N266CA, cancelled Aug 21, 2012

Service difficulty reports · 59

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 = 'N266CA' AND deregistration_id = 'N266CA-2012-08-21'
  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 COMA0110040Battery · dischargedAFT CABIN EMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY BATTERY.Mar 6, 2001 · N266CA · Emb EMB120RT · Emergency LightingSDR COMA0110002Relay · malfunctionedAFTER GEAR RETRACTION, HYDRAULIC LOW LEVEL WARNING. GEAR DOORS DID NOT CLOSE. REPLACED THE LANDING GEAR RELAY BOX.Dec 28, 2000 · N266CA · Emb EMB120RT · Landing Gear Position and WarningSDR COMA0010304Skin · gougedUPON COMPLIANCE OF 2 YEAR CORROSION INSPECTION TASK 5310-132-C01E, THE FUSELAGE RT LOWER SKIN BELOW LAV DUMP VALVE DOUBLER WAS FOUND TO BE GOUGED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMBRAER REPAIR NR SST-Jul 14, 2000 · N266CA · Emb EMB120RT · Fuselage Main, Plate/SkinSDR COMA0010277Skin · gougedUPON COMPLIANCE OF 2 YEAR CORROSION INSPECTION TASK 5310-132-CO1E, THE FUSELAGE RT LOWER SKIN BELOW LAV DUMP VALVE DOUBLER WAS FOUND TO BE GOUGED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMBRAER REPAIR NR SST-Jul 14, 2000 · N266CA · Emb EMB120RT · Fuselage Main, Plate/SkinSDR COMA0060457Battery · dischargedEMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY LIGHT BATTERY.May 25, 2000 · N266CA · Cndair CL6002B19 · Emergency LightingSDR COMA0010107Adi · malfunctionedNR 1 ADI FLICKERING. REPLACED THE NR 1 ADI.May 20, 2000 · N266CA · Emb EMB120RT · Attitude and Direction Data SystemSDR COMA0010039Radar · malfunctionedRADAR SPOKING DURING SWEEPS. REPLACED THE WX RADAR RT WXT-25013.Mar 16, 2000 · N266CA · Emb EMB120RT · Weather Radar SystemSDR COMA9910171Mechanism · lack of lubeDOOR WARNING DURING FLIGHT. CLEANED AND LUBED DOOR MECHANISM.Nov 4, 1999 · N266CA · Emb EMB120RT · Passenger/Crew DoorsSDR COMA9910156Switches · dirtyAFTER DEPARTURE FROM LAN, THE CABIN DOOR WARNING CAUTION ACTIVATED ON MAP. AIRCRAFT RETURNED TO THE FIELD. CLEANED ALL CABIN DOOR MICROSWITCHES, OPERATIONAL CHECK INDICATED CABIN DOOR INDICATING SYSTEM SATISFACTORY.Oct 3, 1999 · N266CA · Emb EMB120RT · Door Warning SystemSDR COMA9910118Door · not closedSERVICE DOOR WARNING DURING TAKEOFF. FUEL SERVICE DOOR NOT COMPLETELY CLOSED. SECURED FUEL SERVICE DOOR.Jul 25, 1999 · N266CA · Emb EMB120RT · Fluid Service DoorsSDR COA9910095Sign · brokenEXIT SIGN AT ROW 5 IS BROKEN. REPLACED EXIT SIGN.Jun 17, 1999 · N266CA · Emb EMB120RT · Emergency LightingSDR COMA9910051Handle · brokenLEFT MAIN LANDING GEAR DOOR WILL NOT CLOSE. REPLACED GEAR DOOR HANDLE.Mar 31, 1999 · N266CA · Emb EMB120RT · Landing Gear DoorsSDR COMA9810255Battery · dischargedEMERGENCY LIGHTING IS WEAK. REPLACED EMERGENCY BATTERY.Nov 4, 1998 · N266CA · Emb EMB120RT · Emergency LightingSDR COMA9810227Engine · malfunctionedRIGHT HAND ENGINE NP WAS 104 PERCENT AFTER TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. GROUND RUNS AND FLIGHT CHECK WERE SATISFACTORY.Oct 5, 1998 · N266CA · Emb EMB120RT · Engine (Turbine/Turboprop)SDR COMA9810178Ahrs · malfunctionATTITUDE DISPLAY WARNING DURING TAKEOFF. REPLACED THE NR 1 AHRS.Aug 14, 1998 · N266CA · Emb EMB120RT · Integrated Flight SystemSDR COMA9810161Battery · dischargedEMERGENCY LIGHTS ROW 1 AND 2 ARE INOPERABLE. REPLACED EMERGENCY BATTERY.Jul 19, 1998 · N266CA · Emb EMB120RT · Emergency LightingSDR COMA9810149Sign · brokenEMERGENCY EXIT SIGN AT ROW 5 BROKEN. REPLACED SIGN.Jun 28, 1998 · N266CA · Emb EMB120RT · Emergency LightingSDR COMA9810065Fan · overheatedSTRONG ELECTRICAL SMELL IN COCKPIT. RIGHT HAND RECIRCULATION FAN CIRCUIT BREAKER TRIPPED. REPLACED THE RIGHT HAND RECIRCULATION FAN.Mar 14, 1998 · N266CA · Emb EMB120RT · Air Distribution FanSDR COMA9710509Brush Block · wornRIGHT HAND PROPELLER DE-ICE FAILED. REPLACED THE BRUSH BLOCK ASSY.Dec 24, 1997 · N266CA · Emb EMB120RT · Propeller/Rotor Anti-Ice/De-Ice SystemSDR COMA9710490Rccb · malfunctionLEFT HAND PROPELLER DE-ICE FAILED DURING FLIGHT. REPLACED THE LEFT HAND PROPELLER DE-ICE SYSTEM RCCB.Dec 6, 1997 · N266CA · Emb EMB120RT · Propeller/Rotor Anti-Ice/De-Ice SystemSDR COMA9710488Light · looseEMERGENCY FLOOR LIGHT AT GALLEY AREA IS LOOSE. SECURED FLOOR LIGHT ASSY.Dec 2, 1997 · N266CA · Emb EMB120RT · Emergency LightingSDR COMA9710435Bracket · crackedUPON REPLACEMENT OF A BROKEN CARGO DOOR LIFTING MECHANISM TORSION BAR, THE TORSION BAR SUPPORT BRACKET BETWEEN FUSELAGE FRAMES 38 AND 39, WAS FOUND TO BE CRACKED. THE BRACKET WAS REPLACED PER AERODESIGN REPORT NR 1397-1, REV IR 2-15-95, AND EMBRAER FAX NR TPEOct 21, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710417Stator · crackedDURING TEARDOWN OF BRAKE ASSY P/N 2-1585, THE ACCESSORY SHOP FOUND THE NUMBER ONE STATOR CRACKED. OVERHAULED BRAKE.Sep 22, 1997 · N266CA · Emb EMB120RT · BrakeSDR COMA9710209Frame · burnedON 2C TAS K 313-01Z, FUSELAGE FRAME 52 CANTED FRAME, UPPER HALF, WAS FOUND DAMAGED BY ARCING OF THE APU GENERATOR WIRE TERMINALS BOLTED TO THE FRAME. THE FRAME UPPER HALF WAS REPLACED PER SRM CHAP 51 STANDARD PRACTICES AND THE APU FIREWALL WAS REPAIRED PER SRMar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Main, FrameSDR COMA9710208Beam · corrodedON 2C TASK 5310-131/132-O1I, THE CABIN DOOR FLOOR SUPPORT FORWARD CENTER OMEGA BEAM WAS FOUND DAMAGED IN THREE PLACES, 1) CORROSION, 2) SMALL CRACK, 3) HOLE CAUSED BY CARPET TRIM SCREW IMPROPERLY INSTALLED. THE OMEGA BEAM WAS REPAIRED PER AERODESIGN REPORT NRMar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710207Frame · cougedON 4C TASK 5330-262-01I, FUSELAGE FRAME 44 WAS FOUND DAMAGED BY CARGO COMPARTMENT LINING SCREWS IMPROPERLY INSTALLED ON RT SIDE. FRAME 44 WAS REPAIRED PER AERODESIGN REPORT NR 2243-1,REV.IR, 3-26-97.Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Main, FrameSDR COMA9710206Angle · corrodedON 4C TASK 5320-152-01I, THE FUSELAGE DOOR FRAME, FOR THE RT AFT EMERGENCY EXIT LOWER ANGLE WAS FOUND CORRODED, WHERE THE EXIT DOOR LOWER GUIDE PIN RECEPTACLES (P/N 120-27743-001) ARE ATTACHED TO IT. THE RECEPTACLES AND THE ANGLE WERE REPLACED PER SRM CHAP 51Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710205Butt Strap · corrodedON 2C TASK 5320-141-03I, THE CABIN FLOORBEAM LT BUTT-STRAP WAS FOUND CORRODED. REPLACED PER SRM CHAP 51 STANDARD PRACTICES.Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710204Tee Section · corrodedON 2C TASK 5310-131-01I, THE CABIN FLOOR SUPPORT LT T-SECTION OF FRAME 20 WAS FOUND CORRODED. REPLACED PER SRM CHAP 51 STANDARD PRACTICES.Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710203Crossbeam · corrodedON 2C TASK 5310-131-01I, THE CABIN FLOOR SUPPORT LT CROSSBEAM AT FRAME 20 WAS FOUND CORRODED. REPLACED PER SRM CHAP 51 STANDARD PRACTICES.Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710202Sill · corrodedON 2C TASK 5310-131-01I, THE CABIN FLOOR SUPPORT FORWARD LT SILL WAS FOUND CORRODED. REPLACED PER SRM CHAP 51 STANDARD PRACTICES.Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710200Tee Section · corrodedON 2C TASK 5310-131-01I, THE CABIN FLOOR SUPPORT LT T-SECTION AT FRAME 16 WAS FOUND CORRODED. REPLACED PER SRM CHAP 51 STANDARD PRACTICES.Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710199Crossbeam · corrodedON 2C TASK 5310-132-01I, THE CABIN FLOOR SUPPORT RT CROSSBEAM AT FRAME 16 WAS FOUND CORRODED. REPLACED PER SRM CHAP 51 STANDARD PRACTICES.Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710198Butt Strap · corrodedON 2C TASK 5310-132-01I, THE FORWARD RT FLOOR BEAM BUTT STRAP WAS FOUND CORRODED. REPLACED PER SRM CHAP 51 STANDARD PRACTICES.Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710197Butt Strap · corrodedON 2C TASK 5310-131-01I, THE FORWARD LEFT FLOORBEAM BUTT-STRAP, WAS FOUND CORRODED. REPLACED PER SRM CHAP 51 STANDARD PRACTICES.Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710196Butt Strap · corrodedON 2C TASK 5310-131/132-01I, THE CABIN FLOORBEAM CENTER BUTT STRAP WAS FOUND CORRODED. REPLACED PER SRM CHAP 51 STANDARD PRACTICES.Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710195Butt Strap · corrodedON 2C TASK 5310-131/132O1I, THE FORWARD CABIN FLOOR SUPPORT CENTER BUTT STRAP WAS FOUND CORRODED. REPLACED PER AERODESIGN REPORT NR 1671-1, REV. A, 1-28-97.Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710194Angle · crackedON 2C TASK 5720-651-01I, THE RIGHT WING LOWER SKIN SUPPORT ANGLE, AT RIB 16, BETWEEN STRINGERS 8 AND 10, WAS FOUND CRACKED. THE ANGLE WAS REPLACED PER SRM CHAP 51 STANDARD PRACTICES.Mar 27, 1997 · N266CA · Emb EMB120RT · Wing Miscellaneous StructureSDR COMA9710193Angle · crackedON 2C TASK 5720-622-01I, THE RIGHT WING LOWER SKIN SUPPORT ANGLE WAS FOUND CRACKED AT RIB 8, BETWEEN STRINGERS 10 AND 11. THE ANGLE WAS REPLACED PER SRM CHAP 51 STANDARD PRACTICES.Mar 27, 1997 · N266CA · Emb EMB120RT · Wing Miscellaneous StructureSDR COMA9710157Roller · dirtyFLAP DISAGREEMENT WARNING WHEN FLAPS RETRACTED AFTER TAKE OFF. REPLACED OUTBOARD FLAP ROLLERS.Feb 23, 1997 · N266CA · Emb EMB120RT · Trailing Edge FlapsSDR COMA9710152Switch · malfunctionFLAP DISAGREE WARNING AFTER TAKEOFF. REPLACED THE FLAP SELECTOR HANDLE.Feb 14, 1997 · N266CA · Emb EMB120RT · Trailing Edge Flap Control SystemSDR COMA9710100Test Panel · malfunctionSTALL WARNING ACTIVATED DURING FLIGHT. REPLACED THE STALL TEST PANEL.Feb 2, 1997 · N266CA · Emb EMB120RT · Stall Warning SystemSDR COMA9610335Sig Cond Unit · malfunctionAUTOFEATHER WARNING SOUNDED AFTER TAKEOFF. REPLACED THE RT SIGNAL CONDITIONER UNIT.Nov 21, 1996 · N266CA · Emb EMB120RT · Propeller Controlling SystemSDR COMA9610329Sig Cond Unit · malfunctionAUTO COARSEN SYSTEM DID NOT ARM DURING TAKEOFF. REPLACED THE SIGNAL CONDITIONER UNIT.Nov 8, 1996 · N266CA · Emb EMB120RT · Propeller Controlling SystemSDR COMA9610328Fastener · wornSERVICE DOOR WARNING ON AFTER TAKEOFF. REPLACED LATCHES ON FUEL SINGLE POINT SERVICE DOOR AND SECURED DOOR CLOSED.Nov 8, 1996 · N266CA · Emb EMB120RT · Fluid Service DoorsSDR COMA9610294Relay Box · malfunctionLANDING GEAR RETRACTED NORMALLY AND INDICATED UP, BUT THE LANDING GEAR AURAL WARNING SOUNDED CONTINUOUSLY. REPLACED THE LANDING GEAR RELAY BOX.Oct 4, 1996 · N266CA · Emb EMB120RT · Landing Gear Position and WarningSDR COMA9610287Sequence Valve · malfunctionLANDING GEAR WILL NOT RETRACT. REPLACED LT MLG DOOR SEQUENCE VALVES.Sep 25, 1996 · N266CA · Emb EMB120RT · Landing Gear Door Retract SectionSDR COMA9610253Bulb · failedLT AFT EMERGENCY LIGHT IS INOP. REPLACED BULB.Aug 21, 1996 · N266CA · Emb EMB120RT · Emergency LightingSDR COMA9610245Pcu · leakingLEFT ENGINE LOW OIL PRESSURE WARNING DURING TAKEOFF. OIL LEAKING FROM LEFT NACELLE.Aug 8, 1996 · N266CA · Emb EMB120RT · Propeller Controlling SystemSDR COMA9610229Solenoid · failedLEFT POWER LEVER, FLIGHT IDLE STOP SOLENOID CIRCUIT BREAKER, TRIPPED. REPLACED THE FLIGHT IDLE STOP SOLENOID.Jul 21, 1996 · N266CA · Emb EMB120RT · Power Lever
Back to N266CA, cancelled Aug 21, 2012