N463CA, cancelled Sep 6, 2013

Service difficulty reports · 92

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 = 'N463CA' AND deregistration_id = 'N463CA-2013-09-06'
  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 COMA0210027Roller · wornFLIGHT 6043 FLAP DISAGREEMENT WARNING AFTER T/O.REPLACED WORN ROLLERS ON R/H OUTBD FLAP.Jun 17, 2002 · N463CA · Emb EMB120RT · Trailing Edge Flap Control SystemSDR COMA0210026GeneratorFLIGHT 5067 #1 GENERATOR FAILED AFTER T/O.DEFERRED MAINT ON #1 GENERATOR PER MEL.Jun 15, 2002 · N463CA · Emb EMB120RT · DC Generating SystemSDR COMA0210022EngineFLIGHT 5067 - DURING CRUISE FLIGHT, DESTINATION EYW THE RIGHT ENGINE WAS SHUT DOWN DUE TO LOSS OF OIL PRESSURE.REPLACED THE RIGHT ENGINE ASSEMBLY DUE TO HOT SECTION FAILURE.May 23, 2002 · N463CA · Emb EMB120RT · Turbine Engine Combustion SectionSDR COMA0210013Valve · malfunctionedFLIGHT 5069 CABIN VERY HOT A/C SYSTEM NOT WORKING.REPLACED THE L/H TEMP CONTROL VALVE.Apr 7, 2002 · N463CA · Emb EMB120RT · Cabin Cooling SystemSDR COMA0110159GyroFLIGHT #5049 - AFTER T/O, RED FD FLAP ON PILOTS AND COPILOTS EADI.COULD NOT DUPLICATE. SYSTEM TEST WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.Dec 3, 2001 · N463CA · Emb EMB120RT · Autopilot SystemSDR COMA0110145Circuit BreakerFLIGHT #5057. DURING PRE-FLIGHT CREW DISCOVERED THE CIRCUIT BREAKER FOR THE FLIGHT IDLE STOP SOLENOID TRIPPED.PERFOMRED RESET AND OPERATIONAL CHECK OF THE FLIGHT IDLE STOP CIRCUIT BREAKER.Sep 25, 2001 · N463CA · Emb EMB120RT · Battery Overheat Warning SystemSDR COMA0110143Indicator · faultyFLIGHT #5017. DURING TAKE OFF AT MCO THE LEFT ENGINE DIGITAL TORQUE INDICATION WAS INTERMITTENT, TAKE OFF WAS ABORTED AND REUTRNED TO THE GATE.REPLACED THE LEFT ENGINE TORQUE GAUGE.Sep 22, 2001 · N463CA · Emb EMB120RT · Power Indicating SystemSDR COMA0110137Computer · faultyFLIGHT #5005. DURING TAXI OUT RECEIVED A HEADING COMPUTER WARNING, AIRCRAFT RETURNED TO THE GATE.REPLACED THE AHC-85.Aug 29, 2001 · N463CA · Emb EMB120RT · Attitude and Direction Data SystemSDR COMA0110130Sill · corrodedDURING 2C-CHECK TASK 141-01Z, THE AFT LEFT FLOOR SUPPORT SILL INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110129Skin · gougedDURING 2 YEAR CORROSION CHECK TASK 5310-132-C01E, THE LOWER RH FUSELAGE SKIN WAS FOUND GOUGED JUST BELOW THE LAV DUMP VALVE DOUBLER. THE SKIN WAS REPAIRED PER EMBRAER SRM STANDARD PRACTICES AND REPAIR FAX GST-0992/01, DATED 3/28/01.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Main, Plate/SkinSDR COMA0110128Stringer · dentedDURING 2C-CHECK TASK 5410-442-04I, THE RIGHT NACELLE OUTBOARD STRINGER NR 1 WAS FOUND TO BE DENTED BY THE GEAR DOOR TENSIONER. THE STRINGER WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES AND EMBRAER REPAIR GST-1034/01, DATED 3/30/01.Apr 18, 2001 · N463CA · Emb EMB120RT · Nacelle/Pylon, Longeron/StringerSDR COMA0110127Support · crackedDURING 2C-CHECK TASK 5710-652-01I, THE RIGHT WING UPPER SKIN SUPPORT ON RIB NR 21, BETWEEN STRINGERS NR 2 AND 3, WAS FOUND TO BE CRACKED. THE SKIN SUPPORT WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Wing Miscellaneous StructureSDR COMA0110126Skin · crackedDURING 2C-CHECK (NO SPECIFIC TASK APPLIES), THE LEFT NACELLE FLAP LOWER SKIN WAS FOUND TO BE CRACKED AT ACCESS PANEL NR 436AB CUTOUT. THE NACELLE FLAP WAS REMOVED AND REPLACED PER EMB-120 MM 27-50-03.Apr 18, 2001 · N463CA · Emb EMB120RT · Trailing Edge FlapsSDR COMA0110125Support · crackedDURING 2C-CHECK 5720-552-01I, THE LEFT WING UPPER SKIN SUPPORT AT RIB NR 21, BETWEEN FRONT SPAR AND STRINGER NR 2, WAS FOUND TO BE CRACKED. THE SKIN SUPPORT WAS REMOVED AND REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Wing Miscellaneous StructureSDR COMA0110124Support · crackedDURING 2C-CHECK 5720-552-01I, THE LEFT WING UPPER SKIN SUPPORT AT RIB 21, BETWEEN STRINGER NR 2 AND 3, WAS FOUND TO BE CRACKED. THE SKIN SUPPORT WAS REMOVED AND REPLACED PER EMB-120 SRM STANDRAD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Wing Miscellaneous StructureSDR COMA0110123Floor Support · crackedDURING 2C-CHECK TASK 5310-121-01I, THE LEFT FUSELAGE FLOOR PROP AT FRAME NR 13 WAS FOUND TO BE CRACKED. THE FLOOR PROP WAS REPAIRED PER EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 3647-1, REV IR, 5-3-00.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110122Floor Support · crackedDURING 2C-CHECK TASK 5310-122-01I, THE RIGHT FUSELAGE FLOOR PROP AT FRAME NR 13 WAS FOUND TO BE CRACKED. THE FLOOR PROP WAS REPAIRED PER EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 3647-1, REV IR, 5-3-00.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110121Angle · crackedDURING 2C-CHECK TASK 5320-243-01I, THE LEFT WING UPPER SKIN ATTACH ANGLE FOR FAIRING NR 193 WAS FOUND TO BE CRACKED. THE ANGLE WAS REPAIRED PER EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 1126-21, REV IR, 7/6/99.Apr 18, 2001 · N463CA · Emb EMB120RT · Wing Miscellaneous StructureSDR COMA0110120Shear Tie · crackedDURING 2C-CHECK TASK 232-01Z, THE RIGHT FUSELAGE SKIN SUPPORT AT FRAME NR 13A AND STRINGER NR 14R, WAS FOUND TO BE CRACKED. THE SUPPORT WAS REPAIRED PER EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 3653-2, REV IR, 11/7/00.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0110119Shear Tie · crackedDURING 2C-CHECK TASK 221-01Z, THE LEFT FUSELAGE SKIN SUPPORT JUST BEHIND CAPTAIN''S DV WINDOW, BETWEEN FRAMES 12A AND 23, WAS FOUND TO BE CRACKED. THE SUPPORT WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0110118Bracket · crackedDURING 2C-CHECK TASK 262-01Z, THE AFT CARGO DOOR TRACK UPPER MOUNTING BRACKET WAS FOUND TO BE CRACKED. THE BRACKET WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 1657-3, REV IR, 6/12/00.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110117Channel · crackedDURING 2C-CHECK TASK 811-02Z, THE CHANNEL INSIDE THE PASSENGER DOOR WAS FOUND TO BE CRACKED. THE CHANNEL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Passenger/Crew DoorsSDR COMA0110116Shear Tie · crackedDURING 2C-CHECK TASK 221-01Z, THE FUSLEAGE SKIN SUPPORT ON LEFT SIDE OF COCKPIT AT FRAME NR 9 WAS FOUND TO BE CRACKED. THE SKIN SUPPORT WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 660-1, REV IR, 2/16/93.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0110115Shear Tie · crackedDURING 2C-CHECK TASK 222-01Z, THE FUSELAGE SKIN SUPPORT ON RIGHT SIDE OF COCKPIT AT FRAME NR 9 WAS FOUND TO BE CRACKED. THE SKIN SUPPORT WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 660-1, REV IR, 2/16/93.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0110114Channel · crackedDURING 2C-CHECK TASK 811-02Z, THE U-CHANNEL INSIDE THE PASSENGER DOOR WAS FOUND TO BE CRACKED. THE CHANNEL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Passenger/Crew DoorsSDR COMA0110113Sill · corrodedDURING 2-C CHECK TASK 164-01Z, THE AFT RIGHT FLOOR SUPPORT SILL INSIDE THE CARGO COMPARTMENT WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 3661-1, REV IR, 5/15/00.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110112Sill · corrodedDURING 2C-CHECK TASK 162-01Z, THE FORWARD RIGHT FLOOR SUPPORT SILL INSIDE THE CARGO COMPARTMENT WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110111Strap · corrodedDURING 2-C CHECK TASK 152-01Z, THE AFT RIGHT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110110Strap · corrodedDURING 2-C CHECK TASK 152-01Z, THE AFT RIGHT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110109Strap · corrodedDURING 2C-CHECK TASK 151/152-01Z, THE AFT CENTER FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110108Strap · corrodedDURING 2C-CHECK TASK 151-01Z, THE AFT LEFT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110107Strap · corrodedDURING 2C-CHECK TASK 141-01Z, THE LEFT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110106Strap · corrodedDURING 2C-CHECK TASK 141-01Z, THE LEFT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110105Strap · corrodedDURING 2C-CHECK TASK 142-01Z, THE RIGHT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110104Strap · corrodedDURING 2C-CHECK TASK 142-01Z, THE RIGHT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EM-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110103Sill · corrodedDURING 2C-CHECK TASK 142-01Z, THE RIGHT FLOOR SUPPORT SILL INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110102Sill · corrodedDURING 2C-CHECK TASK 142-01Z, THE RIGHT FLOOR SUPPORT SILL INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110101Support · corrodedDURING 2C-CHECK TASK 243-01Z, THE LEFT SIDEWALL SUPPORT SECTION INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SUPPORTING SECTION WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110100Strap · corrodedDURING 2C-CHECK TASK 132-01Z, THE RIGHT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110099Strap · corrodedDURING 2C-CHECK TASK 131/132-01Z, THE CENTER FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110098Strap · corrodedDURING 2C-CHECK TASK 131-01Z, THE LEFT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110097Strap · corrodedDURING 2C-CHECK TASK 131-01Z, THE FORWARD LEFT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER SRM STANDARD PRACTICES AND AERODESIGN REPORT 1671-2, REV IR 12/4/96.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110096Strap · corrodedDURING 2C-CHECK TASK 131/132-01Z, THE FORWARD CENTER FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PRACTICE AND AERODESIGN REPORT 1671-1, REV A, 1/28/97.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110095Sill · corrodedDURING 2C-CHECK TASK 132-01Z, THE FOWARD RIGHT FLOOR SUPPORT SILL INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110094Support · corrodedDURING 2C-CHECK TASK 232-01Z, THE FORWARD RIGHT SIDEWALL SEAT TRACK SUPPORT INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SUPPORT WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110093Support · corrodedDURING 2C-CHECK TASK 242-01Z, THE RIGHT SIDEWALL SEAT TRACK SUPPORT INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SUPPORT WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110092Floorbeam · corrodedDURING 2C-CHECK TASK 131-01Z, THE FORWARD LEFT FLOOR SUPPORT T-SECTION AT FRAME 16 INSIDE THE CABIN ,WAS FOUND TO BE CORRODED. THE T-SECTION WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA0110091Crossbeam · corrodedDURING 2C-CHECK TASK 151-01Z, THE LEFT FLOOR SUPPORT CROSSBEAM AT FRAME 36, INSIDE THE CABIN, WAS FOUND TO BE CORRODED. THE CROSSBEAM WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0110090Door Frame · corrodedDURING 2C-CHECK TASK 811-02Z, THE PASSENGER DOOR LOWER LONGITUDINAL FRAME, WAS FOUND TO BE CORRODED. THE FRAME WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Passenger/Crew DoorsSDR COMA0110089Angle · corrodedDURING 2C-CHECK TASK 131/132-01Z, THE FUSELAGE FORWARD FLOOR SUPPORTING Z-SECTION AT FRAME 13 WAS FOUND TO BE CORRODED. THE Z-SECTION WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES.Apr 18, 2001 · N463CA · Emb EMB120RT · Fuselage Miscellaneous Structure
Back to N463CA, cancelled Sep 6, 2013