N462CA, cancelled Sep 3, 2013
Service difficulty reports · 88
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 = 'N462CA' AND deregistration_id = 'N462CA-2013-09-03' 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.
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 = 'N462CA' AND deregistration_id = 'N462CA-2013-09-03' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FXGA20101214001Skin · chafedFUSELAGE SKIN CHAFED BY A FLEX DUCT AT FRAME 30(F/S 10172) AND STRINGER L18. REPAIRED IAW SRM 53-00-01.SDR COMA0210024Brake AssyFLIGHT 5064 DURING LANDING ALL 4 MLG TIRES BLEW OUT. REPLACED 4 MLG BRAKE ASSY, 4 MLG WHEEL AND TIRES. REPLACED BOTH BRAKE CONTROL VALVES FOR PREVENTIVE MAINT. & ANTI SKID CONTROL BOX - CAUSE OF LOCK UP UNDETERMINED.SDR COMA0210014Bracket · crackedDUIRNG A 2,000 FLIGHT CYCLE INSPECTION, THE FUEL SHUT-OFF SUPPORT BRACKET (P/N 120-24373-002) ON THE RIGHT WING BOX FORWARD SIDE AFT OF FRAME 10 WAS FOUND TO BE CRACKED.THE CRACKED BRACKET (P/N 120-24373-002) WAS REMOVED FROM THE AIRCRAFT, REPAIRED AND RE-INSTSDR COMA0110161Gauge · malfunctionedFLIGHT 5070 R/H ENGINE TORQUE GAUGE FAILED DURING T/O.REPLACED THE TORQUE INDICATOR.SDR COMA0110132Light · brokenEMERGENCY LIGHT AT ROW 5 IS BROKEN.REPLACED LIGHT ASSY.SDR COMA0110081Floor Support · crackedDURING 2C CHECK TASK 121-01Z, THE FUSELAGE LT FLOOR PROP AT FRAME 13 WAS FOUND CRACKED. THE PART WAS REPAIRED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 3647-1, REV IR, 5-3-00.SDR COMA0110080Strap · corrodedDURING 2C CHECK TASK 141-01Z, THE FUSELAGE LT FLOORBEAM BUTT STRAP WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 2174-1, REV IR, 1-15-97.SDR COMA0110079Crossbeam · corrodedDURING 2C CHECK TASK 131-01Z, THE FUSELAGE LT FLOOR CROSSBEAM AT FRAME 15 WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110078Floorbeam · corrodedDURING 2C CHECK TASK 152-01Z, THE FUSELAGE RT FLOOR T-SECTION AT FRAME 36 WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110077Support · crackedDURING 2C CHECK TASK 5720-552-01I, THE LT WING UPPER SKIN SUPPORT AT RIB 21, BETWEEN FR ON SPAR AND STRINGERS 2A, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110076Support · crackedDURING 2C CHECK TASK 5720-552-01I, THE LT WING SUPPER SKIN SUPPORT AT RIB 20, BETWEEN STRINGERS 2A AND 3A, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110075Support · crackedDURING 2C CHECK TASK 5720-552-01I, THE LT WING UPPER SUPPORT AT RIB 20, BETWEEN STRINGERS 3A AND 4A, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRCTICES.SDR COMA0110074Support · crackedDURING 2C CHECK TASK 232-01Z, THE FUSELAGE RT SKIN SUPPORT AT FRAME 13A, STRINGER 14R WAS FOUND CRACKED. THE PART WAS REPAIRED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 3653-2, REV IR, 11-7-00.SDR COMA0110073Support · crackedDURING 2C CHECK TASK 5310-221-05I, THE FUSELAGE LT SKIN SUPPORT BEHIND THE CAPTAIN''S DV WINDOW, BETWEEN FRAMES 12A AND 13, WAS FOUND CRCKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110072Support · crackedDURING 2C CHECK TASK 5310-221-05I, THE FUSELAGE LT SKIN SUPPORT BEHIND AND ABOVE THE CAPTAIN''S DV WINDOW, BETWEEN FRAMES 12A AND 13, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110071Support · crackedDURING 2C CHECK TASK 261-01Z, THE FUSELAGE LT SKIN SUPPORT AT FRAME 40, BETWEEN STRINGERS 3L AND 4L, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110070Frame · gougedDURING 2C CHECK TASK 163-01Z, THE FUSELAGE FRAME 46A WAS FOUND TO BE GOUGED BY AN INTERIOR LINING SCREW AT FLOOR LEVEL ON THE LEFT SIDE. THE FRAME WAS REPAIRED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 2400=5, REV IR, 3-5-01.SDR COMA0110069Strap · corrodedDURING 2C CHECK TASK 162-01Z, THE FORWARD RT FLOORBEAM BUTTSTRAP IN THE CARGO COMPARTMENT, WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110068Stringer · crackedDURING 2C CHECK TASK 5410-432-04I, THE LEFT NACELLE OUTBOARD STRINGER NR 1 WAS FOUND TO BE CRACKED JUST AFT OF NACELLE FRAME 10. THE STRINGER WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110067Strap · corrodedDURING 2C CHECK TASK 142-01Z, THE RT FLOORBEAM BUTTSTRAP WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 2174-1, REV IR, 1-15-97.SDR COMA0110066Floorbeam · corrodedDURING 2C CHECK TASK 131-01Z, THE FUSELAGE LT FLOORBEAM T-SECTION AT FRAME 16 WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110065Skin · gougedDURING 2 YEAR CORROSION CHECK TASK 5310-132-CO1E, THE FUSELAGE LOWER SKIN WAS FOUND TO BE GOUGED JUST BELOW THE LAV DUMP VALVE DOUBLER. THE SKIN WAS REPAIRED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND EMBRAER REPAIR FAX GST-0738/01.SDR COMA0110064Support · crackedDURING 2C CHECK TASK 5720-561-01I, THE LT WING UPPER SUPPORT AT RIB 23, BETWEEN STRINGERS 2A AND 3A, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110063Support · crackedDURING 2C CHECK TASK 5310-221-05I, THE LT FUSELAGE SKIN SUPPORT AT FRAME 9, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 660-1, REV IR, 2-16-93.SDR COMA0110062Stiffener · crackedDURING 2C CHECK TASK 5410-442-04I, THE RT NACELLE FRAME 10 STIFFENER ANGLE, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110061Shear Tie · crackedDURING 2C CHECK TASK 5310-222-05I, THE RT FUSELAGE SKIN SUPPORT AT FRAME 9, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 660-1, REV IR, 2-16-93.SDR COMA0110060Support · crackedDURING 2C CHECK TASK 5720-561-01I, THE LT WING UPPER SKIN SUPPORT AT RIB 23, BETWEEN STRINGERS 3A AND 4A, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110059Floor Support · crackedDURING 2C CHECK TASK 122-01Z, THE FUSELAGE RT FLOOR PROP AT FRAME 13 WAS FOUND CRACKED. THE PART WAS REPAIRED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT NR 3647-1, REV IR, 5-3-00.SDR COMA0110058Support · crackedDURING 2C CHECK TASK 5720-561-01I, THE LT WING UPPER SKIN SUPPORT AT RIB 23, BETWEEN STRINGER 5A AND REAR SPAR, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110057Support · crackedDURING 2C CHECK TASK 5720-522-011, THE LT WING LOWER SKIN SUPPORT AT RIB 8, AND STRINGER 10, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 3813-1, REV IR, 11-5-00.SDR COMA0110056Crossbeam · corrodedDURING 2C CHECK TASK 132-01Z, THE FUSELAGE RT FLOOR CROSSBEAM AT FRAME 16 WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110055Beam · crackedDURING 2C CHECK TASK 811-02Z, THE PAX DOOR AFT LATERAL BEAM WAS FOUND CRACKED. THE PART WAS REPAIRED IN ACCORDANCE WITH EMB-120 SRM 52-10-02, FIGURE 201.SDR COMA0110054Floorbeam · corrodedDURING 2C CHECK TASK 131/132-01Z, THE FUSELAGE CENTER FORWARD FLOOR OMEGA BEAM WAS FOUND CORRODED. THE PART WAS REPAIRED IN ACCORDANCE WITH EMB-120 STANDARD PRACTICES AND AERODESIGN REPORT 2181-12, REV IR, 3-4-01.SDR COMA0110053Strap · corrodedDURING 2C CHECK TASK 132-01Z, THE FUSELAGE RT FORWARD FLOOR BEAM BUTTSTRAP WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110052Sill · corrodedDURING 2C CHECK TASK 131-01Z, THE FUSELAGE LT FORWARD FLOOR BEAM SILL WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110051Sill · corrodedDURING 2C CHECK TASK 132-01Z, THE FUSELAGE RT FORWARD FLOORBEAM SILL WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110050Strap · corrodedDURING 2C CHECK TASK 131/132-01Z, THE FUSELAGE CENTER FORWARD FLOORBEAM BUTTSTRAP WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110048Strap · corrodedDURING 2C CHECK TASK 131-01Z, THE FUSELAGE LT FORWARD FLOORBEAM BUTTSTRAP WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110047Strap · corrodedDURING 2C CHECK TASK 131/132-01Z, THE FUSELAGE CENTER FORWARD FLOORBEAM BUTTSTRAP WAS FOUND CORRODED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT 1671-1, REV A, 1-28-97.SDR COMA0110046Channel · crackedDURING 2C CHECK TASK 811-02Z, THE PAX DOOR 3RD U-CHANNEL WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110045Channel · crackedDURING 2C CHECK TASK 811-02Z, THE PAX DOOR AFT U-CHANNEL WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110044Channel · crackedDURING 2C CHECK TASK 811-02Z, THE PAX DOOR 1ST U-CHANNEL WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR COMA0110003Relay · malfunctionedLANDING GEAR WILL NOT RETRACT. REPLACED THE LANDING GEAR RELAY BOX.SDR COMA0010005Relay · inoperativeEMERGENCY LIGHTS WILL NOT ARM. REPLACED RELAY KO201.SDR COMA9910100Sign · missingEMERGENCY EXIT SIGN ON BULKHEAD AT CABIN DOOR WAS MISSING. REPLACED EXIT SIGN ASSY.SDR COMA9910057Windshield · shatteredPILOTS WINDSHIELD SHATTERED. REPLACED WINDSHIELD.SDR COMA9810181Fuel Line · crackedWHILE REPLACING LEAKING RIVET IN RIGHT OUTBOARD WING, FOUND RE-FUEL LINE (P/N 120-08728-009) CRACKED AT BEND RADIUS. REPLACED CRACKED FUEL LINE.SDR COMA0810177Battery · dischargedEMERGENCY LIGHTS INOPERABLE. REPLACED BATTERY.SDR COMA9810154Lamp · failedTHREE EMERGENCY LIGHTS ARE INOP ROW 6 AND 7. REPLACED INOP LAMPS.SDR COMA9810135Battery · dischargedEMERGENCY LIGHTS AFT OF ROW 6 ARE INOPERABLE. REPLACED EMERGENCY LIGHTS BATTERY.
Back to N462CA, cancelled Sep 3, 2013