N257CA, cancelled Jul 11, 2013

Service difficulty reports · 105

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 = 'N257CA' AND deregistration_id = 'N257CA-2013-07-11'
  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 COMA0110023Skin · dentedTHE AIRCRAFT CARGO DOOR SKIN IS PULLED OUT AT FORWARD UPPER CORNER AREA. THE CARGO SKIN WAS REPAIRED BY ADDING A DOUBLER IN ACCORDANCE WITH AERODESIGN REPORT 3872-1, REV IR DATED 1-18-01.Jan 18, 2001 · N257CA · Emb EMB120RT · Cargo/Baggage DoorsSDR COMA0110007Controller · malfunctionedAIRCRAFT WILL NOT PRESSURIZE. REPLACED THE PRESSURIZATION HAND CONTROLLER.Jan 9, 2001 · N257CA · Emb EMB120RT · Cabin Pressure ControllerSDR COMA0110005Outflow Valve · malfunctionedAIRCRAFT WOULD NOT PRESSURIZE. REPLACED THE OUTFLOW VALVE.Jan 7, 2001 · N257CA · Emb EMB120RT · Pressure Regulator/Outflow ValveSDR COMA0010407Battery · dischargedFORWARD SECTION OF EMREGENCY FLOOR LIGHTING IS INOPERABLE. REPLACED EMERGENCY BATTERY.Dec 3, 2000 · N257CA · Emb EMB120RT · Emergency LightingSDR COMA0010301Battery · dischargedEMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY BATTERY.Jul 13, 2000 · N257CA · Emb EMB120RT · Emergency LightingSDR COMA0010206Switch · out of adjAUTO FEATHER WARNING DURING TAKEOFF. ADJUSTED THE RIGHT HAND POWER LEVER ARMING MICROSWITCH.Jun 25, 2000 · N257CA · Emb EMB120RT · Propeller Feathering/ReversingSDR COMA0010205Signal Cond Unit · malfunctionedAUTO FEATHER WARNING DURING TAKEOFF. REPLACED THE LEFT ENGINE TORQUE SIGNAL CONDITIONER.Jun 23, 2000 · N257CA · Emb EMB120RT · Propeller Feathering/ReversingSDR COMA0010204Switch · malfunctionedAUTO FEATHER CONFIG WARNING DURING TAKEOFF. REPLACED SWITCHES SO 299 AND SO 300 IN POWER LEVER QUADRANT.Jun 21, 2000 · N257CA · Emb EMB120RT · Propeller Feathering/ReversingSDR COMA0010203Sensor · out of adjTAKEOFF TRIM CONFIG WARNING. ADJUSTED THE LEFT HAND ELEVATOR TRIM PROXIMITY SENSOR.Jun 19, 2000 · N257CA · Emb EMB120RT · Elevator Tab Control SystemSDR COMA011008Crossbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-121/122-011 THE FRAME 12 CROSS BEAM WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0010159Clip · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5720-522-0II, THE RIB NR 5 SKIN CLIP WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Wing Main, Frame StructureSDR COMA0010158Frame · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 161/162-01Z, THE FRAME 43 CHANNEL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 3674-2.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Main, FrameSDR COMA0010157Angle · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5320-243/244-02I, THE WING TO FUSE FAIRING LOWER ATTACH ANGLES WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 1226-9.May 31, 2000 · N257CA · Emb EMB120RT · Wing Miscellaneous StructureSDR COMA0010156Beam · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z, THE CENTER OMEGA BEAM WAS FOUND TO BE CRACKED IN TWO PLACES AND CORRODED IN ANOTHER. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 1716-5.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010155Channel · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 811-02Z, DOOR CHANNEL WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Passenger/Crew DoorsSDR COMA0010154Shear Tie · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-221/222-15I, THE FRAME 9 LEFT AND RIGHT SKIN SUPPORTS WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 660-1.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0010153Frame · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 141/142-01Z, THE FRAME 22 CHANNEL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 3674-1.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Main, FrameSDR COMA0010152Floorbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 151/152-01Z, THE RT FLOOR CROSSBEAM FRAME 33 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA0010151Threshold · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 161/162-01Z, THE CARGO AFT RIGHT HAND SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 3661-1.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010150Threshold · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 161/162-01Z, THE CARGO FORWARD RIGHT HAND SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 3661-2.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010149Floorbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z, THE RIGHT HAND FLOOR CROSSBEAM AT FRAME 19 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA0010148Floorbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z, THE FRAME 16 FLOOR T SECTION WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA0010147Support Bracket · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 231/232-01Z, THE RIGHT HAND FORWARD SIDEWALL SEAT TRACK SUPPORT WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010146Threshold · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z, THE RIGHT HAND NR 1 SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010145Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z, THE RIGHT HAND NR 1 BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA0010144Floorbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 141/142-01Z, THE LEFT HAND FLOOR CROSSBEAM AT FRAME 23 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA0010143Floor Support · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z, THE LEFT HAND FLOOR SUPPORT T-SECTION AT FRAME 16 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010142Support Bracket · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 231/232-01Z, THE LEFT HAND NR 1 SIDEWALL SEAT TRACK SUPPORT WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010141Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 151/152-01Z, THE LEFT HAND NR 6 BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010140Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 151/152-01Z, THE LEFT HAND NR 4 BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010139Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 141/142-01Z, THE LEFT HAND NR 2 BUTT STRAP WAS FOUND TO BE CORROCED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA0010138Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z, THE LEFT HAND NR 1 BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010137Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z, THE CENTER NR 1 BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-12O STRUCTURAL REPAIR MANUALSTANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010136Plate · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z, THE LT FWD BUTT PLATE WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 1671-2.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010135Plate · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z, THE CENTER FWD BUTT PLATE WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 1671-1.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010134Shear Tie · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-121/122-O1I, THE FRAME 12 SKIN SUPPORT WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 3653-1.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0010133Channel · corrodedUPON COMPLICANCE OF 2C INSPECTION TASK 5310-121/122-01I, THE FRAME 12 Z SECTION WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0010132Shear Tie · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 261/262-01Z, THE FRAME 40 SKIN SUPPORT WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0010130Floorbeam · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-121/122-01I, THE LEFT AND RIGHT FLOOR PROP ANGLES WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 3647-1.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA0010129Receptacle · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 152-01Z, THE ROW 8 P/N RECEPTACLES WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUALSTANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010128Seat Track · corrodedUPON COMPLIANCE OF 2C INSPECTION THE FOLLOWING P/N SEAT TRACKS WERE FOUND WITH CORROSION AND REPLACED WITH FACTORY REPLACEMENT PARTS: 120-26865-005, 120-15997-603, 120-26864-005 , 120-15994-003 , 120-47507-001, 120-16000-603, 120-15996-005, 120-15995-007, 12May 31, 2000 · N257CA · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR COMA0010127Angle · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 152-01Z, THE ROW 8 EXIT ANGLE WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010061Placard · missingEMERGENCY EXIT PLACARD MISSING. REPLACED PLACARD.Apr 30, 2000 · N257CA · Emb EMB120RT · Placards and MarkingsSDR COMA0010040Switch · out of adjCARGO DOOR WARNING AFTER TAKEOFF. ADJUSTED DOOR WARNING MICRO SWITCH.Mar 22, 2000 · N257CA · Emb EMB120RT · Door Warning SystemSDR COMA0010043Bracket · looseCARGO DOOR WARNING AFTER TAKEOFF. SECURED LOOSE BRACKET AT CARGO DOOR WARNING MICRO SWITCH.Mar 22, 2000 · N257CA · Emb EMB120RT · Door Warning SystemSDR COMA9910173Warning · activatedCARGO DOOR WARNING DURING TAKEOFF. DEFERRED DOOR WARNING, AIRCRAFT CONTINUED SERVICE.Nov 16, 1999 · N257CA · Emb EMB120RT · Door Warning SystemSDR COMA9910069Sensor · malfunctionedWHEN LANDING GEAR SELECTED UP, THE NLG INTRANSIT LIGHT REMAINED ON. REPLACED THE NLG UPLOCK PROXIMITY SENSOR.May 2, 1999 · N257CA · Emb EMB120RT · Landing Gear Position and WarningSDR COMA9910064Fuel Line · leakingFUEL LEAK LEFT ENGINE. REPLACED LEAKING FUEL LINE AT LEFT HAND ENGINE FUEL CONTROL UNIT.Apr 20, 1999 · N257CA · Emb EMB120RT · Engine Fuel DistributionSDR COMA9910046Skin · crackedDURING 2,000 FLIGHT CYCLE CHECK, FOUND CRACK EXTENDING FROM RIVET HOLE FORWARD ON RIGHT SIDE BETWEEN RIGHT DV WINDOW AND RJ WINDSHIELD (POST SKIN). REPAIRED DAMAGED AREA IAW EMB FAX EST 474/95 DATED 01 NOVEMBER 95.Mar 26, 1999 · N257CA · Emb EMB120RT · Fuselage Main, Plate/SkinSDR COMA9910045Sign · brokenEMERGENCY EXIT SIGN AT ROW 8 IS BROKEN. REPLACED EXIT SIGN.Mar 19, 1999 · N257CA · Emb EMB120RT · Emergency Lighting
Back to N257CA, cancelled Jul 11, 2013