# N628BR: Canadair CL-600-2B19, registration cancelled 2006-12-06 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 6, 2006 - Exported to: South Africa - Status when cancelled: Valid registration - Airframe: [Canadair CL-600-2B19](https://openairdocs.org/model/canadair-cl-600-2b19) (registry code 1900309) - Data sheets: [TCDS A21EA-1](https://openairdocs.org/tcds/A21EA-1) (OpenAirDocs) - Serial number: 7240 - Type of aircraft: Fixed wing multi engine - Certificate issued: August 15, 2006 - Last registry action: August 15, 2006 - Mode S code: A8341E - Owner when cancelled: [US Bank Trust Na Trustee](https://openairdocs.org/faa-owner/US%20BANK%20TRUST%20NA%20TRUSTEE) - Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington) - Owner type: Corporation - Owner's area on the map: 39.4944° N, 75.6775° W: Placed by OpenAirDocs at the center of ZIP code 19709, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N628BR - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=628BR - Page: https://openairdocs.org/deregistered/N628BR-2006-12-06 From the FAA registry file of November 5, 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 Canadair CL-600-2B19: https://openairdocs.org/model/canadair-cl-600-2b19.md ## Service difficulty reports (20) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR VTZA200500110](https://openairdocs.org/sdr/VTZA200500110), Jun 14, 2005: DOOR FRAME. CRACKED. PASSENGER DOOR FRAME TOP RADIUS CRACKED AT 1 INCH IN LENGTH FORWARD OF DATUM 1 AT FS 338.90. - [SDR VTZA200500115](https://openairdocs.org/sdr/VTZA200500115), Jun 13, 2005: ANGLE. CRACKED. RIGHT 280 VERTICAL ANGLE IS CRACKED AT .5 INCH BETWEEN FASTENERS. - [SDR VTZA200500111](https://openairdocs.org/sdr/VTZA200500111), Jun 13, 2005: ANGLE. CRACKED. LEFT 280 VERTICAL ANGLE IS CRACKED AT .5 INCH BETWEEN FASTENERS. - [SDR VTZA200500113](https://openairdocs.org/sdr/VTZA200500113), Jun 13, 2005: BULKHEAD. CRACKED. RIGHT SIDE COPILOTS BULKHEAD AT FS 280 RBL 9.0 IS CRACKED AT 1.0 INCH IN WEB RADIUS. - [SDR VTZA200500112](https://openairdocs.org/sdr/VTZA200500112), Jun 13, 2005: RIB. CRACKED. LEFT BATT RIB IS CRACKED 1.5 INCH. - [SDR VTZA200500114](https://openairdocs.org/sdr/VTZA200500114), Jun 13, 2005: RIB. CRACKED. RIGHT BATT RIB IS CRACKED .750 INCH BETWEEN THE ATTACHING FASTENERS. - [SDR 05055628](https://openairdocs.org/sdr/05055628), Feb 24, 2005: CONTACTOR. FAILED. EVENT SUMMARY STATED 628BR RTF DUE TO ELECTRICAL FAILURE. REMOVED AND REPLACED ESS BUSS CONTACTOR & ADG AUTO DEPLOY CONTROL. - [SDR 05025628](https://openairdocs.org/sdr/05025628), Jan 25, 2005: ENGINE. SPLIT. EVENT SUMMARY STATED THAT 1 N2 SPLIT AFTER TAKEOFF, READ AS HIGH AS 2.2. ALL OTHER PARAMETERS MATCHED. REMOVED AND REPLACED ENG SPEED CONTROL PANEL IAW AMM 73-2 - [SDR 04235628](https://openairdocs.org/sdr/04235628), Aug 22, 2004: MOTOR. WEAK. CABIN DOOR HEAVY TO OPEN. REMOVED AND REPLACED PAX DOOR COUNTERBALANCES. DOOR ASSIST MOTOR WEAK. - [SDR 04127628](https://openairdocs.org/sdr/04127628), May 6, 2004: BULB. BURNED OUT. DURING INSPECTION THE NR 3 OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. THE AIRCRAF - [SDR 04035628](https://openairdocs.org/sdr/04035628), Feb 4, 2004: CONTROL UNIT. FAULTY. DURING APPROACH THE CREW REPORTED A FLAP SYSTEM FAILURE WITH FLAPS AT 0 DEGREE POSITION. FLIGHT LANDED UNEVENTFULLY AND PASSENGERS DEPLANED NORMALLY. THE FLAP E - [SDR 03301628](https://openairdocs.org/sdr/03301628), Oct 28, 2003: LANDING GEAR. CORRODED. DURING FLIGHT CREW RECEIVED A NOSE GEAR DISAGREE WARNING MESSAGE. UPON TROUBLESHOOTING ON GROUND THE NOSE LANDING GEAR ASSEMBLY WAS FOUND TO BE CORRODED AND GOU - [SDR 03268628](https://openairdocs.org/sdr/03268628), Sep 25, 2003: TIRE. SEPARATED. DURING LANDING THE NR 3 MAIN TIRE HAD TREAD SEPARATION. NO EMERGENCY DECLARED AIRCRAFT TAXIED TO GATE WITHOUT INCIDENT PASSENGERS WERE DEPLANED NORMALLY. MAINTE - [SDR 03265628](https://openairdocs.org/sdr/03265628), Sep 22, 2003: LIGHT. INOPERATIVE. DURING INSPECTION THE 2ND CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LIGHT BULB. A SATISFACTORY OPE - [SDR 03121628](https://openairdocs.org/sdr/03121628), May 1, 2003: BULB. BURNED OUT. DURING PREFLIGHT INSPECTION THE CREW DISCOVERED A CEILING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE PERSONNEL REPLACED A BULB AND PERFORMED A SATISFACTORY OPERAT - [SDR 03101628](https://openairdocs.org/sdr/03101628), Apr 11, 2003: BATTERY. INOPERATIVE. DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS WOULD NOT STAY ILLUMINATED. MAINTENANCE PERSONNEL REMOVED AND REPLACED THREE EMERG - [SDR 03088628](https://openairdocs.org/sdr/03088628), Mar 29, 2003: BULB. BURNED OUT. DURING MAINTENANCE INSPECTION, THE CABIN DOOR AND SERVICE DOOR EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED TH - [SDR 03086628](https://openairdocs.org/sdr/03086628), Mar 27, 2003: CONNECTOR. DAMAGED. DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY FLOOR TRACK AT SEAT ROW 1 WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE CONN - [SDR 02174628](https://openairdocs.org/sdr/02174628), Jun 23, 2002: MECHANISM. LACK OF LUBE. DURING TURN AROUND SERVICING, THE CREW NOTED THAT THE GALLEY SERVICE DOOR COULD NOT BE OPENED FROM THE OUTSIDE. MAINTENANCE PERSONNEL LUBRICATED THE GALLEY SERV - [SDR 02132628](https://openairdocs.org/sdr/02132628), May 12, 2002: LINE. FAILED. PASSING THROUGH 8000 FT IN THE CLIMB, THE CREW NOTED THE R ENG OIL PRESS RED WARNING ON THE EICAS. THE QRH WAS COMPLIED WITH, THE ENGINE WAS SHUT DOWN. THE AIRC --- 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.