7062-3
- [SDR SWIA200413821](https://openairdocs.org/sdr/SWIA200413821), Sep 20, 2004: CONTROL UNIT. MALFUNCTIONED. STAB CHANNEL 2 WILL NOT ENGAGE. REMOVED AND REPLACED HSTCU IAW AMM 27-41-01. OPERATIONAL CHECK GOOD.
- [SDR SWIA200413794](https://openairdocs.org/sdr/SWIA200413794), Sep 10, 2004: TRIM SWITCH. MALFUNCTIONED. STAB TRIM CHANNEL 2 WILL NOT ENGAGE. REMOVED AND REPLACED BOTH TRIM SWITCHES IAW MM 27-41-30. OPERATIONAL CHECK GOOD.
- [SDR SWIA200413689](https://openairdocs.org/sdr/SWIA200413689), Aug 12, 2004: CONTROL UNIT. MALFUNCTIONED. STAB TRIM CHANEL 1 INOPERATIVE. REMOVED AND REPLACED STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT IAW MM 27-42-01 AND 27-42-05. OPERATIONAL CHECK GOOD. P/N: 8396-3
- [SDR SWIA200413679](https://openairdocs.org/sdr/SWIA200413679), Aug 2, 2004: SWITCH. MALFUNCTIONED. STAB CH 1 INOP MESSAGE. REMOVED AND REPLACED CAPTIANS STAB TRIM DISCONNECT SWITCH IAW MM 27-41-30. OPERATIONAL CHECK GOOD.
- [SDR SWIA200413394](https://openairdocs.org/sdr/SWIA200413394), Jun 4, 2004: PCU. MALFUNCTIONED. SPOILERON FAULT MESSAGE ON TAXI OUT WITH BOTH ENGINES RUNNING. REMOVED AND REPLACED LT NR 1 SPOILERON PCU IAW MM 27-62-01. OPERATIONAL CHECK GOOD.
- [SDR SWIA200413373](https://openairdocs.org/sdr/SWIA200413373), May 31, 2004: PCU. MALFUNCTIONED. SPOILERON FAULT STATUS MESSAGE WOULD NOT CLEAR. REMOVED AND REPLACED LEFT WING INBOARD FLIGHT SPOILER INBOARD PCU IAW MM 27-61-00. LEAK AND OPS CHECK GOOD.
- [SDR SWIA200413007](https://openairdocs.org/sdr/SWIA200413007), Mar 8, 2004: CONTROL UNIT. FAILED. LEFT SPOILERON FAULT MESSAGE ON EICAS. REMOVED AND REPLACED NR 1 SECU IAW MM 27-61-05. OPS CHECK GOOD. P/N 49-164-06, S/N OFF 0929.
- [SDR SWIA200412970](https://openairdocs.org/sdr/SWIA200412970), Mar 2, 2004: BPSU. MALFUNCTIONED. RECEIVED A FLAPS FAIL WHEN SELECTING FLAPS 20 DURING APPROACH. REMOVED AND REPLACED LEFT BPSU IAW CRJ MM 27-51-10. OPS CHECK GOOD. P/N: 855D100-9, S/N ON: 316B,
- [SDR SWIA200412945](https://openairdocs.org/sdr/SWIA200412945), Feb 27, 2004: SENSOR. MALFUNCTIONED. STALL FAIL AFTER ROTATION. REMOVED AND REPLACED LEFT AOA SENSOR IAW CL600 MM 27-35-05. OPS CHECKS GOOD.
- [SDR SWIA200412757](https://openairdocs.org/sdr/SWIA200412757), Jan 4, 2004: PDU. MALFUNCTIONED. FLAP FAIL MESSAGE WHEN SELECTING FLAPS AT 45 DEGREES. REMOVED AND REPLACED FLAP PDU IAW MM 27-52-01. OPS CHECKS GOOD.
- [SDR SWIA200312668](https://openairdocs.org/sdr/SWIA200312668), Dec 5, 2003: SUPPORT. CRACKED. ENGINE SUPPORT BEAM UPPER WEB RBL 6 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. UPPER WEB REPAIRED IAW CRJ REO 601R-53-61-345 REV ''C'' AND RII 53-401.
- [SDR SWIA200312667](https://openairdocs.org/sdr/SWIA200312667), Dec 5, 2003: SILL. CRACKED. CARGO PIT CARGO DOOR FLOOR LANDING SILL IS CRACKED UNDER STEP PLATE ASSY PIN STOP FITTING; FS 576.00; LBL 42.0. DISCOVERED DURING C-CHECK INSPECTION. ANGLE REPL
- [SDR SWIA200312666](https://openairdocs.org/sdr/SWIA200312666), Dec 5, 2003: BEAM. CRACKED. TRANSVERSE BEAM REMOTE ANGLE FOR DOOR STOP FITTING IS CRACKED; FS 589.00; LBL 42.0. DISCOVERED DURING C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11 & 
- [SDR SWIA200312665](https://openairdocs.org/sdr/SWIA200312665), Dec 5, 2003: BEAM. CRACKED. ENGINE SUPPORT BEAM LOWER WEB RIGHT SIDE RBL 34 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. WEB REPAIRED IAW CRJ REO 601R-53-61-366 REV ''D'', RII 53-401.
- [SDR SWIA200312664](https://openairdocs.org/sdr/SWIA200312664), Dec 5, 2003: BEAM. CRACKED. ENGINE SUPPORT BEAM LOWER WEB LT SIDE LBL 34 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. WEB REPAIRED IAW CRJ REO 601R-53-61-366 REV ''D'' AND RII 53-401.
- [SDR SWIA200312663](https://openairdocs.org/sdr/SWIA200312663), Dec 5, 2003: INTERCOSTAL. CRACKED. FS 625 RIGHT INTERCOSTAL STRINGER 14R CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED INTERCOSTAL IAW CRJ SRM 51-40-11, 51-42-06.
- [SDR SWIA200312662](https://openairdocs.org/sdr/SWIA200312662), Dec 5, 2003: FLOORBEAM. CRACKED. FS 460 RIGHT FLOORBEAM RBL 9.0 O/B FITTING CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED FITTING IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21 & 
- [SDR SWIA200312661](https://openairdocs.org/sdr/SWIA200312661), Dec 5, 2003: BEAM. CRACKED. FS 280 TRANSVERSE BEAM RBL 11 LOWER FLANGE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. CUT-OUT AND REPAIRED DAMAGED SECTION OF TRANSVERSE BEAM IAW CRJ REO 60
- [SDR SWIA200312660](https://openairdocs.org/sdr/SWIA200312660), Dec 5, 2003: BEAM. CRACKED. FS 280 TRANSVERSE BEAM LBL 11 LOWER FLANGE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. CUT-OUT AND REPAIRED DAMAGED SECTION OF TRANSVERSE BEAM IAW CRJ REO 60
- [SDR SWIA200312659](https://openairdocs.org/sdr/SWIA200312659), Dec 5, 2003: FLOORBEAM. CRACKED. FS 280 RT FLOORBEAM RBL 90 INBOARD AND OUTBOARD ATTACH ANGLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11 & RII 53-401.
- [SDR SWIA200312760](https://openairdocs.org/sdr/SWIA200312760), Nov 28, 2003: RIB. CRACKED. LT PYLON FS 605 RIB CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED RIB IAW CRJ SRM 51-40-11. P/N: 601-37004-85.
- [SDR SWIA200312759](https://openairdocs.org/sdr/SWIA200312759), Nov 28, 2003: INTERCOSTAL. CRACKED. FS 484 LT INTERCOSTAL O/B FLANGE LBL 36 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED INTERCOSTAL IAW CRJ REO 601R-53-41-059 REV A AND RII
- [SDR SWIA200312758](https://openairdocs.org/sdr/SWIA200312758), Nov 28, 2003: FRAME. CRACKED. OUTER FLANGE ON FUSELAGE FRAME AT FS 220 AND STR 23L IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED FLANGE IAW CRJ DWG 600-34013 & RII 53-401.
- [SDR SWIA200312270](https://openairdocs.org/sdr/SWIA200312270), Aug 17, 2003: HEATER. MALFUNCTIONED. THE NR 1 GALLEY HTR CAUSES A SMOKEY SMELL WHEN ON. CREW REPORTS THAT THERE IS A STRONG BURNT ELECTRICAL SMELL IN THE GALLEY OR FLIGHT DECK JUST AFTER PUSHBACK. 
- [SDR SWIA200312198](https://openairdocs.org/sdr/SWIA200312198), Jul 16, 2003: ENGINE. MALFUNCTIONED. LEFT ENGINE FAILED ON DESCENT. JUST PRIOR TO FAILURE, ''L MAIN EJECTOR'' AND ''L SCAV EJECTOR'' MSG DISPLAYED ON EICAS. REMOVED AND REPLACED LEFT POWER PLANT IA
- [SDR SWIA200211614](https://openairdocs.org/sdr/SWIA200211614), Dec 24, 2002: ENGINE. MALFUNCTIONED. ENGINE NR 2 FAILURE INFLIGHT. DURING CRUISE FLIGHT THE RT ITT WAS 50 DEGREES HIGHER THAN ENGINE NR 1 WITH A REDUCTION OF N1 ON ENGINE NR 2 OF 4 PERCENT. REMOVED
- [SDR SWIA200211563](https://openairdocs.org/sdr/SWIA200211563), Dec 8, 2002: WARNING SYSTEM. ACTIVATED. STAB TRIM CHANNELS 1 AND 2 FAILED ON TAKEOFF. STAB TRIM AND MACH TRIM CAUTION MESSAGES. RETURNED TO MEM. PERFORMED BITE CHECK OF HSTCU. HSTCU SHOWS NO FAULTS IA

All 58: https://openairdocs.org/deregistered/N592SW-2012-02-03/reports.md

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