N638BR, cancelled Jul 18, 2011

Service difficulty reports · 36

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

Query with SQL
duckdb -csv -c "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 = 'N638BR' AND deregistration_id = 'N638BR-2011-07-18'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR CHQA200800210Overheat Loop · malfunctionedFLIGHT 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 QRH CHECKLISTS WERE FOLLOWED AND A L JETPIPE OVERHEAT MESSAGE APPEARED ALONG WITH THE TRIPLE CHIMOct 23, 2008 · N638BR · Cndair CL6002B19 · Overheat DetectionSDR CHQA200800147Uplock Sensor · out of adjustFLIGHT 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 THE DOWN POSITION AND THE LT MAIN LANDING GEAR INDICATED A RED UNSAFE CONDITION. THE GEAR FINALLJul 16, 2008 · N638BR · Cndair CL6002B19 · Landing Gear Position and WarningSDR CHQA200800113Indication Sys · malfunctionedFLIGHT 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 LT MAIN SHOWED A RED UNSAFE INDICATION. THIS WAS PRECEDED BY A RED DISAGREE MESSAGE. THE CREW FOJun 15, 2008 · N638BR · Cndair CL6002B19 · Landing Gear Position and WarningSDR CHQA200800052Connector · looseMAF 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 AIRCRAFT PERFORMANCE NOTED. THE CREW PERFORMED THE APPROPRIATE CHECKLISTS AND RETURNED TO MAF. MMar 15, 2008 · N638BR · Cndair CL6002B19 · Engine Exhaust System WiringSDR CHQA200800015Pseu · faultedCMH 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 SDF WHERE THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE INTERROGATED THE PSEU FOR FAULT CODES WHIJan 28, 2008 · N638BR · Cndair CL6002B19 · Landing Gear Position and WarningSDR CHQA200800005Line · crackedIAH 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 FIELD AT IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE HYDRAULIC SYSTEM AND FOUND A HAIRLJan 6, 2008 · N638BR · Cndair CL6002B19 · Hydraulic System, MainSDR CHQA20070043Trim Switch · malfunctionedIAH TO SDF - WHILE CLIMBING THROUGH 12,000FT EXPERIENCED A NOSE DOWN PITCH TRIM RUNAWAY. ACCOMPLISHED PITCH TRIM RUNAWAY MEMORY ITEMS AND DECLARED AN EMERGENCY. LANDED IN IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN'S PITCH TRIM SWITCHAug 31, 2007 · N638BR · Bombdr CL6002D15 · Stabilizer Control SystemSDR CHQA200700035Pdu · inoperativeFLIGHT 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. IMMEDIATELY REDUCED AIRSPEED AND INITIATED A DESCENT TO 15,000 FEET. IN DESCENT, THE FLAPS CONTINUED TOJul 14, 2007 · N638BR · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VTZA200500044Intercostal · crackedINTERCOSTAL CRACKED AT .250 INCH IN LENGTH ON LEFT INBOARD SIDE AT FS 484 AT BL 36.00.Apr 1, 2005 · N638BR · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VTZA200500043Intercostal · crackedINTERCOSTAL CRACKED AT .250 INCH IN LENGTH ON RIGHT INBOARD SIDE AT FS 484 AT BL 36.00.Apr 1, 2005 · N638BR · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VTZA200500042Intercostal · crackedINTERCOSTAL CRACKED AT .250 INCH IN LENGTH ON RIGHT OUTBOARD SIDE AT FS 484 AT BL 27.00.Apr 1, 2005 · N638BR · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VTZA200500036Bulkhead · crackedRIGHT SIDE PILOTS BULKHEAD AT FS 280 RBL 9.0 IS CRACKED AT 1 INCH IN WEB RADIUS.Mar 31, 2005 · N638BR · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VTZA200500035Bulkhead · corrodedBULKHEAD AT FS 280 BETWEEN RBL 9.0 AND LBL 9.0 HAS LEVEL 2 CORROSION ON WEB .020 INCH DEEP.Mar 31, 2005 · N638BR · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VTZA200500033Support Beam · crackedLEFT ENGINE SUPPORT BEAM IS CRACKED IN LOWER WEB AT .75 INCH.Mar 31, 2005 · N638BR · Cndair CL6002B19 · Fuselage, Landing Gear Attach FittingsSDR VTZA200500031Intercostal · crackedPAX DOOR INTERCOSTAL TOP RADIUS CRACKED AT 1 INCH IN LENGTH AT DATUM 1 FS 338.Mar 31, 2005 · N638BR · Cndair CL6002B19 · Passenger/Crew DoorsSDR VTZA200500030Angle · crackedLEFT 280 VERTICAL ANGLE IS CRACKED AT .5 INCH BETWEEN FASTENERS.Mar 31, 2005 · N638BR · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VTZA200500034Frame · crackedRIGHT FS 640 FRAME DOUBLER IS CRACKED IN RADIUS AT 1 INCH IN LENGTH.Mar 31, 2005 · N638BR · Cndair CL6002B19 · Fuselage Main, FrameSDR VTZA200500032Rib · crackedLEFT BATTERY RIB IS CRACKED 1.5 INCH.Mar 31, 2005 · N638BR · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR VTZA200500041Angle · crackedRT OBLIQUE ANGLE IS CRACKED AT 1 INCH IN RADIUS.Mar 31, 2005 · N638BR · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VTZA200500040Angle · crackedLEFT 624 OBLIQUE ANGLE IS CRACKED AT 1 INCH IN LENGTH.Mar 31, 2005 · N638BR · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VTZA200500039Frame · crackedLEFT FS 640 FRAME DOUBLER IS CRACKED IN RADIUS AT 1 INCH IN LENGTH.Mar 31, 2005 · N638BR · Cndair CL6002B19 · Fuselage Main, FrameSDR VTZA200500038Rib · crackedRIGHT BATTERY RIB IS CRACKED .750 INCH BETWEEN THE ATTACHING FASTENERS.Mar 31, 2005 · N638BR · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR VTZA200500037Angle · crackedRIGHT 280 VERTICAL ANGLE IS CRACKED AT .5 INCH BETWEEN FASTENERS.Mar 31, 2005 · N638BR · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR 050606394Angle · crackedLEFT 624 OBLIQUE ANGLE IS CRACKED AT 1 INCH IN RADIUS.Mar 1, 2005 · N638BR · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR 04165638Battery · dischargedDURING INSPECTION THE FORWARD EMERGENCY LIGHTS WERE FOUND DIM. THE BATTERY WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE.Jun 13, 2004 · N638BR · Cndair CL6002B19 · Emergency LightingSDR 04132638Bulb · burned outDURING INSPECTION AN OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE.May 11, 2004 · N638BR · Cndair CL6002B19 · Emergency LightingSDR 04038638Computer · faultyDURING APPROACH CREW REPORTED A STALL SYSTEM FAILURE WHEN FLAPS WERE SELECTED TO 8 DEGREES. THE STALL COMPUTER WAS FOUND FAULTY AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE.Feb 7, 2004 · N638BR · Cndair CL6002B19 · Stall Warning SystemSDR 03338638Light · inoperativeDURING INSPECTION THE LT EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND TO BE INOPERATIVE AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE.Dec 4, 2003 · N638BR · Cndair CL6002B19 · Emergency LightingSDR 03289638Light · inoperativeDURING INSPECTION THE NR 2 CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE.Oct 16, 2003 · N638BR · Cndair CL6002B19 · Emergency LightingSDR 03284638Wire · looseDURING INSPECTION THE OVERHEAD EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE BULB AS WELL AS REPAIRED A WIRE TO THE LIGHT ASSEMBLY. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUOct 11, 2003 · N638BR · Cndair CL6002B19 · Light System WiringSDR 03236638Light · inoperativeDURING MAINTENANCE INSPECTION THE EMERGENCY TRACK LIGHTING IN ROWS 2-5 WAS FOUND INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE ROW 2-5 EMERGENCY ESCAPE PATH LIGHTING STRIP. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASEAug 24, 2003 · N638BR · Cndair CL6002B19 · Emergency LightingSDR 03153638Seal · leakingDURING 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 PERSONNEL REMOVED AND REPLACED THE SERVICE DOOR SEAL. PRESSURIZATION AND OPERATIONAL CHECKS WERE SJun 2, 2003 · N638BR · Cndair CL6002B19 · Service DoorsSDR 03101638ALamp · inoperativeDURING MAINTENANCE INSPECTION, THE RT EXTERIOR OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO Apr 11, 2003 · N638BR · Cndair CL6002B19 · Emergency LightingSDR 03101638Light · inoperativeDURING MAINTENANCE INSPECTION, THE EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL CLEANED THE CONNECTOR FOR THE EMERGENCY FLOOR TRACK LIGHTS. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE.Apr 11, 2003 · N638BR · Cndair CL6002B19 · Emergency LightingSDR 02035638LampDuring maintenance inspection, it was discovered that the aft emergency flood light was inoperative. Maintenance personnel removed and replaced the lamp in the aft emergency flood light. An operational check was satisfactory and the aircraft was returned to Feb 4, 2002 · N638BR · Cndair CL6002B19 · Emergency LightingSDR VTZA990071Hose · leakingORD/SGE - FLT 7621 - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO NR 1 HYDRAULIC SYSTEM FAILURE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED FLEXIBLE PRESSURE LINE, OPS CHECK OK. AIRCRAFT WAS RELEASED AMay 8, 1999 · N638BR · Cndair CL6002B19 · Hydraulic System, Main
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