N263CA, cancelled Nov 16, 2006
Service difficulty reports · 55
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 = 'N263CA' AND deregistration_id = 'N263CA-2006-11-16' 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 = 'N263CA' AND deregistration_id = 'N263CA-2006-11-16' 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 COMA0110004Frame · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131-012 AND 132-012 THE FUSELAGE FRAME 20 CHANNEL BETWEEN STRINGERS 20L AND 20R WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURE REPAIR MANUAL STANDARD PRACTICES AND SRM 53-10-04 FIGURE 201 ASDR COMA0010108Floorbeam · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-121-01I, THE LT FLOOR PROP AT FRAME 13 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3647-1, REV IR, 5-3-00.SDR COMA0010123Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I, THE RT NACELLE INBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED IAW EMB 120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, REV IR, 7-25-99.SDR COMA0010122Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I, THE RT NACELLE OUTBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, REV IR, 7-25-99.SDR COMA0010121Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-432-04I, THE LT NACELLE OUTBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, REV IR, 7-25-99.SDR COMA0010120Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-432-04I, THE LT NACELLE INBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, REV IR, 7-25-99.SDR COMA0010119Shear Tie · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 231-012, WHILE GAINING ACCESS THE LT FUSELAGE SKIN SUPPORT BETWEEN FRAMES 12 AND 13 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010118Shear Tie · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 232-012, THE FUSELAGE FRAME 13A SKIN SUPPORT AT STRINGER 14R WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3653-1, REV IR, 5-6-00.SDR COMA0010117Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 164-012, THE CARGO COMPARTMENT FLOOR SUPPORT AFT RT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3661-1, REV IR, 5-15-SDR COMA0010116Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 163-012, THE CARGO COMPARTMENT FLOOR SUPPORT AFT LT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3661-1, REV IR, 5-15-SDR COMA0010115Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 162-012, THE CARGO COMPARTMENT FLOOR SUPPORT FORWARD RT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB 120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3661-1, REV IR, 5SDR COMA0010113Stringer · dentedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I, THE RT NACELLE OUTBOARD STRINGER NR 1 WAS FOUND TO BE DENTED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND SRM 54-10-01 FIGURE 202.SDR COMA0010112Skin · gougedUPON COMPLIANCE OF 2C INSPECTION TASK 813-02Z, THE CARGO DOOR SKIN WAS FOUND TO BE GOUGED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND SRM 52-30-01 FIGURE 201.SDR COMA0010111Support Bracket · crackedRIVET HEAD WAS NOTICED CRACKED ON LEFT SIDE OF FUSELAGE AT FRAME 9. INTERNAL INVESTIGATION FOUND THE SKIN SUPPORT TO BE CRACKED. THE SKIN SUPPORT WAS REPLACED IAW EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT NR 660-1, REV IR, 2-16-93.SDR COMA0010110Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE FUSELAGE FORWARD LT FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 1671-2, REV IR, 12-4-96.SDR COMA0010109Floorbeam · crackedUPON 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 IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3647-1, REV IR, 5-3-00.SDR COMA0010064Circuit Breaker · trippedLEFT HAND, FLIGHT IDLE STOP SOLENOID, CIRCUIT BREAKER IS TRIPPED. RESET CIRCUIT BREAKER, TESTED SYSTEM FOUND TO OPERATE NORMAL.SDR COMA0010024Sign · looseEXIT SIGN AT ROW 5 FELL OFF. REPLACED EXIT SIGN.SDR COMA9910177Sign · brokenEXIT SIGN AT ROW 5 IS BROKEN. REPLACED SIGN.SDR COMA9910147Relay · failedTHE EMERGENCY BUS LIGHT ILLUMINATED DURING FLIGHT AND WOULD NOT EXTINGUISH. REPLACED RELAY KO440.SDR COMA0010131Sign · brokenEMERGENCY EXIT SIGN AT ROW 5 IS BROKEN. REPLACED SIGN.SDR COMA9910111Sensor · failedLEFT HAND MLG DISAGREEMENT LIGHT REMAINS ON AFTER GEAR RETRACTED. REPLACED THE UPLOCK PROXIMITY SENSORS.SDR COMA9910104Battery · dischargedFORWARD FLOOR EMERGENCY LIGHTING WAS WEAK. REPLACED EMERGENCY BATTERY.SDR COMA9910094Sensor · malfunctionLANDING GEAR DID NOT EXTEND NORMALLY. OVERRIDE SYSTEM WAS USED. REPLACED THE LEFT HAND MLG DOWNLOCK PROX SENSOR SWITCH.SDR COMA9910090Hyd Syst · reqd serviceGREEN HYDRAULIC SYSTEM LOW PRESSURE WARNING DURING GEAR RETRACTION. SERVICED HYDRAULIC RESERVOIR TO PROPER LEVEL.SDR COMA9910061Angle · corrodedWHILE PERFORMING TASK 5320-252-04E ON A 2000 FLIGHT CYCLE INSPECTION, FOUND AFT EXIT PIN RECEPTACLES TO BE CORRODED BETWEEN RECEPTACLES AND FLOOR ANGLE. REMOVED FLOOR ANGLE AND PIN RECEPTACLES AND REPLACED WITH SERV UNITS IAW EMB-120-SRM.SDR COMA9910060Angle · corrodedWHILE PERFORMING TASK 5320-252-04E ON 2000 FLIGHT CYCLE INSPECTION, FOUND LOWER FLOOR ANGLE OF AFT EXIT TO BE CORRODED BETWEEN ANGLE AND PIN RECEPTACLES. REMOVED ANGLE AND PINS AND REPLACED WITH SERVICEABLE UNITS IAW EMB-120 SRM.SDR COMA9910043Rheostat · inoperativeOVERHEAD PANEL LIGHT IS INOPERABLE. REPLACED RHEOSTAT.SDR COMA9810261Sign · brokenEMERGENCY EXIT SIGN AT ROW 8 BROKEN. REMOVED AND REPLACED EXIT SIGN ASSY.SDR COMA9810187Pin · installedNLG DID NOT RETRACT. REMOVED NLG DOWN LOCK SAFETY PIN. AIRCRAFT RETURNED TO SERVICE.SDR COMA9810151Pcu · malfunctionRIGHT HAND RPM DROPPED 30 PERCENT DURING TAKEOFF ROLL. REPLACED THE RIGHT HAND PCU.SDR COMA9810102Leak Warning · activatedRIGHT HAND DUCT LEAK WARNING DURING TAKEOFF. COULD NOT DUPLICATE PROBLEM.SDR COMA9810030Aural Warn Unit · looseTAKEOFF TRIM AURAL WARNING DURING TAKEOFF. SECURED LOOSE AURAL WARNING UNIT IN RACK.SDR COMA9810024Sensor · defectiveTRIM WARNING DURING TAKEOFF. REPLACED THE ELEVATOR TRIM TAB PROXIMITY SENSOR.SDR COMA9810023Bearing · wornDURING PROPELLER DYNAMIC BALANCING PROCEDURES, IT WAS DETERMINED THAT THE PROPELLER COULD NOT BE BALANCED. FURTHER INSPECTION OF PROPELLER FOUND NR 2 BLADE TO BE EXCESSIVELY LOOSE. FURTHER INSPECTION FOUND BLADE PIN BEARING TO BE WORN TO 0.080 WALL THICKNESSSDR COMA9710507Circuit Breaker · trippedTRIM WARNING DURING TAKEOFF. AURAL WARNING CIRCUIT BREAKER WAS TRIPPED. RESET BREAKER AND SYSTEM TEST NORMAL.SDR COMA9710504Lamp · failedLEFT OVERWING EMERGENCY LIGHT IS INOP. REPLACED LAMP.SDR COMA9710482Seal · leakingLEFT ENGINE OIL PRESSURE DECREASED TO 40 PSI DURING FLIGHT (IFSD). REPLACED THE START/GENERATOR DRIVE OIL SEAL.SDR COMA9710214Latch · brokenTHE RIGHT MLG OPENED DURING FLIGHT. REPLACED BROKEN RIGHT MLG OUTBD DOOR LATCH ASSEMBLY.SDR COMA9710073Pitchlock Screw · damagedACTUATOR ASSEMBLY REMOVED ORIGINALLY FOR MAJOR INSPECTION. UPON INITIAL RECEIVING INSPECTION, THE FEATHER STOP TAB (S/N S0328) WAS FOUND TO BE BENT APPROXIMATELY 0.125. PITCHLOCK SCREW WAS REMOVED FROM ASSEMBLY AND RETURNED TO MANUFACTURER.SDR COMA9710042Pcu · inoperativeRIGHT PROPELLER WENT TO 103.7 PERCENT RPM ON TAKEOFF. REPLACED RIGHT PROPELLER PCU.SDR COMA9610408Hydraulic Hose · looseLT HYDRAULIC SYSTEM QUANTITY INDICATED ZERO DURING FLIGHT. EMERGENCY FREE FALL SYSTEM WAS USED TO EXTEND LANDING GEAR. TIGHTENED LOOSE HYDRAULIC PUMP HOSE FITTING AT LT NACELLE FIRE DECK.SDR COMA9610390Engine · failedLEFT ENGINE FAILED AT 23,000 FT, SMOKE IN COCKPIT. CAGED ENGINE AND RETURNED TO FIELD. REPLACED LEFT ENGINE.SDR COMA9610330Deice Lead · brokenRIGHT PROPELLER DEICE FAILED. REPLACED ELECTRICAL DEICE LEAD ON RT PROPELLER.SDR COMA9610311Battery · dischargedAFT EMERGENCY LIGHTS ARE INOP. REPLACED EMERGENCY BATTERY.SDR COMA9710433Lamp · failedTHE AFT LAMP OF THE CABIN FLOOR PATH EMERGENCY LIGHTING IS INOP. REPLACED LAMP.SDR COMA9610296Switch · failedPILOTS PEDAL STEER DISCONNECT SWITCH IS INOP. REPLACED SWITCH.SDR COMA9610232Hinge · brokenRIGHT M.L.G. DID NOT RETRACT WHEN LANDING GEAR WAS SELECTED UP. REPLACED BROKEN LANDING GEAR DOOR AFT HINGE, WHICH DID NOT ALLOW ACTUATION OF THE SEQUENCE VALVE.SDR COMA9610092Autofeather Sw · failedAUTOFEATHER SYSTEM DID NOT ARM DURING TAKEOFF. REPLACED THE AUTOFEATHER ARM MICRO SWITCH IN THE POWER LEVER QUADRANT.SDR COMA9610093Actuator · defectiveLT MLG INDICATED UNSAFE. LANDING GEAR CYCLED TWICE WITH SAME RESULTS. USED EMERGENCY SYSTEM TO EXTEND LANDING GEAR AND ALL GEAR INDICATED SAFE. REPLACED THE LT MLG HYDRAULIC ACTUATOR.
Back to N263CA, cancelled Nov 16, 2006