# Service difficulty reports: N264CA, cancelled Oct 5, 2006 A list on [N264CA, cancelled Oct 5, 2006](https://openairdocs.org/deregistered/N264CA-2006-10-05.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 88 reports - [SDR COMA0210029](https://openairdocs.org/sdr/COMA0210029.md): Lamp · burned out · Jul 18, 2002 · N264CA · Emb EMB120RT · Emergency Lighting > FLIGHT 5047 EMERGENCY LIGHT INOP.REPLACED LIGHT BULB. - [SDR COMA0210015](https://openairdocs.org/sdr/COMA0210015.md): Bracket · cracked · Apr 12, 2002 · N264CA · Emb EMB120RT · Fuselage Main, Structure > DURING AN E-10 PART A INSPECTION THE FUSELAGE SKIN SUPPORT BRACKET (P/N 120-34416-001) ON THE LEFT SIDE JUST BELOW THE PILOTS WINDSHIELD SIDE POST AT FRAME 9 WAS FOUND TO BE CRACKED.THE CRACKED BRACKET (P/N 120-34416-001) WAS REMOVED FROM THE AIRCRAFT AND A SE - [SDR COMA0210012](https://openairdocs.org/sdr/COMA0210012.md): Control Box · malfunctioned · Apr 2, 2002 · N264CA · Emb EMB120RT · Landing Gear Retraction/Extension System > FLIGHT 5070 LANDING GEAR CONTROL COULD NOT BE SELECTED TO THE UP POSITION.REPLACED THE L/G CONTROL HANDLE ASSY. - [SDR COMA0210010](https://openairdocs.org/sdr/COMA0210010.md): Engine · failed · Mar 26, 2002 · N264CA · Emb EMB120RT · Engine (Turbine/Turboprop) > FLIGHT 5059 R/H ENGINE FAILED WITH NO WARNINGS. IFSD REPLACED ENGINE. - [SDR COMA0210003](https://openairdocs.org/sdr/COMA0210003.md): Battery · discharged · Feb 1, 2002 · N264CA · Emb EMB120RT · Emergency Lighting > FLIGHT 5044 EMERGENCY FLOOR PATH LIGHTS ARE INOP IN SEVERAL PLACES. REPLACED THE NR 2 EMERGENCY BATTERY. - [SDR COMA0110156](https://openairdocs.org/sdr/COMA0110156.md): Battery · discharged · Nov 12, 2001 · N264CA · Emb EMB120RT · Emergency Lighting > FLIGHT #5044. EMERGENCY LIGHTS ARE INOP.REPLACED THE EMERGENCY LIGHTS BATTERY. - [SDR COMA0110148](https://openairdocs.org/sdr/COMA0110148.md): Roller · worn · Sep 28, 2001 · N264CA · Emb EMB120RT · Trailing Edge Flap Control System > FLIGHT 5070 FLAP SELECTION BEYOND 25 DEGREES RESULTS IN FLAP DISAGREEMENT WARNING.REPLACED THE R/H OUTBD FLAP ROLLERS. SYSTEM CHECK SATISFACTORY. - [SDR COMA0110139](https://openairdocs.org/sdr/COMA0110139.md): Indicator · faulty · Aug 26, 2001 · N264CA · Emb EMB120RT · Power Indicating System > FLIGHT #5053. DURING APPLICATION OF POWER FOR TAKE OFF AT MCO THE #2 NH ANALOG INDICATION FAILED, AIRCRAFT RETURNED TO THE GATE.REPLACED THE NH/NL INDICATOR. - [SDR COMA0110136](https://openairdocs.org/sdr/COMA0110136.md): Indicator · faulty · Aug 26, 2001 · N264CA · Emb EMB120RT · Power Indicating System > FLIGHT #5053. DURING APPLICATION OF POWER FOR TAKE OFF AT MCO THE #2 NH ANALOG INDICATION FAILED, AIRCRAFT RETURNED TO THE GATE.REPLACED THE NH/NL INDICATOR. - [SDR COMA0110042](https://openairdocs.org/sdr/COMA0110042.md): Boot · damaged · Mar 9, 2001 · N264CA · Emb EMB120RT · Airfoil Anti/De-ice System > WING DE-ICE FAIL WARNING. REPAIRED HOLES IN WING LEADING EDGE DE-ICE BOOTS, USING PATCH KIT. - [SDR COMA0110032](https://openairdocs.org/sdr/COMA0110032.md): Display · malfunctioned · Feb 5, 2001 · N264CA · Emb EMB120RT · Attitude and Direction Data System > ATTITUDE DISPLAY AND FLIGHT DIRECTOR FAILURE WARNINGS. REPLACED THE NR 2 AHRS. - [SDR COMA0110031](https://openairdocs.org/sdr/COMA0110031.md): Reservoir · low · Jan 26, 2001 · N264CA · Emb EMB120RT · Hydraulic Reservoir, Main > HYDRAULIC RESERVOIR LOW LEVEL CAUTION. SERVICED HYD RESERVOIR, NO DEFECTS FOUND WITH HYDRAULIC SYSTEM. - [SDR COMA0010377](https://openairdocs.org/sdr/COMA0010377.md): Buttstrap · corroded · Nov 10, 2000 · N264CA · Emb EMB120RT · Fuselage Main, Floor Beam > UPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z THE FORWARD RH FLOOR SUPPORT BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010376](https://openairdocs.org/sdr/COMA0010376.md): Buttstrap · corroded · Nov 10, 2000 · N264CA · Emb EMB120RT · Fuselage Main, Floor Beam > UPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z THE FORWARD LH FLOOR SUPPORT BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL MANUAL STANDARD PRACTICES. - [SDR COMA0010375](https://openairdocs.org/sdr/COMA0010375.md): Buttstrap · corroded · Nov 10, 2000 · N264CA · Emb EMB120RT · Fuselage Main, Floor Beam > UPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z THE FORWARD CENTER FLOOR SUPPORT BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #1671-1, REV. 1, 1-28-97. - [SDR COMA0010374](https://openairdocs.org/sdr/COMA0010374.md): Skin · gouged · Nov 10, 2000 · N264CA · Emb EMB120RT · Fuselage Main, Plate/Skin > UPON COMPLIANCE OF 2 YEAR CORROSION CHECK TASK 5310-132-CO1E THE FUSELAGE SKIN BELOW THE LAV DUMP VALVE DOUBLER WAS FOUND TO BE GOUGED. THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMBRAER REPAIR FAX #SST-3090/00 - [SDR COMA0010402](https://openairdocs.org/sdr/COMA0010402.md): Skin · chafed · Nov 10, 2000 · N264CA · Emb EMB120RT · Nacelle/Pylon, Plate/Skin > UPON COMPLIANCE OF 2C INSPECTION TASK 5410-432-04I THE LT NACELLE OUTBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-IR, 7-25-99. - [SDR COMA0010401](https://openairdocs.org/sdr/COMA0010401.md): Skin · chafed · Nov 10, 2000 · N264CA · Emb EMB120RT · Nacelle/Pylon, Plate/Skin > UPON COMPLANCE OF 2C INSPECTION TASK 5410-432-04I THE LT NACELLE INBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1,IR,7-25-99. - [SDR COMA0010400](https://openairdocs.org/sdr/COMA0010400.md): Skin · chafed · Nov 10, 2000 · N264CA · Emb EMB120RT · Nacelle/Pylon, Plate/Skin > UPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I THE RT NACELLE INBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, IR, 7-25-99. - [SDR COMA0010399](https://openairdocs.org/sdr/COMA0010399.md): Skin · chafed · Nov 10, 2000 · N264CA · Emb EMB120RT · Nacelle/Pylon, Plate/Skin > UPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I THE RT NACELLE OUTBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, IR, 7-25-99. - [SDR COMA0010398](https://openairdocs.org/sdr/COMA0010398.md): Sill · corroded · Nov 10, 2000 · N264CA · Emb EMB120RT · Fuselage Main, Floor Beam > UPON COMPLIANCE OF 2C INSPECTION TASK 151-01Z THE LT FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010397](https://openairdocs.org/sdr/COMA0010397.md): Floorbeam · corroded · Nov 10, 2000 · N264CA · Emb EMB120RT · Fuselage Main, Floor Beam > UPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z THE RT FLOOR SUPPORT T-SECTION WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010396](https://openairdocs.org/sdr/COMA0010396.md): Channel · cracked · Nov 10, 2000 · N264CA · Emb EMB120RT · Passenger/Crew Doors > UPON COMPLIANCE OF 2C INSPECTION TASK 811-02Z THE PAX DOOR INNER CHANNEL, FOURTH FROM BOTTOM WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010395](https://openairdocs.org/sdr/COMA0010395.md): Channel · cracked · Nov 10, 2000 · N264CA · Emb EMB120RT · Passenger/Crew Doors > UPON COMPLIANCE OF 2C INSPECTION TASK 811-02Z THE PAX DOOR INNER CHANNEL, SECOND FROM BOTTOM WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010394](https://openairdocs.org/sdr/COMA0010394.md): Shear Tie · cracked · Nov 10, 2000 · N264CA · Emb EMB120RT · Fuselage Main, Structure > UPON COMPLIANCE OF 2C INSPECTION 232-01Z THE FUSELAGE SKIN SUPPORT AT FRAME 13A, STRINGER 14R WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3653-IR, 11-7-00. - [SDR COMA0010393](https://openairdocs.org/sdr/COMA0010393.md): Skin · corroded · Nov 10, 2000 · N264CA · Emb EMB120RT · Fuselage Main, Plate/Skin > UPON COMPLIANCE OF 2C INSPECTION TASK 161-01Z THE CARGO DOOR CUTOUT INNER SKIN WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMBRAER REPAIR FAX NR SST-3065/00, 11-3-00. - [SDR COMA0010392](https://openairdocs.org/sdr/COMA0010392.md): Buttstrap · corroded · Nov 10, 2000 · N264CA · Emb EMB120RT · Fuselage Main, Floor Beam > UPON COMPLIANCE OF 2C INSPECTION TASK 161-01Z THE CARGO COMPARTMENT ENTRY THRESHOLD BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3661-3, IR, 6-12-00. - [SDR COMA0010391](https://openairdocs.org/sdr/COMA0010391.md): Floorbeam · cracked · Nov 10, 2000 · N264CA · Emb EMB120RT · Fuselage Main, Floor Beam > UPON COMPLIANCE OF 2C INSPECTION TASK 5310-122-01I THE RT FLOOR PROP AT FRAME 13 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3647-1, IR, 5-3-00. - [SDR COMA0010390](https://openairdocs.org/sdr/COMA0010390.md): Floorbeam · cracked · Nov 10, 2000 · N264CA · Emb EMB120RT · Fuselage Main, Floor Beam > UPON COMPLIANCE OF 2C INSPECTION TASK 5310-121-01I THE LT FLOOR PROP AT FRAME 12 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3647-1, IR, 5-3-00. - [SDR COMA0010389](https://openairdocs.org/sdr/COMA0010389.md): Shear Tie · cracked · Nov 10, 2000 · N264CA · Emb EMB120RT · Fuselage Main, Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 221-01Z THE LT FUSELAGE SKIN SUPPORT BRACKET WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010388](https://openairdocs.org/sdr/COMA0010388.md): Sill · corroded · Nov 10, 2000 · N264CA · Emb EMB120RT · Fuselage Main, Floor Beam > UPON COMPLIANCE OF 2C INSPECTION TASK 164-01Z THE RT FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010387](https://openairdocs.org/sdr/COMA0010387.md): Sill · corroded · Nov 10, 2000 · N264CA · Emb EMB120RT · Fuselage Main, Floor Beam > UPON COMPLIANCE OF 2C INSPECTION TASK 162-01Z THE RT FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010386](https://openairdocs.org/sdr/COMA0010386.md): Crossbeam · corroded · Nov 10, 2000 · N264CA · Emb EMB120RT · Fuselage Main, Floor Beam > UPON COMPLIANCE OF 2C INSPECTION TASK 152-01Z THE RT FLOOR SUPPORT CROSSBEAM WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010385](https://openairdocs.org/sdr/COMA0010385.md): Crossbeam · corroded · Nov 10, 2000 · N264CA · Emb EMB120RT · Fuselage Main, Floor Beam > UPON COMPLIANCE OF 2C INSPECTION TASK 151-01Z THE LT FLOOR SUPPORT CROSSBEAM WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010384](https://openairdocs.org/sdr/COMA0010384.md): Crossbeam · corroded · Nov 10, 2000 · N264CA · Emb EMB120RT · Fuselage Main, Floor Beam > UPON COMPLIANCE OF 2C INSPECTION TASK 145-01Z THE LT FLOOR SUPPORT CROSSBEAM WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010383](https://openairdocs.org/sdr/COMA0010383.md): Sill · corroded · Nov 10, 2000 · N264CA · Emb EMB120RT · Fuselage Main, Floor Beam > UPON COMPLIANCE OF 2C INSPECTION TASK 141-01Z THE LT FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010382](https://openairdocs.org/sdr/COMA0010382.md): Sill · corroded · Nov 10, 2000 · N264CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z THE RT FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010381](https://openairdocs.org/sdr/COMA0010381.md): Buttstrap · corroded · Nov 10, 2000 · N264CA · Emb EMB120RT · Fuselage Main, Floor Beam > UPON COMPLIANCE OF 2C INSPECTION TASK 141-01Z THE LT FLOOR SUPPORT BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL PRACTICES. - [SDR COMA0010380](https://openairdocs.org/sdr/COMA0010380.md): Buttstrap · corroded · Nov 10, 2000 · N264CA · Emb EMB120RT · Fuselage Main, Floor Beam > UPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z THE CENTER FLOOR SUPPORT BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010379](https://openairdocs.org/sdr/COMA0010379.md): T-Section · corroded · Nov 10, 2000 · N264CA · Emb EMB120RT · Fuselage Main, Floor Beam > UPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z THE RT FLOOR SUPPORT T-SECTION AT FRAME 16 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL PRACTICES. - [SDR COMA0010378](https://openairdocs.org/sdr/COMA0010378.md): Floorbeam · corroded · Nov 10, 2000 · N264CA · Emb EMB120RT · Fuselage Main, Floor Beam > UPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z THE LT FLOOR SUPPORT T-SECTION AT FRAME 16 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010372](https://openairdocs.org/sdr/COMA0010372.md): Battery · discharged · Oct 9, 2000 · N264CA · Emb EMB120RT · Emergency Lighting > FWD SECTION OF EMERGENCY FLOOR LIGHTING IS INOP. REPLACED THE NR 1 EMERGENCY BATTERY. - [SDR COMA0010331](https://openairdocs.org/sdr/COMA0010331.md): Light · inoperative · Sep 8, 2000 · N264CA · Emb EMB120RT · Emergency Lighting > EMERGENCY LIGHT AT ROW 5 IS INOPERABLE. COULD NOT DUPLICATE. EMERGENCY LIGHT OPS NORMAL. - [SDR COMA0010327](https://openairdocs.org/sdr/COMA0010327.md): Connector · dirty · Aug 29, 2000 · N264CA · Emb EMB120RT · Propeller Feathering/Reversing > AUTOFEATHER WARNING DURING TAKEOFF. CLEANED CONNECTORS CL4 AND CL28, SYSTEM TESTED SATISFACTORY. - [SDR COMA0010066](https://openairdocs.org/sdr/COMA0010066.md): Receptacle · shorted · May 13, 2000 · N264CA · Emb EMB120RT · External Power System > MECHANIC NOTICED SMOKE COMING FROM THE GPU PLUG WHILE AIRCRAFT WAS PARKED AT THE GATE. REPLACED THE EXTERNAL POWER RECEPTACLE AND MULTIPLE AVIONICS COMPONENTS DUE TO CONTAMINATION FROM FIRE EXTINGUISHER CHEMICALS. - [SDR COMA0010067](https://openairdocs.org/sdr/COMA0010067.md): Pcu · out of rig · May 12, 2000 · N264CA · Emb EMB120RT · Propeller Controlling System > RIGHT PROPELLER RPM 102.7 PERCENT. CHECKED PROPELLER TO PCU RIGGING, FOUND NO DEFECTS AND FUNCTION CHECK NORMAL. A/C RETURNED TO SERVICE. - [SDR COMA0010052](https://openairdocs.org/sdr/COMA0010052.md): Skin · corroded · Apr 18, 2000 · N264CA · Emb EMB120RT · Fuselage Main, Plate/Skin > ON A MAINTENANCE SERVICE CHECK, MECHANIC NOTED POPPED RIVET HEAD ON EXTERNAL SKIN, FRAME 21, LOWER LEFT SIDE, AND SEVERAL BULGES IN SKIN. UPON FURTHER INSPECTION, FOUND CORROSION BETWEEN SKIN AND TITANIUM STRAP. CUT OUT CORRODED AREA, FABRICATED AND INSTALLE - [SDR COMA0010053](https://openairdocs.org/sdr/COMA0010053.md): Potentiometer · malfunctioned · Apr 17, 2000 · N264CA · Emb EMB120RT · Landing Gear Steering System > LANDING GEAR SELECTOR COULD NOT BE SELECTED UP. REPLACED THE NWS FEEDBACK POT. - [SDR COMA0010047](https://openairdocs.org/sdr/COMA0010047.md): Battery · discharged · Mar 26, 2000 · N264CA · Emb EMB120RT · Emergency Lighting > FORWARD SECTION OF EMERGENCY FLOOR PATH LIGHTING IS INOPERABLE. REPLACED EMERGENCY BATTERY. - [SDR COMA0010037](https://openairdocs.org/sdr/COMA0010037.md): Sensor · malfunctioned · Mar 14, 2000 · N264CA · Emb EMB120RT · Landing Gear Position and Warning > LANDING GEAR FAILED TO RETRACT, ALL GREEN INDICATORS ON WITH SELECTOR UP. REPLACED RIGHT HAND MLG UPLOCK SENSOR. Next page: https://openairdocs.org/deregistered/N264CA-2006-10-05/reports.md?page=2 ## 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 = 'N264CA' AND deregistration_id = 'N264CA-2006-10-05' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N264CA-2006-10-05/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.