# Service difficulty reports: N628BR, cancelled Dec 6, 2006 A list on [N628BR, cancelled Dec 6, 2006](https://openairdocs.org/deregistered/N628BR-2006-12-06.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR VTZA200500110](https://openairdocs.org/sdr/VTZA200500110.md): Door Frame · cracked · Jun 14, 2005 · N628BR · Cndair CL6002B19 · Fuselage Main, Structure > 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.md): Angle · cracked · Jun 13, 2005 · N628BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure > RIGHT 280 VERTICAL ANGLE IS CRACKED AT.5 INCH BETWEEN FASTENERS. - [SDR VTZA200500111](https://openairdocs.org/sdr/VTZA200500111.md): Angle · cracked · Jun 13, 2005 · N628BR · Cndair CL6002B19 · Fuselage Miscellaneous Structure > LEFT 280 VERTICAL ANGLE IS CRACKED AT.5 INCH BETWEEN FASTENERS. - [SDR VTZA200500113](https://openairdocs.org/sdr/VTZA200500113.md): Bulkhead · cracked · Jun 13, 2005 · N628BR · Cndair CL6002B19 · Fuselage Main, Bulkhead > 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.md): Rib · cracked · Jun 13, 2005 · N628BR · Cndair CL6002B19 · Wing, Rib/Bulkhead > LEFT BATT RIB IS CRACKED 1.5 INCH. - [SDR VTZA200500114](https://openairdocs.org/sdr/VTZA200500114.md): Rib · cracked · Jun 13, 2005 · N628BR · Cndair CL6002B19 · Wing, Rib/Bulkhead > RIGHT BATT RIB IS CRACKED.750 INCH BETWEEN THE ATTACHING FASTENERS. - [SDR 05055628](https://openairdocs.org/sdr/05055628.md): Contactor · failed · Feb 24, 2005 · N628BR · Cndair CL6002B19 · Electrical Power System Wiring > 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.md): Engine · split · Jan 25, 2005 · N628BR · Cndair CL6002B19 · Engine BMEP/Torque Indicating > 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 73-21-00. OPS CHECK GOOD. - [SDR 04235628](https://openairdocs.org/sdr/04235628.md): Motor · weak · Aug 22, 2004 · N628BR · Cndair CL6002B19 · Passenger/Crew Doors > CABIN DOOR HEAVY TO OPEN. REMOVED AND REPLACED PAX DOOR COUNTERBALANCES. DOOR ASSIST MOTOR WEAK. - [SDR 04127628](https://openairdocs.org/sdr/04127628.md): Bulb · burned out · May 6, 2004 · N628BR · Cndair CL6002B19 · Emergency Lighting > DURING INSPECTION THE NR 3 OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. THE AIRCRAFT WAS RETURNED TO SERVICE. - [SDR 04035628](https://openairdocs.org/sdr/04035628.md): Control Unit · faulty · Feb 4, 2004 · N628BR · Cndair CL6002B19 · Trailing Edge Flap Control System > DURING APPROACH THE CREW REPORTED A FLAP SYSTEM FAILURE WITH FLAPS AT 0 DEGREE POSITION. FLIGHT LANDED UNEVENTFULLY AND PASSENGERS DEPLANED NORMALLY. THE FLAP ELECTRONIC CONTROL UNIT WAS FOUND FAULTY AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFOR - [SDR 03301628](https://openairdocs.org/sdr/03301628.md): Landing Gear · corroded · Oct 28, 2003 · N628BR · Cndair CL6002B19 · Nose/Tail Landing Gear > 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 GOUGED. THE BRACKETS AND STRUCTURE ON WHICH THE PROXIMITY SENSORS WERE MOUNTED WERE ALSO FOUND CORROD - [SDR 03268628](https://openairdocs.org/sdr/03268628.md): Tire · separated · Sep 25, 2003 · N628BR · Cndair CL6002B19 · Tire > DURING LANDING THE NR 3 MAIN TIRE HAD TREAD SEPARATION. NO EMERGENCY DECLARED AIRCRAFT TAXIED TO GATE WITHOUT INCIDENT PASSENGERS WERE DEPLANED NORMALLY. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE NR 3 MAIN TIRE. - [SDR 03265628](https://openairdocs.org/sdr/03265628.md): Light · inoperative · Sep 22, 2003 · N628BR · Cndair CL6002B19 · Emergency Lighting > DURING INSPECTION THE 2ND CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE EMERGENCY LIGHT BULB. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. - [SDR 03121628](https://openairdocs.org/sdr/03121628.md): Bulb · burned out · May 1, 2003 · N628BR · Cndair CL6002B19 · Emergency Lighting > DURING PREFLIGHT INSPECTION THE CREW DISCOVERED A CEILING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE PERSONNEL REPLACED A BULB AND PERFORMED A SATISFACTORY OPERATIONAL CHECK. AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE. - [SDR 03101628](https://openairdocs.org/sdr/03101628.md): Battery · inoperative · Apr 11, 2003 · N628BR · Cndair CL6002B19 · Emergency Lighting > DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS WOULD NOT STAY ILLUMINATED. MAINTENANCE PERSONNEL REMOVED AND REPLACED THREE EMERGENCY EXIT LIGHT BATTERIES. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO - [SDR 03088628](https://openairdocs.org/sdr/03088628.md): Bulb · burned out · Mar 29, 2003 · N628BR · Cndair CL6002B19 · Emergency Lighting > DURING MAINTENANCE INSPECTION, THE CABIN DOOR AND SERVICE DOOR EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMPS IN THE EMERGENCY EXIT LIGHTS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS R - [SDR 03086628](https://openairdocs.org/sdr/03086628.md): Connector · damaged · Mar 27, 2003 · N628BR · Cndair CL6002B19 · Emergency Lighting > DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY FLOOR TRACK AT SEAT ROW 1 WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE CONNECTOR FOR THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RET - [SDR 02174628](https://openairdocs.org/sdr/02174628.md): Mechanism · lack of lube · Jun 23, 2002 · N628BR · Cndair CL6002B19 · Service Doors > DURING TURN AROUND SERVICING, THE CREW NOTED THAT THE GALLEY SERVICE DOOR COULD NOT BE OPENED FROM THE OUTSIDE. MAINTENANCE PERSONNEL LUBRICATED THE GALLEY SERVICE DOOR HANDLE OPERATING MECHANISM. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RE - [SDR 02132628](https://openairdocs.org/sdr/02132628.md): Line · failed · May 12, 2002 · N628BR · Cndair CL6002B19 · Engine Oil Distribution (Airframe Furnished) > 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 AIRCRAFT RETURNED TO CAE, AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL FOUND THE B-SUMP OIL LIN ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N628BR' AND deregistration_id = 'N628BR-2006-12-06' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N628BR-2006-12-06/reports --- 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.