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.

SDR COMA0010316Pump · leakingGREEN HYDRAULIC SYSTEM LOST ALL FLUID. REPLACED THE LEFT ENGINE HYDRAULIC PUMP.Aug 15, 2000 · N261CA · Emb EMB120RT · Hydraulic Pump (Electric/Engine), MainSDR COMA0010302Sensor · malfunctionedTAKEOFF TRIM AURAL WARNING. REPLACED ELEVATOR TRIM TAB PROXIMITY SENSOR.Jul 19, 2000 · N261CA · Emb EMB120RT · Elevator Control SystemSDR 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.Jun 14, 2000 · N261CA · Emb EMB120RT · Nacelle/Pylon, Plate/SkinSDR 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.Jun 14, 2000 · N261CA · Emb EMB120RT · Nacelle/Pylon, Plate/SkinSDR 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 Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, Plate/SkinSDR 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.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 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.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 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.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, StructureSDR 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.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, StructureSDR 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-Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, Plate/SkinSDR 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.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 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.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 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.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 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 IJun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 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.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 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.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 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.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 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.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 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.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 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.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR 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.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR 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.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR 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.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR 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.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 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.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR 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.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, FrameSDR 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.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 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.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, FrameSDR 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.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 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.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 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.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 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.Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR 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-Jun 14, 2000 · N261CA · Emb EMB120RT · Wing Miscellaneous StructureSDR 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 Jun 14, 2000 · N261CA · Emb EMB120RT · Wing Miscellaneous StructureSDR 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 NJun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, Plate/SkinSDR 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 660-1Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, StructureSDR 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, REJun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, StructureSDR 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.Jun 14, 2000 · N261CA · Emb EMB120RT · Cargo/Baggage DoorsSDR 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.Jun 14, 2000 · N261CA · Emb EMB120RT · Trailing Edge FlapsSDR 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.Jun 12, 2000 · N261CA · Emb EMB120RT · Wing, Longeron/StringerSDR COMA0010025Battery · dischargedEMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY BATTERIES.Feb 4, 2000 · N261CA · Emb EMB120RT · Emergency LightingSDR COMA9910197Battery · dischargedEMERGENCY LIGHTS ARE INOPERABLE. REPLACED THE EMERGENCY BATTERIES.Dec 23, 1999 · N261CA · Emb EMB120RT · Emergency LightingSDR COMA9910182Air Conditioning · failedRIGHT AIR CONDITIONING FAILED. COULD NOT DUPLICATE. SYSTEM FUNCTION CHECK NORMAL.Dec 6, 1999 · N261CA · Emb EMB120RT · Cabin Cooling SystemSDR COMA9910148Switch · out of adjustSERVICE DOOR WARNING DURING TAKEOFF. ADJUSTED FUEL SERVICE DOOR SWITCH.Sep 16, 1999 · N261CA · Emb EMB120RT · Door Warning SystemSDR COMA9910115Sign · brokenEXIT SIGN AT ROW 8 IS BROKEN. REPLACED SIGN.Jul 19, 1999 · N261CA · Emb EMB120RT · Emergency LightingSDR COMA910113Warning · activatedTRIM INOPERABLE WARNING DURING TAKEOFF. COULD NOT DUPLICATE. RESET SYSTEM AND AIRCRAFT RETURNED TO SERVICE.Jul 17, 1999 · N261CA · Emb EMB120RT · Central WarningSDR COMA9910103Circuit Breaker · trippedTHE FLIGHT IDLE STOP SOLENOID CIRCUIT BREAKERS ARE TRIPPED. RESET BREAKERS AND FUNCTION CHECK OF SYSTEM NORMAL.Jun 28, 1999 · N261CA · Emb EMB120RT · Power LeverSDR COMA9910092Sign · inoperativeEXIT SIGN AT ROW 5 IS INOP. REPLACED EXIT SIGN.Jun 6, 1999 · N261CA · Emb EMB120RT · Emergency LightingSDR 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.Jan 22, 1999 · N261CA · Emb EMB120RT · Propeller Indication SystemSDR COMA9910017Actuator · leakingLT MLG DISAGREEMENT INDICATION WHEN LANDING GEAR RETRACTED. REPLACED THE LT MLG RETRACT ACTUATOR.Jan 21, 1999 · N261CA · Emb EMB120RT · Landing Gear Actuator
Back to N261CA, cancelled May 5, 2006