# N629BR: 1998 Bombardier CL-600-2B19, registration cancelled 2023-02-17 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 17, 2023 - 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: 7251 - Year built: 1998 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 23, 1998 - Certificate issued: February 10, 2015 - Last registry action: September 29, 2020 - Mode S code: A837D5 - Owner when cancelled: [Skywest Airlines Inc](https://openairdocs.org/faa-owner/SKYWEST%20AIRLINES%20INC) - Location: [St George, UT](https://openairdocs.org/faa-place/UT/St%20George) - Owner type: Corporation - Owner's area on the map: 37.0461° N, 113.5573° W: Placed by OpenAirDocs at the center of ZIP code 84790, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N629BR - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=629BR - Page: https://openairdocs.org/deregistered/N629BR-2023-02-17 From the FAA registry file of November 12, 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 (154, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SWIA2019111846767](https://openairdocs.org/sdr/SWIA2019111846767), Nov 17, 2019: WARNING MESSAGE. ILLUMINATED. GEAR DISAGREE & NOSE DOOR OPEN RED WARNING MESSAGE AFTER CALL FOR GEAR UP. 3 SECONDS LATER, MESSAGE EXTINGUISHED WITH NO FURTHER INCIDENT. FLIGHT 4223 CLOSED DE - [SDR SWIA2019010745410](https://openairdocs.org/sdr/SWIA2019010745410), Jan 7, 2019: WARNING SYSTEM. FALSE ACTIVATION. WHILE ON THE GROUND, APU FIRE AND ASSOCIATED FIREX BOTTLE DISCHARGED. APU FAULT MESSAGE INITIALLY BUT NOW EXTINGUISHED ON SUBSEQUENT POWER UP. APU BTL LO CAUTIO - [SDR SWIA2018110645245](https://openairdocs.org/sdr/SWIA2018110645245), Nov 6, 2018: WARNING SYSTEM. ACTIVATED. A/SKID OTBD CAUTION MSG. EMERGENCY DECLARED. DIVERTED. (FLT 7439) CLOSED DEFERRED A/SKID OUTBOARD CHANNEL PER MEL. - [SDR SWIA2018082345007](https://openairdocs.org/sdr/SWIA2018082345007), Aug 23, 2018: SHUTOFF VALVE. FAILED. AFTER TAKEOFF, SWAPPED BLEEDS FROM THE APU TO THE ENGINES AND THE NR 2 PACK SHUTOFF. THEN GOT A NR 1 PACK HIGH PRESSURE. LEVELED THE PLANE AT 10000, AND THE CAB - [SDR SWIA2018062244805](https://openairdocs.org/sdr/SWIA2018062244805), Jun 22, 2018: CONNECTOR. UNSECURE. WOW INPUT CAUTION MESSAGE DURING FINAL, WITH GEAR DOWN, FLAPS 30. COMPLIED WITH QRH. ABORTED APPROACH. LANDED WITHOUT INCIDENT. SECURED THE SAFETY CONNECTOR PLU - [SDR SWIA2018051544663](https://openairdocs.org/sdr/SWIA2018051544663), Apr 21, 2018: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT, BS 559 TO 559+16 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM. - [SDR SWIA2018051544664](https://openairdocs.org/sdr/SWIA2018051544664), Apr 16, 2018: FLOOR PANEL. CORRODED. RIGHT SIDE PRESSURE FLOOR PANEL HAS CORROSION BS 499 TO 559. BLENDED IAW REO. - [SDR SWIA2018051544662](https://openairdocs.org/sdr/SWIA2018051544662), Apr 16, 2018: STRAP. CORRODED. BS 559 FLOORBEAM STRAP HAS CORROSION, BETWEEN RBL 27 AND RBL 42. REMOVED AND REPLACED THE STRAP IAW REO. - [SDR SWIA2018051544661](https://openairdocs.org/sdr/SWIA2018051544661), Apr 16, 2018: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT LEFT SIDE, BS 424 TO 409.128 CORRODED. REPAIRED IAW REO. - [SDR SWIA2018051544660](https://openairdocs.org/sdr/SWIA2018051544660), Apr 14, 2018: SKIN. CORRODED. EXTERIOR LOWER SKIN, BS 599+112, STRINGER 27 CORRODED RT AND LT SIDES. REPAIRED THE SKIN IAW REO. - [SDR SWIA2018051544675](https://openairdocs.org/sdr/SWIA2018051544675), Apr 10, 2018: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT CORRODED AT LBL 43, BS 559+96 - 563. REMOVED AND REPLACED THE FLOOR SUPPORT IAW REO. - [SDR SWIA2018051544674](https://openairdocs.org/sdr/SWIA2018051544674), Apr 10, 2018: FRAME. CORRODED. FRAME AT BS 605 WAS FOUND CORRODED BETWEEN STRINGERS 25L & 26R. REMOVED AND REPLACED THE FRAME IAW SRM. - [SDR SWIA2018051544659](https://openairdocs.org/sdr/SWIA2018051544659), Apr 10, 2018: DOOR SILL. CORRODED. CARGO DOOR SILL CORRODED AT LBL 43, BETWEEN BS 563 & 620. REPLACED THE DOOR SILL IAW REO. - [SDR SWIA2018051544658](https://openairdocs.org/sdr/SWIA2018051544658), Apr 10, 2018: FRAME. CORRODED. FRAME AT BS 574 WAS FOUND CORRODED BETWEEN STRINGERS 26L & 26R. REPAIRED THE FRAME IAW REO. - [SDR SWIA2018051544673](https://openairdocs.org/sdr/SWIA2018051544673), Apr 9, 2018: FLOOR SUPPORT. CORRODED. CARGO FLOOR SUPPORT CORRODED AT LBL 27, BS 569 - 619. REPLACED THE FLOOR SUPPORT IAW SRM AND REO. - [SDR SWIA2018051544672](https://openairdocs.org/sdr/SWIA2018051544672), Apr 9, 2018: BULKHEAD. GOUGED. FWD SIDE OF THE AFT PRESSURE BULKHEAD WAS GOUGED. REPAIRED THE BS 621 BULKHEAD, RBL 27.5, RBL 18, LBL 18, AND LBL 27.5 IAW REO. - [SDR SWIA2018051544671](https://openairdocs.org/sdr/SWIA2018051544671), Apr 8, 2018: SKIN. CORRODED. AFT FUSELAGE, LOWER SKIN AROUND THE CARGO DOOR HAD CORROSION. REMOVED THE CORROSION TO A SMOOTH CONTOUR IAW SRM. - [SDR SWIA2018051544670](https://openairdocs.org/sdr/SWIA2018051544670), Apr 7, 2018: SKIN. DENTED. EXTERNAL LEFT, AFT LOWER FUSELAGE SKIN BETWEEN BS 682 AND 700 HAD TWO INWARD DENTS AND TWO PROTRUDING DENTS. REPAIRED THE SKIN IAW REO. - [SDR SWIA2018051544669](https://openairdocs.org/sdr/SWIA2018051544669), Apr 7, 2018: SKIN. DENTED. EXTERIOR RIGHT LOWER FUSELAGE SKIN BETWEEN BS 630 AND 700 HAD 11 PROTRUDING DENTS. REPAIRED THE SKIN IAW REO - [SDR SWIA2018051544668](https://openairdocs.org/sdr/SWIA2018051544668), Apr 6, 2018: SKIN. GOUGED. PAX DOOR EXTERNAL SKIN WAS FOUND GOUGED ON THE FWD SIDE OF THE EXTERNAL HANDLE. REPAIRED THE DOOR SKIN IAW REO. - [SDR SWIA2018051544667](https://openairdocs.org/sdr/SWIA2018051544667), Apr 6, 2018: SKIN. DENTED. TWO DENTS ON THE RT LOWER FUSELAGE SKIN AFT OF BS 605 AND BETWEEN STRINGERS 24R - 25R AND FWD OF BS 621, BETWEEN STRINGERS 23R - 24R. REPAIRED IAW REO. - [SDR SWIA2018051544666](https://openairdocs.org/sdr/SWIA2018051544666), Apr 6, 2018: SKIN. DENTED. ONE DENT WAS FOUND ON THE LT LOWER FUSELAGE SKIN BETWEEN BS 605 - 621, STRINGERS 22L - 23L. REPAIRED THE SKIN IAW REO. - [SDR SWIA2018051544665](https://openairdocs.org/sdr/SWIA2018051544665), Apr 6, 2018: SKIN. DENTED. A DENT WAS FOUND APPROXIMATELY 18 INCHES FORWARD OF BS 280 ON THE LOWER LEFT FUSELAGE SKIN. REPAIRED IAW REO. - [SDR SWIA201642185](https://openairdocs.org/sdr/SWIA201642185), May 9, 2016: FRAME. CORRODED. FRAME AT BS 319 CORRODED BETWEEN STRINGERS 26 AND 27L. COMPLIED WITH EA. PERFORMED PRESSURIZATION LEAK CHECK IAW AMM. CHECKED GOOD, NO LEAKS NOTED. - [SDR SWIA201642184](https://openairdocs.org/sdr/SWIA201642184), May 9, 2016: ANGLE. CORRODED. ANGLE CORRODED FWD SIDE OF FRAME AT FS 394 BETWEEN STR 25L AND 25R. COMPLIED WITH EA. - [SDR SWIA201642183](https://openairdocs.org/sdr/SWIA201642183), May 6, 2016: VANE. CHAFED. CHAFE DAMAGE FOUND ON LT INBD FLAP VANE, ON OTBD L/E SKIN. REPLACED NEW, IAW SRM. - [SDR SWIA201642182](https://openairdocs.org/sdr/SWIA201642182), May 5, 2016: DOOR SILL. CORRODED. PASSENGER DOOR LOWER SILL, VERTICAL FACE AND CAP ANGLE HAS CORROSION. R & R PAX DOOR LOWER SILL VERTICAL ANGLE, PN: 601R31527-219 AND CAP ANGLE PN: 601R51527-20 - [SDR SWIA201642181](https://openairdocs.org/sdr/SWIA201642181), May 1, 2016: ACCESS PANEL. CHAFED. PANEL 599BB IS CHAFED. REPLACED PANEL 599BB WITH FACTORY NEW PART IAW SRM. - [SDR SWIA201642180](https://openairdocs.org/sdr/SWIA201642180), May 1, 2016: ACCESS PANEL. CORRODED. PAX DOOR PANEL 832ER HAS CORROSION. REPLACED PANEL 832ER IAW SRM. - [SDR SWIA201642179](https://openairdocs.org/sdr/SWIA201642179), May 1, 2016: ACCESS PANEL. CORRODED. PAX DOOR PANEL 832EL HAS CORROSION. REPLACED PANEL 832EL IAW SRM. - [SDR SWIA201642178](https://openairdocs.org/sdr/SWIA201642178), May 1, 2016: ACCESS PANEL. CORRODED. PAX DOOR PANEL 832BL HAS CORROSION. INSTALLED PANEL 832BL IAW SRM. - [SDR SWIA201642177](https://openairdocs.org/sdr/SWIA201642177), May 1, 2016: ACCESS PANEL. CORRODED. PAX DOOR PANEL 832BR HAS CORROSION. PAX DOOR ACCESS PANEL 832BR REPLACED WITH A NEW PANEL, IAW SRM. - [SDR SWIA201541321](https://openairdocs.org/sdr/SWIA201541321), Jun 13, 2015: FLOORBEAM. CRACKED. FS 280 FLOORBEAM HAS LOWER FLANGE CRACKED LBL 12 - 13.5 AND OTBD, LBL 9. REPAIRED THE FLOORBEAM IAW EA. - [SDR SWIA201541327](https://openairdocs.org/sdr/SWIA201541327), Jun 11, 2015: FLOORBOARD. DELAMINATED. FLOORBOARD 232BRF DELAMINATED. REPAIRED IAW EA. - [SDR SWIA201541326](https://openairdocs.org/sdr/SWIA201541326), Jun 11, 2015: PLATE. CORRODED. FOUND CORROSION ON RT FWD EMERGENCY EXIT DOOR LOWER SILL COVER PLATE ASSY, REPLACED COVER PLATE ASSY IAW SRM. - [SDR SWIA201541325](https://openairdocs.org/sdr/SWIA201541325), Jun 11, 2015: FLOORBEAM. CRACKED. FS 280 TO RBL 9, FLOORBEAM ANGLE WAS FOUND CRACKED. R & R THE ANGLE IAW SRM. - [SDR SWIA201541324](https://openairdocs.org/sdr/SWIA201541324), Jun 11, 2015: SEAT TRACK. CORRODED. SEAT TRACK AT RBL 9 FROM BS 364 - 400 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM. - [SDR SWIA201541323](https://openairdocs.org/sdr/SWIA201541323), Jun 11, 2015: SEAT TRACK. GOUGED. SEAT TRACK LBL 9 FROM BS 364-400 GOUGED. REMOVED DAMAGED SEAT TRACK AND INSTALLED A NEW SEAT TRACK IAW AMM. - [SDR SWIA201541322](https://openairdocs.org/sdr/SWIA201541322), Jun 11, 2015: FLOORBEAM. CORRODED. FS 280, FWD FLOORBEAM ANGLE IS CORRODED FROM RBL 9 TO LBL 9. R & R THE FLOORBEAM ANGLE IAW SRM. - [SDR SWIA201541320](https://openairdocs.org/sdr/SWIA201541320), Jun 11, 2015: DOOR SILL. CORRODED. PASSENGER DOOR BOTTOM PLATE SILL CORRODED. REMOVED BLISTERED AND FLAKING PAINT FROM PASSENGER DOOR BOTTOM PLATE SILL IAW SRM, NO DAMAGE NOTED. - [SDR SWIA201439518](https://openairdocs.org/sdr/SWIA201439518), Oct 15, 2014: WARNING LIGHT. FALSE ACTIVATION. RETURNED TO DEPARTURE FOR PRESSURIZATION ISSUES AND SERVICE DOOR CAUTION. INSPECTED ALL DOOR SEALS-NO ISSUES. PERFORMED OPS CHECK OF THE PRESSURIZATION SYSTEM. - [SDR SWIA201439262](https://openairdocs.org/sdr/SWIA201439262), Sep 9, 2014: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHT OUT IN THE CABIN. CHANGED ALL FOUR BATTERY PACKS. - [SDR SWIA201439105](https://openairdocs.org/sdr/SWIA201439105), Aug 8, 2014: BATTERY PACK. INOPERATIVE. F/O EMERGENCY FLASHLIGHT INOPERATIVE. R & R BATTERY PACK FOR THE F/O EMEGENCY FLASHLIGHT IAW AMM. - [SDR SWIA201438869](https://openairdocs.org/sdr/SWIA201438869), Jul 27, 2014: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LIGHT. - [SDR SWIA201438303](https://openairdocs.org/sdr/SWIA201438303), Jun 21, 2014: LAMP. INOPERATIVE. RT SIDE EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP. - [SDR SWIA2014061338165](https://openairdocs.org/sdr/SWIA2014061338165), Jun 5, 2014: BATTERY PACK. INOPERATIVE. EXIT LIGHT ROW 8A IS INOPERATIVE. R & R NR 2 EMERGENCY LIGHTING BATTERY PACK IAW AMM, PN ON: 2013-1A, PN OFF: AD-2013-1A, SN ON: 112163, SN OFF: 69898. (2014NM0 - [SDR SWIA201437765](https://openairdocs.org/sdr/SWIA201437765), May 24, 2014: LIGHT. INOPERATIVE. NR 7 EMERGENCY LIGHT ON THE EXTERIOR LT SIDE OF THE FUSELAGE INOPERATIVE. R & R NR 7 EMERGENCY LIGHT IAW AMM. - [SDR SWIA201437599](https://openairdocs.org/sdr/SWIA201437599), May 15, 2014: LIGHT. INOPERATIVE. LEFT WING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT IAW AMM. - [SDR SWIA201437460](https://openairdocs.org/sdr/SWIA201437460), May 2, 2014: PANEL. CHAFED. PANEL 599BB CHAFED . C-CHECK, BLENDED CHAFE ON PANEL 599BB IAW REO. - [SDR SWIA201437482](https://openairdocs.org/sdr/SWIA201437482), Apr 25, 2014: SKIN. CORRODED. FUEL ACCESS PANEL ON LT LOWER WING PLANK UNDER PANEL 550GB HAS CORROSION. C-CHECK, REMOVED CORROSION UNDER PANEL 550GB ON WING PLANK IAW REO. All 154: https://openairdocs.org/deregistered/N629BR-2023-02-17/reports.md --- 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, except the copies of manufacturers’ service documents, which belong to their rights holders.