Embraer EMB-120RT
Service difficulty reports · 5,310
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 = 'EMB120RT' 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 aircraft_model_key = 'EMB120RT' 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 C2XA97CL015Apu · failedCLE - FLT 3076 - CREW REPORTED SMOKE IN CABIN WITH A WARNING ALARM. MAINTENANCE INSPECTED THE AIRCRAFT AND AFTER EXTENSIVE TROUBLESHOOTING THE AUXILIARY POWER UNIT WAS REMOVED AND REPLACED IAW EMB-120 MM 49-00-02. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORSDR C2XA97IA048Engine · failedIAH - FLT 3718 - DURING CLIMB-OUT, AT 10,000 FEET, CREW EXPERIENCED COMPLETE POWER LOSS OF NR 2 ENGINE. CREW SHUT DOWN NR 2 ENGINE, FOLLOWING EMERGENCY CHECKLIST PROCEDURES, AND RETURNED TO IAH AND LANDED WITHOUT INCIDENT. PRIOR TO INCIDENT ALL ENGINE PARAMESDR C2XA97CL014Smoke Detector · looseCLE - FLT 3090 - CREW REPORTED THAT WHILE INBOUND TO CLE THE LAVATORY SMOKE WARNING SOUNDED CONTINUOUSLY, AIRCRAFT MADE AND UNEVENTFUL LANDING IN CLE. MAINTENANCE INSPECTED THE LAVATORY SMOKE DETECTOR AND SMOKE ALARM PANEL, AFTER RE-SEATING THE CONNECTORS THESDR C2XA97CL013De-Ice Boot · rupturedCLE - FLT 3293 - CREW REPORTED THAT BOTH THE LEFT AND RIGHT ENGINE AIR INLET DE-ICE SYSTEMS FAILED AFTER TAKEOFF. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE LEFT ENGINE AIR INLET DE-ICE BOOT IAW EMB 120 ER MMSDR GLBA97017Oil Press Warn · illuminatedORD - LEFT ENGINE OIL PRESSURE WARNING CAME ON AT V-1 DURING TAKEOFF. SECURED ENGINE AND LANDED. MAINTENANCE INSPECTED LEFT ENGINE AND RAN FOR 20 MINUTES. NO LEAKS AND ENGINE PARAMETERS WERE OK. (M)SDR COMA9710123Butt Strap · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE LT BUTT STRAP WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER SRM STANDARD PRACTICES.SDR COMA9710122Butt Strap · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT BUTT STRAP WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER SRM STANDARD PRACTICES.SDR COMA9710121Beam · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE LT OMEGA BEAM WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER SRM STANDARD PRACTICES.SDR COMA9710120Butt Strap · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER SRM STANDARD PRACTICES.SDR COMA9710119Butt Strap · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER AERODESIGN REPORT NR 1671-1, REV A, DATED 1-28-97.SDR COMA9710118Sill · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT SILL WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER SRM STANDARD PRACTICES.SDR COMA9710117Sill · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT SILL WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER SRM STANDARD PRACTICES.SDR COMA9710116Sill · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT SILL WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER SRM STANDARD PRACTICES.SDR COMA9710115Sill · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT SILL WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER SRM STANDARD PRACTICES.SDR COMA9710114Sill · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT SILL WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER SRM STANDARD PRACTICES.SDR COMA9710113Supporting Sect · corrodedON 2C CHECK, THE LT SIDEWALL SEAT TRACK SUPPORTING SECTION WAS FOUND CORRODED. THE PART WAS REPLACED PER SRM STANDARD PRACTICES.SDR COMA9710112Supporting Sect · corrodedON 2C CHECK, THE RT SIDEWALL SEAT TRACK SUPPORTING SECTION WAS FOUND CORRODED. THE PART WAS REPLACED PER SRM STANDARD PRACTICES.SDR COMA9710111Crossbeam · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE LT CROSSBEAM WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER SRM STANDARD PRACTICES.SDR COMA9710110Support · corrodedON 2C CHECK, THE LOWER FUSELAGE SKIN SUPPORT AT FRAME 14 WAS FOUND CORRODED. THE PART WAS REPLACED PER EMB 120 SRM STANDARD PRACTICES.SDR COMA9710109Angle · corrodedON 2C CHECK, THE ATTACHING ANGLE AT STRINGER 18L, BETWEEN FRAMES 15 AND 15A WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER SRM STANDARD PRACTICES.SDR COMA9710108Supporting Sect · corrodedON 2C CHECK, THE RT FWD SIDEWALL SEAT TRACK SUPPORTING SECTION WAS FOUND CORRODED. THE PART WAS REPLACED PER SRM STANDARD PRACTICES.SDR COMA9710107Stringer · corrodedON 2C CHECK, THE FUSELAGE STRINGER 18L WAS FOUND TO BE CORRODED NEAR FRAME 16, THE STRINGER WAS REPAIRED PER AERODESIGN REPORT NR 1990-5, REV IR, DATED 1-28-97.SDR COMA9710106Sill · gougedON 2C CHECK, THE CARGO COMPARTMENT FLOOR SUPPORT LT SILL WAS FOUND DAMGED BY INTERIOR LINING SCREWS. THE SILL WAS REPLACED PER SRM STANDARD PRACTICES.SDR COMA9710105Skin · gougedON 2C CHECK, THE CARGO DOOR OUTER SKIN WAS FOUND TO BE GOUGED ALONG THE TOP EDGE, CAUSED BY THE FUSELAGE MOUNTED DOOR STOPS. THE SKIN WAS REPAIRED PER SRM 52-30-01, PG 201 TO 203.SDR COMA9710103Prop Blade · out of balanceVIBRATION FELT DURING TAXI, SUSPECT OUT OF BALANCE PROPELLER. REPLACED NR 4 BLADE ON RT PROPELLER.SDR COMA9710102Prox Sensor · failed'TAKE OFF TRIM' AURAL WARNING DURING TAKEOFF. REPLACED ELEVATOR TRIM TAB PROXIMITY SENSORS.SDR COMA9710101Connector · looseLT ANTI-SKID INOP WARNING DURING TAXI. SECURED LOOSE WIRING CONNECTOR AT THE RT ANTI-SKID TRANSDUCER.SDR COMA9710099Pitchlock Screw · damagedPROPELLER ASSEMBLY REMOVED FROM AIRCRAFT DUE TO BEING STRUCK BY LAVORATORY CART WHILE STATIC ON AIRCRAFT RAMP. DURING PROPELLER IMPACT INSPECTION ACTUATOR FEATHER STOP TAB WAS FOUND TO BE DISPLACED APPROXIMATELY .125 FEET. ACTUATOR S/N 20383 WAS SUBSEQUENTLYSDR C2XA97IA049Wire · brokenIAH - DURING A ROUTINE INSPECTION OF THE EMERGENCY LIGHTING SYSTEM, ONE FLOOR LEVEL EXIT PROXIMITY LIGHT FAILED TO ILLUMINATE. INSPECTED AND FOUND A BROKEN WIRE AT LIGHT SOCKET ADJACENT TO RIGHT AFT EMERGENCY EXIT. REPARIED WIRE AT LIGHT SOCKET, OPERATIONAL SDR WTAA970021Battery Pack · dischargedACV - OVERWING EXIT EMERGENCY LIGHTS AT ROW 5 REPORTED INOPERATIONAL. MAINTENANCE REPLACED CENTER EMERGENCY LIGHTS BATTERY PACK. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M)SDR COMA9710104Fcu · malfunctionFLAP CONTROL FAULT WARNING DURING TAXI. REPLACED THE FLAP CONTROL UNIT.SDR COMA9710100Test Panel · malfunctionSTALL WARNING ACTIVATED DURING FLIGHT. REPLACED THE STALL TEST PANEL.SDR COMA9710126Connector · looseWHEN FLAPS EXTENDED, INBOARD FLAPS REMAINED UP AND OUTBOARD FLAPS WENT FULL DOWN. REPAIRED LOOSE WIRE CONNECTOR AT THE FLAP CONTROL UNIT.SDR C2XA97CL011Manifold · failedCLE - FLT 3061 - CREW REPORTED THAT THE PEDAL STEERING LIGHT ILLUMINATED IN FLIGHT AND UNABLE TO EXTINGUISH IT. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE STEEING MANIFOLD IAW EMB-120 MM 32-50-04. OPERATIONASDR WTAA970019Camlock · failedFAT - SERVICE DOOR LIGHT ILLUMINATING ON TAKEOFF. TAKEOFF ABORTED. MAINTENANCE RESECURED FUEL DOOR CAMLOCK. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M)SDR COMA9710098Flap Contl Unit · malfunctionFLAP CONTROL FAULT WARNING DURING TAXI. REPLACED THE FLAP CONTROL UNIT. PART TOTAL CYCLES, 2,093.SDR COMA9710096Pitchlock Screw · bentACTUATOR ASSEMBLY REMOVED FROM AIRCRAFT DUE TO FEATHER STOP TAB BEING FOUND DISPLACED. AIRCRAFT BROUGHT IN FOR SCHEDULED MAINTENANCE. UPON INITIAL RECEIVING INSPECTION THE FEATHER STOP TAB S/N S0561 WAS FOUND TO BE BENT APPROXIMATELY 0.125 INCH. PITCHLOCK SSDR C2XA97CL010Transducer · failedTYS - FLT 212C - CREW REPORTED, COMPLETED A PRECAUTIONRAY RIGHT ENGINE SHUT DOWN DUE TO OIL PRESSURE INDICATING LESS THEN 20 PSI. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED THE RIGHT ENGINE AND REMOVED AND REPLACED THE ENGINE OIL PRESSURE TRANSDUCER ISDR COMA9710097Wire · chafedLANDING GEAR WARNING SOUNDS REPEATEDLY DURING FLIGHT. REPAIRED DEFECTIVE WIRING IN LANDING GEAR WARNING CIRCUIT.SDR COMA9710095Pitchlock Screw · bentACTUATOR ASSEMBLY REMOVED ORIGINALLY FOR PROPELLER FEATHERING PROBLEMS. UPON INITIAL RECEIVING INSPECTION THE FEATHER STOP TAB S/N S0159 WAS FOUND TO BE BENT APPROXIMATELY 0.25 INCH. PITCHLOCK SCREW WAS REMOVED FROM ASSEMBLY AND RETURNED TO MANUFACTURER. PASDR COMA9710091Hinge · brokenLT M.L.G. DOORS DO NOT CLOSE PROPERLY. REPLACED BROKEN DOOR HINGE ON LT M.L.G. AFT DOOR.SDR C2XA97IA043Support · corrodedIAH - DURING C-CHECK INSPECTION, THE TOILET FLUSH VALVE SUPPORT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SUPPORT AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA97IA042Stringer · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT WING STRINGER 10 WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE AFFECTED PORTION OF STRINGER USING A SPLICE REPAIR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA97IA041Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT WALL SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA97IA040Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT SIDEWALL SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA97IA039Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT FORWARD SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA97IA038Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT AFT FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA97IA037Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT FORWARD SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA97IA036Buttstrap · corrodedIAH - DURING C-CHECK INSPECTION, THE CENTER BUTTSTRAP BETWEEN FRAMES 40 AND 44, WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA97IA035Buttstrap · corrodedIAH - DURING C-CHECK INSPECTION, THE BUTTSTRAP BETWEEN FRAMES 39 AND 44 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
Back to Embraer EMB-120RT