Embraer EMB-120

Service difficulty reports · 605

Newest first. General aviation reporting is voluntary.

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 aircraft_model_key = 'EMB120'
  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 AU010366Connector · faulty(AUS) AUTOFEATHER SYSTEM FAULTY. INSPECTION OF THE SYSTEM AND CLEANING OF CONNECTOR PLUGS CARRIED OUT. NO DEFECTS EVIDENT.Apr 3, 2001 · Emb EMB120 · Propeller Feathering/ReversingSDR AU010300Actuator · failed(AUS) LT OUTBOARD FLAP ACTUATOR FAULTY.Mar 26, 2001 · Emb EMB120 · Trailing Edge Flap ActuatorSDR GLBA2001064Sensor · inoperativeABORTED T/O, RIGHT NH INDICATOR FAILED. REPLACED NH SENSOR, OPS CHECKED SYSTEM GOOD.Mar 26, 2001 · N96ZK · Emb EMB120 · Engine RPM Indicating SystemSDR AU010288Controller · faulty(AUS) OUTBOARD FLAP DISAGREEMENT WARNING. INSPECTION COULD FIND NOFAULTS.Mar 25, 2001 · Emb EMB120 · Trailing Edge Flap Control SystemSDR AUS20010442Wire · worn(AUS) CABIN LIGHTING SYSTEM INVERTER OUTPUT WIRING CHAFING AGAINST GASPER AIR DUCT CAUSING THE WIRING LOOM AND DUCT INSULATION TO BURN.Mar 21, 2001 · Emb EMB120 · Light System WiringSDR AU010218Connector · contaminated(AUS) LT ENGINE TORQUE SIGNAL CONDITIONER AND ENGINE ELECTRONIC CONTROL (EEC) ELECTRICAL CONNECTORS CONTAMINATED WITH OIL.Mar 7, 2001 · Emb EMB120 · Fuel Control/Turbine EnginesSDR AU010186Blade · cracked(AUS) PROPELLER BLADE NICKEL SHEATH CRACKED. CRACK LENGTH APPROXIMATELY 50.8MM (2IN) LOCATED ON THE FACE APPROXIMATELY 50.8MM (2IN) FROMTHE BLADE HEATER.Mar 5, 2001 · Emb EMB120 · Propeller Blade SectionSDR AU010181Blade · damaged(AUS) LT PROPELLER NR 1 BLADE DAMAGED BY FOD. LEADING EDGE SHEATH HAD APIECE MISSING APPROXIMATELY 10MM (0.393IN) IN DIAMETER. THE LEFT FRONT PASSENGER WINDOW BEHIND THE GALLEY HAD A LARGE IMPACT MARK APPROXIMATELY 12MM (0.472IN) IN DIAMETER.Feb 27, 2001 · Emb EMB120 · Propeller Blade SectionSDR AU010153Skin · cracked(AUS) SKIN SURROUNDING THE COPILOTS WINDOW FRAME CRACKED.Feb 13, 2001 · Emb EMB120 · Fuselage Main, Plate/SkinSDR AU010152Disk · broken(AUS) BRAKE ROTATING DISC (CARRIER AND LINING ASSEMBLY) BROKEN.Feb 13, 2001 · Emb EMB120 · BrakeSDR AU010134Beam · corroded(AUS) FLIGHT ATTENDANTS SEAT SUPPORT FRAMES CORRODED.Feb 7, 2001 · Emb EMB120 · Fuselage Miscellaneous StructureSDR AU010133Beam · corroded(AUS) FLIGHT ATTENDANT SEAT SUPPORT FRAMES CORRODED.Feb 7, 2001 · Emb EMB120 · Fuselage Miscellaneous StructureSDR AU010136Outflow Valve · faulty(AUS) PRESSURISATION SYSTEM OUTFLOW VALVE FAULTY.Feb 6, 2001 · Emb EMB120 · Pressure Regulator/Outflow ValveSDR AU010126Door · separated(AUS) RT HYDRAULIC BAY DOOR FAILED AND SEPARATED DURING FLIGHT. DOORHAD BEEN OPENED FOR MAINTENANCE BEFORE FLIGHT AND IT IS SUSPECTED THAT IT WAS NOT PROPERLY CLOSED AND LATCHED.Feb 6, 2001 · Emb EMB120 · Hydraulic Compartment DoorsSDR AU010089Fitting · leaking(AUS) HYDRAULIC FITTING LOCATED IN LT OUTBOARD NACELLE LEAKING UNDERPRESSURE.Feb 5, 2001 · Emb EMB120 · Hydraulic System, MainSDR ASOA01016Detector · malfunctionedFLT 4240 - DURING FLIGHT FROM ILM-ATL, LEFT DUCT LEAK LIGHT ILLUMINATED. CAPTAIN FOLLOWED POH AND SHUTDOWN ENGINE. AIRCRAFT DIVERTED TO MYR AND LANDED SAFELY. MAINTENANCE OPERATED AIRCRAFT AT 60 PERCENT TORQUE FOR 10 MINUTES AND THEN WENT UP TO 95 PERCENT TJan 31, 2001 · N262AS · Emb EMB120 · Overheat DetectionSDR AU010074Blade · damaged(AUS) LT PROPELLER BLADE DAMAGED BY MISSING SPINNER ATTACHMENT SCREW. THREE SCREWS MISSING FROM SPINNER. ONE SCREW WAS FOUND EMBEDDED IN THE PROPELLER BLADE. MAINTENANCE HAD BEEN CARRIED OUT ON THE PROPELLER PRIOR TO THE FLIGHT.Jan 29, 2001 · Emb EMB120 · Propeller Blade SectionSDR ASOA01014Battery · dischargedDURING INSPECTION, CREW FOUND ROW 5 EMERGENCY FLOOR TRACKING LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY BATTERY. OPS CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)Jan 29, 2001 · N262AS · Emb EMB120 · Emergency LightingSDR AU010069Pin · loose(AUS) NOSE WHEEL STEERING RELAY BOX CONNECTOR PIN LOOSE.Jan 28, 2001 · Emb EMB120 · Landing Gear Steering SystemSDR R7MR32667Hinge · wornELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNITS FROM 1 EACH KIT PART NUMBER 355A33-2153-00, CORRECTED PROBLEM. 2 TEETERING BEARINGS EQUALS 1 KIT.Jan 25, 2001 · N92GL · Emb EMB120 · Tail Rotor BladesSDR AU010030Switch · faulty(AUS) AIR CONDITIONING SYSTEM CROSS BLEED VALVE SWITCH FAULTY.Jan 13, 2001 · Emb EMB120 · Cabin Cooling SystemSDR 20010206CW008Stator · crackedBRAKE ASSEMBLY PN2-1661 FAILED PREMATURELY. NR 2 STATOR CRACKED THROUGH AT 1 RELIEF HOLE, BINDING ON TORQUE TUBE.NOTE: OEM PARTS INSTALLED IN BRAKE ASSEMBLY AND THE MOST RECENT BRAKE CONFIGURATION PN 2-1661.Jan 11, 2001 · Emb EMB120 · BrakeSDR GLBA2001005Connector · contaminatedRETURN TO BLOCK - FLAP DISAGREEMENT AFTER T/O. CLEANED AND REMOVED GLYCOL FROM ACTUATOR CANNON PLUG, OPS CHECKED SYSTEM GOOD.Jan 10, 2001 · N96ZK · Emb EMB120 · Trailing Edge Flap ActuatorSDR GLBA20010002Connector · contaminatedRETURN TO BLOCK - FLAP DISAGREEMENT AFTER T/O. CLEANED AND REMOVED GLYCOL FROM ACTUATOR CANNON PLUG, OPS CHECKED SYSTEM GOOD.Jan 10, 2001 · N96ZK · Emb EMB120 · Trailing Edge Flap ActuatorSDR 20010129CW018Stator · crackedBRAKE ASSEMBLY PN 21661 FAILED PREMATURELY. NR2 STATOR CRACKED AT RELIEF HOLES. 25 PERCENT OF STATOR MISSING. HEAT STACK WARPED AND UNEVEN WEAR.NOTE OEM PARTS INSTALLED IN BRAKE ASSEMBLY AND THE MOST RECENT BRAKE CONFIGURATION PN 21Jan 9, 2001 · Emb EMB120 · BrakeSDR AU001251Generator · failed(AUS) NR 2 (RT) MAIN GENERATOR FAILED.Dec 13, 2000 · Emb EMB120 · DC Generator-AlternatorSDR AU001184Adc · faulty(AUS) AIR DATA COMPUTER (ADC) FAULTY.Dec 6, 2000 · Emb EMB120 · Air Data ComputerSDR AU001149Engine · making metal(AUS) LH ENGINE CHIP DETECTOR METAL CONTAMINATION. FOURTH STAGE TURBINE DAMAGED.Dec 4, 2000 · Emb EMB120 · Turbine SectionSDR AU001140Oxygen Mask · failed(AUS) PASSENGER OXYGEN MASKS FAILED TO DEPLOY AT 14,000 FEET. SUSPECT CAUSED BY DRY AND STIFF HINGES ON THE OXYGEN MASK DOORS DUE TOINFREQUENT USE AND SOLVENTS USED IN REPAINTING HAVING WASHED ANYLUBRICANT FROM THE HINGES. THE TOILET OXYGEN MASK DOOR ELECTRIC Nov 22, 2000 · Emb EMB120 · Passenger Oxygen SystemSDR AU001278Proximity Switch · faulty(AUS) NOSE LANDING GEAR SYSTEM B PROXIMITY SWITCH AND HARNESS SUSPECT FAULTY.Nov 16, 2000 · Emb EMB120 · Landing Gear Position and WarningSDR 20001108SH014Stator · crackedBRAKE ASSY, PN 2-1661, FAILED PREMATURELY. NR 1 STATOR CRACKED AT RELIEF HOLES. HEAT STACK WARPED AND UNEVEN WEAR. SUBMITTER STATED THIS IS A CONTINUAL DISCREPANCY. NOTE: OEM PARTS INSTALLED IN BRAKE ASSY, AND THE MOST RECENT BRAKE CONFIGURATION, PN 2-166Oct 18, 2000 · Emb EMB120 · BrakeSDR 20001108SH015Stator · crackedBRAKE ASSY, PN 2-1661, FAILED PREMATURELY. NR 1 AND NR 2 STATORS CRACKED AT RELIEF HOLES. HEAT STACK WARPED AND UNEVEN WEAR. SUBMITTER STATED THIS IS A CONTINUAL DISCREPANCY. NOTE: OEM PARTS INSTALLED IN BRAKE ASSY, AND THE MOST RECENT BRAKE CONFIGURATIONOct 17, 2000 · Emb EMB120 · BrakeSDR 20001108SH009Stator · crackedBRAKE ASSY, PN 2-1661, FAILED PREMATURELY. NR 1 AND NR 2 STATOR CRACKED AT RELIEF HOLES. HEAT STACK WARPED AND UNEVEN WEAR. SUBMITTER STATED THIS IS A CONTINUAL DISCREPANCY. NOTE: OEM PARTS INSTALLED IN BRAKE ASSY AND THE MOST RECENT BRAKE CONFIGURATION,Oct 17, 2000 · Emb EMB120 · BrakeSDR 20001108SH005Stator · crackedBRAKE ASSY, PN 2-1661, FAILED PREMATURELY. NR 1 AND NR 2 STATORS CRACKED AT RELIEF HOLES. HEAT STACK WARPED AND UNEVEN WEAR. SUBMITTER STATED THIS IS A CONTINUAL DISCREPANCY. NOTE: OEM PARTS INSTALLED IN BRAKE ASSY, AND THE MOST RECENT BRAKE CONFIGURATIONOct 16, 2000 · Emb EMB120 · BrakeSDR 20001108SH017Stator · crackedBRAKE ASSY, P/N 2-1585-R, FAILED PREMATURELY. NR 1 AND NR 2 STATORS CRACKED AT RELIEF HOLES. HEAT STACK WARPED AND UNEVEN WEAR. SUBMITTER STATED THIS IS A CONTINUAL DISCREPANCY. NOTE: RAPCO FLEET SUPPORT PARTS INSTALLED IN BRAKE ASSY. (X)Oct 14, 2000 · Emb EMB120 · BrakeSDR 20001108SH006Stator · crackedBRAKE ASSY, PN 2-15-85-R, FAILED PREMATURELY. NR 1 AND NR 2 STATORS CRACKED AT RELIEF HOLES. HEAT STACK WARPED AND UNEVEN WEAR. SUBMITTER STATED THIS IS A CONTINUAL DISCREPANCY. NOTE: RAPCO FLEET SUPPORT PARTS INSTALLED IN BRAKE ASSEMBLY. (X)Oct 14, 2000 · Emb EMB120 · BrakeSDR 20001108SH016Stator · crackedBRAKE ASSY, PN 2-1661, FAILED PREMATURELY. NR 1 AND NR 2 STATORS CRACKED AT RELIEF HOLES. HEAT STACK WARPED AND UNEVEN WEAR. SUBMITTER STATED THIS IS A CONTINUAL DISCREPANCY. NOTE: OEM PARTS INSTALLED IN BRAKE ASSY, AND THE MOST RECENT BRAKE CONFIGURATIONOct 13, 2000 · Emb EMB120 · BrakeSDR 20001108SH018Stator · crackedBRAKE ASSY, P/N 2-1661, FAILED PREMATURELY. NR 1 STATOR CRACKED AT RELIEF HOLES. HEAT STACK WARPED AND UNEVEN WEAR. SUBMITTER STATED THIS IS A CONTINUAL DISCREPANCY. NOTE: OEM PARTS INSTALLED IN BRAKE ASSY, AND THE MOST RECENT BRAKE CONFIGURATION, P/N 2-1Oct 12, 2000 · Emb EMB120 · BrakeSDR 20001108SH013Stator · crackedBRAKE ASSY, PN 2-1661, FAILED PREMATURELY. NR 1 AND NR 2 STATORS CRACKED AT RELIEF HOLES. HEAT STACK WARPED AND UNEVEN WEAR. SUBMITTER STATED THIS IS A CONTINUAL DISCREPANCY. NOTE: OEM PARTS INSTALLED IN BRAKE ASSY, AND THE MOST RECENT BRAKE CONFIGURATIONOct 12, 2000 · Emb EMB120 · BrakeSDR 20001108SH011Stator · crackedBRAKE ASSY, PN 2-1661, FAILED PREMATURELY. NR 1 AND NR 2 STATORS CRACKED AT RELIEF HOLES. HEAT STACK WARPED AND UNEVEN WEAR. SUBMITTER STATED THIS IS A CONTINUAL DISCREPANCY. NOTE: OEM PARTS INSTALLED IN BRAKE ASSY AND THE MOST RECENT BRAKE CONFIGURATIONOct 12, 2000 · Emb EMB120 · BrakeSDR 20001108SH010Stator · crackedBRAKE ASSY, PN 2-1661, FAILED PREMATURELY. NR 1 AND NR 2 STATORS CRACKED AT RELIEF HOLES. HEAT STACK WARPED AND UNEVEN WEAR. SUBMITTER STATED THIS IS A CONTINUAL DISCREPANCY. NOTE: OEM PARTS INSTALLED IN BRAKE ASSY AND THE MOST RECENT BRAKE CONFIGURATION,Oct 12, 2000 · Emb EMB120 · BrakeSDR 20001108SH007Stator · crackedBRAKE ASSY, PN 2-1661, FAILED PREMATURELY. NR 1 AND NR 2 STATORS CRACKED AT RELIEF HOLES. HEAT STACK WARPED AND UNEVEN WEAR. SUBMITTER STATED THIS IS A CONTINUAL DISCREPANCY. NOTE: OEM PARTS INSTALLED IN BRAKE ASSY AND THE MOST RECENT BRAKE CONFIGURATION,Oct 11, 2000 · Emb EMB120 · BrakeSDR AU000997Hmu · faulty(AUS) LT ENGINE HYDRO MECHANICAL UNIT (HMU) FAULTY.Oct 11, 2000 · Emb EMB120 · Fuel Control/Reciprocating EnginesSDR 20001108SH004Stator · crackedBRAKE ASSY, PN 2-1585-R, FAILED PREMATURELY. NR 2 STATOR CRACKED AT RELIEF HOLES. HEAT STACK WARPED AND UNEVEN WEAR. SUBMITTER STATED THIS IS A CONTINUAL DISCREPANCY. NOTE: RAPCO FLEET SUPPORT PARTS INSTALLED IN BRAKE ASSY. (X)Oct 10, 2000 · Emb EMB120 · BrakeSDR AU000978Engine · malfunctioned(AUS) NR 1 ENGINE OIL PRESSURE LOW.Oct 10, 2000 · Emb EMB120 · Turbine Engine Oil SystemSDR 20001026SH017Stator · crackedBRAKE ASSEMBLY, PN 2-1585-R, FAILED PREMATURELY. NR 1 AND NR 2 STATORS CRACKED AT RELIEF HOLES. HEAT STACK WARPED AND UNEVEN WEAR. SUBMITTER STATED THIS IS A CONTINUAL DISCREPANCY. NOTE: RAPCO FLEET SUPPORT PARTS INSTALLED IN BRAKE ASSY. (X)Oct 10, 2000 · Emb EMB120 · BrakeSDR 20001108SH012Stator · crackedBRAKE ASSY, PN 2-1585-R, FAILED PREMATURELY. NR 1 AND NR 2 STATORS CRACKED AT RELIEF HOLES. HEAT STACK WARPED AND UNEVEN WEAR. SUBMITTER STATED THIS IS A CONTINUAL DISCREPANCY. NOTE: RAPCO FLEET SUPPORT PARTS INSTALLED IN BRAKE ASSY. (X)Oct 9, 2000 · Emb EMB120 · BrakeSDR 20001024SH009Stator · crackedBRAKE ASSY, PN 2-1585-R, FAILED PREMATURELY. NR 1 AND NR 2 STATORS CRACKED AT RELIEF HOLES. HEAT STACK WARPED AND UNEVEN WEAR. SUBMITTER STATED THIS IS A CONTINUAL DISCREPANCY. NOTE: RAPCO FLEET SUPPORT PARTS INSTALLED IN BRAKE ASSEMBLY. (X)Oct 4, 2000 · Emb EMB120 · BrakeSDR 20001024SH010Stator · crackedBRAKE ASSY, P/N 2-1661, FAILED PREMATURELY. NR 1 AND NR 2 STATORS CRACKED AT RELIEF HOLES. HEAT STACK WARPED AND UNEVEN WEAR. SUBMITTER STATED THIS IS A CONTINUAL DISCREPANCY. NOTE: OEM PARTS INSTALLED IN BRAKE ASSY AND THE MOST RECENT BRAKE CONFIGURATIONOct 2, 2000 · Emb EMB120 · BrakeSDR 20001024SH011Stator · crackedBRAKE ASSEMBLY, PN 2-1585-R, FAILED PREMATURELY. NR 1 STATOR BROKEN THROUGH. NR 2 STATOR CRACKED AT RELIEF HOLES. HEAT STACK WARPED AND UNEVEN WEAR. SUBMITTER STATED THIS IS A CONTINUAL DISCREPANCY. NOTE: RAPCO FLEET SUPPORT PARTS INSTALLED IN BRAKE ASSYSep 30, 2000 · Emb EMB120 · Brake
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