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 COMA9710156Actuator · malfunctionFLAP CONTROL FAULT WARNING AFTER TAKE OFF. REPLACED THE LEFT NACELLE FLAP ACTUATOR.SDR C2XA97CL017Wave Guide · wornCLE - FLT 3009 - CREW REPORTED THAT THE RADAR WAS INOPERATIVE, THEY RECEIVED A FAULT ON THE DISPLAY. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE RADAR WAVE GUIDE. OPERATIONAL CHECKS WERE GOOD IAW EMB 120 ER MSDR C2XA97IA067Skin · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT WING LOWER SKIN AT THE INBOARD NACELLE JUNCTION, WAS FOUND TO BE CRACKED. THE WING SKIN WAS REPAIRED BY REMAINING THE FASTENER HOLE AND INSERTING A BUSHING. ALL WORK WAS ACCOMPLISHED IAW CONTINENTAL EXPRESS ENGINEERISDR C2XA97IA066Stringer · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT WING STRINGER NR 10 WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE AFFECTED PORTION OF STRINGER USING A SPLICE REPAIR. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M)SDR COMA9710155Control · malfunctionedNLG GREEN LIGHTS ARE INTERMITTENT. COULD NOT DUPLICATE DISCREPANCY. REPLACED THE LANDING GEAR CONTROL FOR TROUBLESHOOTING.SDR COMA9710153Wire · looseCENTER SECTION OF CABIN EMERGENCY LIGHTING IS INOPERATIVE. TIGHTENED LOOSE CONNECTION AT EMERGENCY BATTERY.SDR COMA9710154Water Separator · brokenRIGHT HAND BLEED AIR DUCT LEAK WARNING DURING FLIGHT. REPLACED DEFECTIVE BLEED AIR WATER SEPARATOR.SDR WTAA970029Airspeed Ind · failedLAX - HIGH SPEED WARNING ON TAKEOFF. TAKEOFF ABORTED. MAINTENANCE REPLACED CAPTAINS AIRSPEED INDICATOR. OPERATIONAL AND LEAK CHECKS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M)SDR COMA9710151Relay · inoperativeRIGHT HAND PROPELLER AUTO FEATHER SYSTEM DOES NOT TEST. REPLACED RELAY K0039, SYSTEM TEST NORMAL.SDR COMA970150Roller · dirtyFLAP DISAGREE WARNING AFTER TAKEOFF. REPLACED THE FLAP ROLLERS.SDR COMA9710152Switch · malfunctionFLAP DISAGREE WARNING AFTER TAKEOFF. REPLACED THE FLAP SELECTOR HANDLE.SDR WTAA970028Tire Wheel Assy · failedSFO - RIGHT INBOARD TIRE BLOWN ON TAKEOFF REPORTED. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE REPLACED BOTH RIGHT MAIN TIRES AND WHEEL ASSEMBLIES, P/N 314461. AIRCRAFT RETURNED TO SERVICE. (M)SDR GLBA97026Connector · dirtyORD - FLAP DISAGREEMENT AFTER TAKEOFF. MAINTENANCE RESET FLAP ACTUATING SYSTEM, CLEANED CANNON PLUGS AND FLAP TRACKS OF CONTAMINATION. (M)SDR AU970116Filter · cracked(AUS) LH ENGINE DE-ICE SYSTEM AIR LINE WATER FILTER HOUSING CRACKEDSDR COMA9710149Skin · corrodedON 2C INSPECTION, THE LOWER FUSELAGE SKIN WAS FOUND CORRODED UNDER THE TITANIUM STRAP AT FRAME 21, BETWEEN STRINGERS 19L AND 20L. THE SKIN WAS REPAIRED PER SRM 53-00-01, FIGURE 202.SDR COMA9710148Skin · corrodedON 2C INSPECTION, THE LOWER FUSELAGE SKIN WAS FOUND CORRODED UNDER TITANIUM STRAP AT FRAME 23, BETWEEN STRINGERS 20R AND 21R. THE SKIN WAS REPAIRED PER AERODESIGN REPORT NR 1896-1, REV A, DATED 2-7-97.SDR COMA9710147Sill · corrodedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT SILL WAS FOUND CORRODED. REPLACED WITH A NEW PART PER SRM 51 STANDARD PRACTICES.SDR COMA9710146Crossbeam · corrodedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT CROSSBEAM WAS FOUND CORRODED. REPLACED WITH A NEW PART PER SRM 51 STANDARD PRACTICES.SDR COMA9710145Butt Strap · corrodedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE LT BUTT-STRAP WAS FOUND CORRODED. REPLACED WITH A NEW PART PER SRM 51 STANDARD PRACTICES.SDR COMA9710144Butt Strap · corrodedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT BUTT-STRAP WAS FOUND CORRODED. REPLACED WITH A NEW PART PER SRM 51 STANDARD PRACTICES.SDR COMA9710143Butt Strap · corrodedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT BUTT STRAP WAS FOUND CORRODED. REPLACED WITH A NEW PART PER SRM 51 STANDARD PRACTICES.SDR COMA9710142Omega Beam · corrodedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE LT OMEGA BEAM WAS FOUND CORRODED. REPLACED WITH A NEW PART PER SRM 51 STANDARD PRACTICES.SDR COMA9710141Supporting Sect · corrodedON 2C INSPECTION, THE FWD SECTION RT SIDEWALL SEAT TRACK SUPPORTING SECTION WAS FOUND CORRODED. REPLACED WITH A NEW PART PER SRM CHAPT 51 STANDARD PRACTICES.SDR COMA9710140Supporting Sect · corrodedON 2C INSPECTION, THE AFT SECTION RT SIDEWALL SEAT TRACK SUPPORTING SECTION WAS FOUND CORRODED. REPLACED WITH A NEW PART PER SRM CHAPT 51 STANDARD PRACTICES.SDR COMA9710139Butt Strap · corrodedON 2C INSPECTION, THE FUSLEAGE FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP WAS FOUND CORRODED. REPLACED WITH A NEW PART PER SRM 51 STANDARD PRACTICES AND AERODESIGN REPORT NR 1671-1, REV IR, DATED 10-22-95.SDR COMA9710138Angle · corrodedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE Z-ANGLE WAS FOUND CORRODED. REPLACED WITH A NEW PART PER SRM 51 STANDARD PRACTICES.SDR COMA9710137Angle · corrodedON 2C INSPECTION, THE AFT RIGHT EMERGENCY EXIT LOWER GUIDE PIN RECEPTACLES ON FUSELAGE AND THE LOWER ANGLE THEY'RE ATTACHED TO WERE FOUND CORRODED. THE LOWER ANGLE AND BOTH RECEPTACLES WERE REPLACED PER SRM CHAPT 51 STANDARD PRACTICES.SDR COMA9710136Skin · corrodedON 2C INSPECTION, THE FUSELAGE PASSENGER DOOR SURROUND STRUCTURE INNER SKIN WAS FOUND CORRODED BETWEEN FRAMES 15 AND 15A, JUST ABOVE STRINGER 17L. AN EXTERNAL DOUBLER REPAIR WAS INSTALLED PER AERODESIGN REPORT NR 2118-2, REV IR, DATED 2-8-97.SDR COMA9710135Skin · gougedON 2C CHECK, THE CARGO DOOR OUTER SKIN WAS FOUND GOUGED ALONG THE TOP EDGE BY CONTACTING THE FUSELAGE FIXED STOPS DURING DOOR OPENING AND CLOSING. THE SKIN WAS REPAIRED PER SRM 52-30-01, PG 201 TO 203.SDR COMA9710133Annunciator · malfunctionFLAP CONTROL FAULT WARNING DURING TAXI. REPLACED THE FLAP ANNUNCIATOR PANEL. PART TOTAL CYCLES, 8,700.SDR COMA9710132Door · not latchedSERVICE DOOR WARNING DURING TAKEOFF. SECURED SINGLE POINT FUEL SERVICE DOOR. AIRCRAFT CONTINUED SERVICE.SDR COMA9710131Servo · bindingAILERONS BINDING AND NOISY WHEN MOVED LT OR RT. REPLACED THE AUTO PILOT SERVO. PART TOTAL CYCLES, 20,917.SDR COMA9710130Prox Sensor · failedNOSE WHEEL STEERING INOP DURING LANDING. REPLACED THE RT MLG WEIGHT ON WHEELS PROXIMITY SENSOR.SDR COMA9710129Wire · damagedWHEN FLAPS SELECTED TO 15 DEGREES, CONTROL FAULT WARNING ON. REPAIRED DAMAGED WIRING CONNECTION AT RT OUTBOARD FLAP ACTUATOR.SDR COMA9710128Pitchlock Screw · malfunctionedPROPELLER ASSEMBLY REMOVED FROM AIRCRAFT FOR ACTUATOR AND HUB MAJOR INSPECTION. UPON INITIAL RECEIVING INSPECTION THE FEATHER STOP TAB WAS FOUND DISPLACED .025 INCH. PITCHLOCK SCREW WAS REMOVED FROM ASSEMBLY AND RETURNED TO MANUFACTURER. PART TOTAL CYCLES, SDR C2XA97IA064Skin · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT WING LOWER SKIN WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE LOWER SKIN USING A DOUBLER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA97IA063Skin · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT WING LOWER SKIN WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE SKIN USING A DOUBLER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA97IA062Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA97IA061Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT FORWARD 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 C2XA97IA060Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT AFT FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA97IA059Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT FORWARD SIDEWALL SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA97IA058T-Profile · corrodedIAH - DURING C-CHECK INSEPCTION, THE RIGHT T-PROFILE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA97IA057T-Profile · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT CENTER T-PROFILE AT FRAME 36 AND 38, WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA97IA056T-Profile · corrodedIAH - DURING C-CHECK INSPECTION, THE T-PROFILER AT FRAME 38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR COMA9710134Roller · wornFLAP CONTROL FAULT WHEN FLAPS SELECTED TO 25 DEGREES. REPLACED FLAP ROLLERS ON ALL FLAP SECTIONS.SDR COMA9710124Actuator · malfunctionFLAP CONTROL FAULT WARNING DURING TAXI. REPLACED THE RT OUTBOARD FLAP ACTUATOR.SDR C2XA97CL016Prox Sensors · dirtyIAD - FLT 3492 - CREW REPORTED THAT AFTER DEPARTURE THE LANDING GEAR FAILED TO RETRACT. AIRCRAFT RETURNED TO FIELD. THE AIRCRAFT ACCOMPLISHED AN UNEVENTFUL FERRY FLIGHT FROM IAD TO CLE. MAINTENANCE INSPECTED THE LANDING GEAR AND CLEANED THE A/B SYSTEM PROXISDR WTAA970026Air Distr · odorACV - FUMES REPORTED IN COCKPIT AND CABIN. MAINTENANCE INSPECTED AIRCRAFT. NO LEAKS OR FUMES NOTED. DEFERRED APU BLEED SYSTEM PER MEL 49-52-1 AS PRECAUTION. TEST FLIGHT SATISFACTORY. MAINTENANCE SUBSEQUENTLY CLEARED PREVIOUS DEFERRAL WITH A DETAILED INSPESDR COMA9710125Wire · defective'TAKE OFF TRIM' AURAL WARNING. REPAIRED DEFECTIVE WIRING AT THE ELEVATOR TRIM PROXIMITY SENSORS.SDR GLBA97020De-Ice Lead · failedCIU - RIGHT PROP DE-ICE FAILED. AIR TURN BACK TO CIU WHERE MAINTENANCE REPLACED PROP DE-ICE LEAD. (M)
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