# N638BR: Bombardier CL-600-2B19, registration cancelled 2011-07-18 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 18, 2011 - Status when cancelled: Valid registration - Airframe: [Bombardier CL-600-2B19](https://openairdocs.org/model/bombardier-cl-600-2b19) (registry code 1390008) - Data sheets: [TCDS A21EA-1](https://openairdocs.org/tcds/A21EA-1) (OpenAirDocs) - Serial number: 7311 - Type of aircraft: Fixed wing multi engine - Certificate issued: February 9, 2011 - Last registry action: February 9, 2011 - Mode S code: A85B9D - Owner when cancelled: [Trust N695br N696br N697br](https://openairdocs.org/faa-owner/TRUST%20N695BR%20N696BR%20N697BR) - 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/N638BR - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=638BR - Page: https://openairdocs.org/deregistered/N638BR-2011-07-18 From the FAA registry file of October 31, 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 (36) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CHQA200800210](https://openairdocs.org/sdr/CHQA200800210), Oct 23, 2008: OVERHEAT LOOP. MALFUNCTIONED. FLIGHT 5601, IAH TO JAX. DURING CLIMB THE FLIGHT CREW RECEIVED AN L JETPIPE OVHT FAIL CAUTION MESSAGE. THE MESSAGE APPEARED AND EXTINGUISHED SEVERAL TIMES. THE - [SDR CHQA200800147](https://openairdocs.org/sdr/CHQA200800147), Jul 16, 2008: UPLOCK SENSOR. OUT OF ADJUST. FLIGHT 5596, IAH TO BRO. AFTER TAKEOFF THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT WHEN THE GEAR WAS SELECTED UP. THE GEAR LEVER WAS MOVED BACK TO - [SDR CHQA200800113](https://openairdocs.org/sdr/CHQA200800113), Jun 15, 2008: INDICATION SYS. MALFUNCTIONED. FLIGHT 5534, IAH TO CRP. ON INITIAL CLIMBOUT THE FLIGHT CREW SELECTED THE LANDING GEAR TO THE UP POSITION AND THE NOSE AND RT LANDING GEAR INDICATED UP, BUT THE - [SDR CHQA200800052](https://openairdocs.org/sdr/CHQA200800052), Mar 15, 2008: CONNECTOR. LOOSE. MAF TO IAH - WHILE CLIMBING THROUGH 17,000 FT, THE CREW RECEIVED AT L REV UNLOCKED MESSAGE ON EICAS WITH A REV ICON ON THE N1 GAUGE. THERE WAS NO DEGRADATION OF - [SDR CHQA200800015](https://openairdocs.org/sdr/CHQA200800015), Jan 28, 2008: PSEU. FAULTED. CMH TO IAH - DURING TAKEOFF, CREW RECEIVED A WOW INPUT AND WOW OUTPUT EICAS MESSAGE. AFTER RUNNING THE APPROPRIATE QRH CHECKLISTS, IT WAS DECIDED TO DIVERT TO S - [SDR CHQA200800005](https://openairdocs.org/sdr/CHQA200800005), Jan 6, 2008: LINE. CRACKED. IAH TO CMH - DURING CLIMB, THE CREW RECEIVED A HYDRAULIC SYSTEM 2 FAIL MESSAGE THEN CONFIRMED THAT THE SYSTEM 2 QUANTITY WAS ZERO. THE AIRCRAFT RETURNED TO FIEL - [SDR CHQA20070043](https://openairdocs.org/sdr/CHQA20070043), Aug 31, 2007: TRIM SWITCH. MALFUNCTIONED. IAH TO SDF - WHILE CLIMBING THROUGH 12,000FT EXPERIENCED A NOSE DOWN PITCH TRIM RUNAWAY. ACCOMPLISHED PITCH TRIM RUNAWAY MEMORY ITEMS AND DECLARED AN EMERGENCY. - [SDR CHQA200700035](https://openairdocs.org/sdr/CHQA200700035), Jul 14, 2007: PDU. INOPERATIVE. FLIGHT 3203 - CMH-IAH - AT FL360, EXPERIENCED AN UNCOMMANDED FLAP DEPLOYMENT OF UP TO 8 DEGREES IN FLIGHT WITH THE FLAP SELECTOR IN THE 0 DEGREE POSITION. IMMED - [SDR VTZA200500044](https://openairdocs.org/sdr/VTZA200500044), Apr 1, 2005: INTERCOSTAL. CRACKED. INTERCOSTAL CRACKED AT .250 INCH IN LENGTH ON LEFT INBOARD SIDE AT FS 484 AT BL 36.00. - [SDR VTZA200500043](https://openairdocs.org/sdr/VTZA200500043), Apr 1, 2005: INTERCOSTAL. CRACKED. INTERCOSTAL CRACKED AT .250 INCH IN LENGTH ON RIGHT INBOARD SIDE AT FS 484 AT BL 36.00. - [SDR VTZA200500042](https://openairdocs.org/sdr/VTZA200500042), Apr 1, 2005: INTERCOSTAL. CRACKED. INTERCOSTAL CRACKED AT .250 INCH IN LENGTH ON RIGHT OUTBOARD SIDE AT FS 484 AT BL 27.00. - [SDR VTZA200500036](https://openairdocs.org/sdr/VTZA200500036), Mar 31, 2005: BULKHEAD. CRACKED. RIGHT SIDE PILOTS BULKHEAD AT FS 280 RBL 9.0 IS CRACKED AT 1 INCH IN WEB RADIUS. - [SDR VTZA200500035](https://openairdocs.org/sdr/VTZA200500035), Mar 31, 2005: BULKHEAD. CORRODED. BULKHEAD AT FS 280 BETWEEN RBL 9.0 AND LBL 9.0 HAS LEVEL 2 CORROSION ON WEB .020 INCH DEEP. - [SDR VTZA200500033](https://openairdocs.org/sdr/VTZA200500033), Mar 31, 2005: SUPPORT BEAM. CRACKED. LEFT ENGINE SUPPORT BEAM IS CRACKED IN LOWER WEB AT .75 INCH. - [SDR VTZA200500031](https://openairdocs.org/sdr/VTZA200500031), Mar 31, 2005: INTERCOSTAL. CRACKED. PAX DOOR INTERCOSTAL TOP RADIUS CRACKED AT 1 INCH IN LENGTH AT DATUM 1 FS 338. - [SDR VTZA200500030](https://openairdocs.org/sdr/VTZA200500030), Mar 31, 2005: ANGLE. CRACKED. LEFT 280 VERTICAL ANGLE IS CRACKED AT .5 INCH BETWEEN FASTENERS. - [SDR VTZA200500034](https://openairdocs.org/sdr/VTZA200500034), Mar 31, 2005: FRAME. CRACKED. RIGHT FS 640 FRAME DOUBLER IS CRACKED IN RADIUS AT 1 INCH IN LENGTH. - [SDR VTZA200500032](https://openairdocs.org/sdr/VTZA200500032), Mar 31, 2005: RIB. CRACKED. LEFT BATTERY RIB IS CRACKED 1.5 INCH. - [SDR VTZA200500041](https://openairdocs.org/sdr/VTZA200500041), Mar 31, 2005: ANGLE. CRACKED. RT OBLIQUE ANGLE IS CRACKED AT 1 INCH IN RADIUS. - [SDR VTZA200500040](https://openairdocs.org/sdr/VTZA200500040), Mar 31, 2005: ANGLE. CRACKED. LEFT 624 OBLIQUE ANGLE IS CRACKED AT 1 INCH IN LENGTH. - [SDR VTZA200500039](https://openairdocs.org/sdr/VTZA200500039), Mar 31, 2005: FRAME. CRACKED. LEFT FS 640 FRAME DOUBLER IS CRACKED IN RADIUS AT 1 INCH IN LENGTH. - [SDR VTZA200500038](https://openairdocs.org/sdr/VTZA200500038), Mar 31, 2005: RIB. CRACKED. RIGHT BATTERY RIB IS CRACKED .750 INCH BETWEEN THE ATTACHING FASTENERS. - [SDR VTZA200500037](https://openairdocs.org/sdr/VTZA200500037), Mar 31, 2005: ANGLE. CRACKED. RIGHT 280 VERTICAL ANGLE IS CRACKED AT .5 INCH BETWEEN FASTENERS. - [SDR 050606394](https://openairdocs.org/sdr/050606394), Mar 1, 2005: ANGLE. CRACKED. LEFT 624 OBLIQUE ANGLE IS CRACKED AT 1 INCH IN RADIUS. - [SDR 04165638](https://openairdocs.org/sdr/04165638), Jun 13, 2004: BATTERY. DISCHARGED. DURING INSPECTION THE FORWARD EMERGENCY LIGHTS WERE FOUND DIM. THE BATTERY WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNE - [SDR 04132638](https://openairdocs.org/sdr/04132638), May 11, 2004: BULB. BURNED OUT. DURING INSPECTION AN OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS - [SDR 04038638](https://openairdocs.org/sdr/04038638), Feb 7, 2004: COMPUTER. FAULTY. DURING APPROACH CREW REPORTED A STALL SYSTEM FAILURE WHEN FLAPS WERE SELECTED TO 8 DEGREES. THE STALL COMPUTER WAS FOUND FAULTY AND REPLACED. A SATISFACTORY OPE - [SDR 03338638](https://openairdocs.org/sdr/03338638), Dec 4, 2003: LIGHT. INOPERATIVE. DURING INSPECTION THE LT EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND TO BE INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERF - [SDR 03289638](https://openairdocs.org/sdr/03289638), Oct 16, 2003: LIGHT. INOPERATIVE. DURING INSPECTION THE NR 2 CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. - [SDR 03284638](https://openairdocs.org/sdr/03284638), Oct 11, 2003: WIRE. LOOSE. DURING INSPECTION THE OVERHEAD EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE BULB AS WELL AS REPAIRED A WIRE TO THE LI - [SDR 03236638](https://openairdocs.org/sdr/03236638), Aug 24, 2003: LIGHT. INOPERATIVE. DURING MAINTENANCE INSPECTION THE EMERGENCY TRACK LIGHTING IN ROWS 2-5 WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE ROW 2-5 EMERGENCY E - [SDR 03153638](https://openairdocs.org/sdr/03153638), Jun 2, 2003: SEAL. LEAKING. DURING CRUISE, THE CREW REPORTED A LOUD WHISTLING NOISE FROM THE RT FRONT OF THE AIRCRAFT. THE FLIGHT DIVERTED TO ORF AND LANDED WITHOUT INCIDENT. MAINTENANCE P - [SDR 03101638A](https://openairdocs.org/sdr/03101638A), Apr 11, 2003: LAMP. INOPERATIVE. DURING MAINTENANCE INSPECTION, THE RT EXTERIOR OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN - [SDR 03101638](https://openairdocs.org/sdr/03101638), Apr 11, 2003: LIGHT. INOPERATIVE. DURING MAINTENANCE INSPECTION, THE EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL CLEANED THE CONNECTOR FOR THE EMERGENCY FLOO - [SDR 02035638](https://openairdocs.org/sdr/02035638), Feb 4, 2002: LAMP. During maintenance inspection, it was discovered that the aft emergency flood light was inoperative. Maintenance personnel removed and replaced the lamp in the - [SDR VTZA990071](https://openairdocs.org/sdr/VTZA990071), May 8, 1999: HOSE. LEAKING. ORD/SGE - FLT 7621 - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO NR 1 HYDRAULIC SYSTEM FAILURE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEM ## 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 20030715013659I](https://openairdocs.org/incident/20030715013659I), Jul 15, 2003: Cndair CL6002B19 (N638BR), Kansas City, MO. (-23) On July 15, 2003 united express N638BR flt 783 (a/c operated by atlantic coast airlines) a CL-600 advised ATC of a cargo compartment low caution message,… --- 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.