N261CA, cancelled May 5, 2006
Service difficulty reports · 70
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 = 'N261CA' AND deregistration_id = 'N261CA-2006-05-05' 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 = 'N261CA' AND deregistration_id = 'N261CA-2006-05-05' 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 COMA0010316Pump · leakingGREEN HYDRAULIC SYSTEM LOST ALL FLUID. REPLACED THE LEFT ENGINE HYDRAULIC PUMP.SDR COMA0010302Sensor · malfunctionedTAKEOFF TRIM AURAL WARNING. REPLACED ELEVATOR TRIM TAB PROXIMITY SENSOR.SDR COMA0010200Skin · chafedUPON COMPLIANCE OF2C INSPECTION TASK 5410-432-04I, THE LEFT 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 COMA0010199Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I, THE LEFT 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 COMA0010198Skin · gougedUPON COMPLIANCE OF 2C INSPECTION TASK 192-01Z, THE RIGHT FUSELAGE SKIN AT STRINGER 17R, 3 INCHES FORWARD OF FRAME 24 WAS FOUND TO BE GOUGED BY THE DEICE PRESSURE REGULATOR. THE DAMAGED PART WAS REPAIRED IAW EMB 120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES SDR COMA0010197Floor Support · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-121-01I, THE FUSELAGE LEFT SIDE FRAME 13 FLOOR PROP WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3647-1, REV IR, 5-3-00.SDR COMA0010196Floor Support · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-122-01I, THE FUSELAGE RIGHT SIDE FRAME 13 FLOOR PROP WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3647-1, REV IR, 5-3-00.SDR COMA0010195Shear Tie · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 261-01Z, THE FUSELAGE FRAME 40 SKIN SUPPORT BETWEEN STRINGERS 3L AND 4L WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB 120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010194Shear Tie · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-221-05I, THE SKIN SUPPORT BEHIND CAPTAIN''S DV WINDOW FRAME WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB 120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010193Skin · gougedUPON COMPLIANCE OF 2 YEAR CORROSION INSPECTION TASK 5310-132-COIE, THE LOWER RIGHT FUSELAGE SKIN JUST UNDER THE LAV DUMP VALVE DOUBLER WAS FOUND TO BE GOUGED. THE DAMAGED PART WAS REPAIRED IAW EMB 120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND SRM 53-00-SDR COMA0010192Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-142-03I, THE RIGHT HAND FLOORBEAM BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB 120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 2174-1, REV IR, 1-15-97.SDR COMA0010191Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-141-03I, THE LEFT HAND FLOORBEAM BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 2174-1, REV IR, 1-15-97.SDR COMA0010190Threshold · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-141-03I, THE LEFT HAND FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010189Threshold · gougedUPON COMPLIANCE OF 2C INSPECTION TASK 164-01Z, THE AFT RIGHT HAND CARGO FLOOR SILL WAS FOUND TO BE DAMAGED BY AN INTERIOR LINING SCREW. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3661-1, REV ISDR COMA0010188Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z, THE FORWARD FLOOR SUPPORT RIGHT HAND BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL MANUAL STANDARD PRACTICES.SDR COMA0010187Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE FORWARD LEFT HAND FLOOR BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010186Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE FORWARD LEFT HAND FLOOR 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 COMA0010185Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z, THE FORWARD CABIN CENTER BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 1671-1, REV A, 1-28-97.SDR COMA0010184Threshold · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z, THE FORWARD RIGHT HAND CABIN FLOOR SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010183Floorbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE FORWARD LT FLOOR CROSSBEAM AT FRAME 15 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010182Floorbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z, THE FORWARD RT FLOOR CROSSBEAM AT FRAME 16 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010181Floorbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE LEFT HAND FLOOR CROSSBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010180Floorbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z, THE RIGHT HAND FLOOR CROSSBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STURCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010179Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z, THE FORWARD CABIN FLOOR CENTER BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010178Floorbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE FORWARD CABIN FLOOR LEFT HAND CROSSBEAM AT FRAME 14 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010177Frame · gougedUPON COMPLIANCE OF 2C INSPECTION TASK 263/264-01Z, THE FUSELAGE FRAME 46A WAS FOUND TO BE GOUGED BY INTERIOR LINING SCREWS IN TWO PLACES. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010176Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 161-01Z, THE CARGO COMPARTMENT ENTRYWAY FLOOR BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3661-3, REV IR, 6-12-00.SDR COMA0010175Frame · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 161/162-01Z, THE FUSELAGE FRAME 42 CHANNEL AT 6 O''CLOCK WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3674-3, REV IR, 6-12-00.SDR COMA0010174Crossbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-121/122-01I, THE FRAME 12 CROSSBEAM AT COCKPIT ENTRANCE FLOOR WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010173Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 163-012Z, THE AFT LEFT HAND CARGO FLOOR SILL 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, 5-15-00.SDR COMA0010172Intercostal · crackedUPON COMPLIANCE 2C INSPECTION TASK 5310-221-05I, THE LEFT HAND COCKPIT OVERHEAD INTERCOSTAL WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010171Floorbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE FUSELAGE FLOOR T-SECTION OF FRAME 16 LT WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010170Angle · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5320-243-01I, THE LEFT WING UPPER SURFACE ATTACH ANGLE FOR FAIRING 193 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR STANDARD PRACTICES AND AERODESIGN REPORT NR 1226-21, REV IR, 7-6-SDR COMA0010169Angle · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5320-244-01I, THE RIGHT WING UPPER SURFACE ATTACH ANGLE FOR FAIRING 194 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 1226-21, REV SDR COMA0010168Skin · gougedUPON COMPLIANCE OF 2 YEAR CORROSION INSPECTION TASK 5310-132-COIE, THE RIGHT HAND FORWARD LOWER FUSELAGE SKIN AT STRINGER 17R WAS FOUND TO BE GOUGED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NSDR COMA0010167Shear Tie · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-221-05I, THE FUSELAGE FRAME 9 SKIN SUPPORT JUST BELOW CAPTAIN''S DV WINDOW WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 660-1SDR COMA0010166Shear Tie · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-022-05I, THE FUSELAGE FRAME 9 SKIN SUPPORT JUST BELOW F/O''S DV WINDOW WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 660-1, RESDR COMA0010165Skin · gougedUPON COMPLIANCE OF 2C INSPECTION TASK 813-02Z, THE CARGO DOOR SKIN AND PREVIOUS REPAIR DOUBLER 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 COMA0010164Skin · delaminatedUPON COMPLIANCE OF 2C INSPECTION TASK 612-01Z, THE RIGHT WING OUTBOARD LEADING EDGE WAS FOUND TO BE DELAMINATED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND SRM 57-40-01, FIGURE 201.SDR COMA0010163Stringer · crackedTHE RIGHT WING STRINGER 10 WAS FOUND TO BE CRACKED JUST INBOARD OF RIB 8. THE STRINGER WAS REPAIRED PER EMB120 SRM 57-20-01, FIGURE 201 AND AERODESIGN REPORT NR 3694-1, REV IR, DATED 6-12-00.SDR COMA0010025Battery · dischargedEMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY BATTERIES.SDR COMA9910197Battery · dischargedEMERGENCY LIGHTS ARE INOPERABLE. REPLACED THE EMERGENCY BATTERIES.SDR COMA9910182Air Conditioning · failedRIGHT AIR CONDITIONING FAILED. COULD NOT DUPLICATE. SYSTEM FUNCTION CHECK NORMAL.SDR COMA9910148Switch · out of adjustSERVICE DOOR WARNING DURING TAKEOFF. ADJUSTED FUEL SERVICE DOOR SWITCH.SDR COMA9910115Sign · brokenEXIT SIGN AT ROW 8 IS BROKEN. REPLACED SIGN.SDR COMA910113Warning · activatedTRIM INOPERABLE WARNING DURING TAKEOFF. COULD NOT DUPLICATE. RESET SYSTEM AND AIRCRAFT RETURNED TO SERVICE.SDR COMA9910103Circuit Breaker · trippedTHE FLIGHT IDLE STOP SOLENOID CIRCUIT BREAKERS ARE TRIPPED. RESET BREAKERS AND FUNCTION CHECK OF SYSTEM NORMAL.SDR COMA9910092Sign · inoperativeEXIT SIGN AT ROW 5 IS INOP. REPLACED EXIT SIGN.SDR COMA9910019Warning · activatedDURING TAKEOFF ROLL, AUTOFEAHTER AURAL WARNING ACTIVATED. INSPECTED LT AND RT ENGINE SCU FOR CONDITION AND SECURITY. PERFORMED OPERATIONAL CHECK OF THE AUTOFEATHER SYSTEM, NO DEFECTS NOTED.SDR COMA9910017Actuator · leakingLT MLG DISAGREEMENT INDICATION WHEN LANDING GEAR RETRACTED. REPLACED THE LT MLG RETRACT ACTUATOR.
Back to N261CA, cancelled May 5, 2006