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 COMA9610171Overheat Switch · defectiveRT BLEED AIR DUCT OVERHEAT WARNING CAME ON DURING FLIGHT. REPLACED DEFECTIVE DUCT OVERHEAT SWITCH.SDR COMA9610170Compressor · damagedLEFT ENGINE HAS FOD DAMAGE ON COMPRESSOR BLADES. REPLACED ENGINE.SDR COMA9610172Solenoid · shortedFLIGHT IDLE STOP SOLENOID CIRCUIT BREAKER TRIPPED, WOULD NOT RESET. REPLACED THE FLIGHT IDLE SOLENOID.SDR COMA9610169Eccentric Shaft · shearedDURING C-1 INSPECTION, FOUND RUDDER ECCENTRIC SHAFT TO BE SHEARED JUST ABOVE SPLINED SHAFT. INSTALLED SERVICEABLE (P/N 120-48563-001) AND RETURNED AIRCRAFT TO SERVICE. ECCENTRIC SHAFT AND FAIL-SAFE PIN SENT TO EMBRAER FOR ANALYSIS.SDR C2XA96IA141Prop Actuator · seizedIAH - FLT 3830 - DURING TAKEOFF ROLL, THE NR 2 ENGINE PRODUCED ONLY 22 PERCENT TORQUE. AIRCRAFT RETURNED, MX FOUND THE RIGHT PROPELLER ACTUATOR PITCH CHANGE MECHANISM SEIZED. THE RIGHT PROPELLER ACTUATOR WAS REMOVED AND REPLACED GROUND OPERATIONAL, LEAK CHECKSDR C2XA96IA143Wow Control · failedIAH - FLT 3866 - AFTER TAKEOFF AND GEAR RETRACTION HAD CONTINOUS AURAL WARNING, BRAKES, TRIM, FLAPS, AUTOFEATHER. AIRCRAFT EXECUTED AIR RETURN TO IAH. MX REMOVED, CLEANED AND RESECURED WOW CANNON PLUGS. AURAL WARNINGS OPS CHECKED GOOD. AIRCRAFT AIR RETURNEDSDR COMA9610168Circuit Breaker · trippedRIGHT POWER LEVER FLIGHT IDLE STOP SOLENOID CIRCUIT BREAKER TRIPPED. RESET BREAKER - SYSTEM TEST NORMAL.SDR COMA9610167Air Speed Ind · failedCOPILOT'S AIR SPEED INDICATOR FAILED DURING TAKEOFF. REPLACED THE AIR SPEED INDICATOR. PART TOTAL CYCLES, 7,765.SDR GLBA96114Filters · cloggedRDU - FUEL FILTER LIGHT ILLUMINATED ON POWER UP FOR DEPARTURE. REMOVED ADN REPLACED FUEL PUMP OUTLET FILTER AND FUEL HEATER FILTER. AIRCRAFT RETURNED TO SERVICE. REFERENCE: OPERATOR CONTROL NR 96ZZZX3648. (X)SDR GLBA96113Flap Actuator · failedRDU - FLAP DISAGREEMENT, OUTBOARD FLAPS HANG AT ABOUT 10 DEGREES WHEN SELECTED FROM 15 DEGREES TO ZERO DEGREES. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR, OPS CHECKS GOOD. (X)SDR COMA9610166Sensor · defectiveWHEN LANDING GEAR SELECTED DOWN, GEAR DID NOT EXTEND. INDICATION WAS 5 RED INTRANSIT AND ONE GREEN DOWNLOCK. EMERGENCY SYSTEM USED TO EXTEND GEAR. REPLACED DEFECTIVE DOWNLOCK PROXIMITY SENSOR ON LEFT MLG.SDR COMA9610163Sensor · defectiveTAKEOFF TRIM AURAL WARNING SOUNDED DURING TAKEOFF. TRIM WAS CONFIRMED TO BE PROPERLY SET. REPLACED DEFECTIVE ELEVATOR TRIM PROXIMITY SENSOR.SDR COMA9610162Skin · corrodedDURING AN E9 INSPECTION, FOUND CORROSION ON FUSELAGE LOWER SKIN AT FRAME 21 (FS 6842.6). AT 7 O'CLOCK POSITION, AIRCRAFT HAD A PREVIOUS REPAIR ON FRAME 21 FOR CORROSION AT THE 6 O'CLOCK POSITION. REMOVED PREVIOUS REPAIR DOUBLER, CUT OUT NEW DAMAGED AREA OF FSDR C2XA96IA140T-Cap · corrodedIAH - DURING C-CHECK INSPECTION, FOUND FRAME 38 LEFT AND RIGHT OUTBOARD T-CAPS TO HAVE CORROSION BEYOND LIMITS. MX REMOVED AND REPLACED LEFT AND RIGHT OUTBOARD T-CAPS FRAME 38. (M)SDR C2XA96IA139T-Cap · corrodedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT INBOARD T-CAP FRAME 38 TO HAVE CORROSION BEYOND LIMITS. MX REMOVED AND REPLACED RT INBOARD T-CAP FRAME 38. (M)SDR C2XA96IA138Buttstrap · corrodedIAH - DURING C-CHECK INSPECTION, FOUND FUSELAGE CENTER BUTTSTRAP FRAME 39 TO FRAME 44 TO HAVE CORROSION BEYOND LIMITS. MX REMOVED AND REPLACED CENTER BUTTSTRAP FROM FRAME 37 TO FRAME 44. (M)SDR C2XA96IA137Buttstrap · corrodedIAH - DURING C-CHECK INSPECTION, FOUND FRAME 37 TO FRAME 41.5 RIGHT INBOARD BUTTSTRAP TO HAVE CORROSION BEYOND LIMITS. MX REMOVED AND REPLACED RT INBOARD BUTTSTRAP FRAME 37 TO FRAME 41.5. (M)SDR C2XA96IA136T-Cap · corrodedIAH - DURING C-CHECK INSPECTION, FOUND FRAME 36 LEFT OUTBOARD T-CAP TO HAVE CORROSION BEYOND LIMITS. MX REMOVED AND REPLACED FRAME 36 LEFT OUTBOARD T-CAP. (M)SDR C2XA96IA135Channel · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT MAIN LANDING INBOARD LOWER NACELLE CHANNEL DEFORMED AND CRACKED BETWEEN NACELLE FRAME 14 AND FRAME 15. MAINTENANCE REMOVED AND REPLACED NACELLE CHANNEL. (M)SDR C2XA961A134Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, FOUND PASSENGER LEFT AND RIGHT SEAT TRACKS TO HAVE CORROSION BEYOND LIMITS. MX REMOVED AND REPLACED SEAT TRACKS, FRAME 29 TO FRAME 39. (M)SDR 96ZZZX3648Filters · cloggedRDU - FUEL FILTER LIGHT ILLUMINATED ON POWER UP FOR DEPARTURE. REMOVED AND REPLACED FUEL PUMP OUTLET FILTER AND FUEL HEATER FILTER. AIRCRAFT RETURNED TO SERVICE. REFERENCE: OPERATOR CONTROL NR GLBA96114.SDR COMA9610165Spinner · loose rivetsLEFT PROPELLER SPINNER HAS LOOSE RIVETS. REPLACED SPINNER.SDR COMA9610164Angle · crackedLEFT WING ROOT FAIRING ATTACH ANGLE IS CRACKED. REPLACED FAIRING ATTACH ANGLE.SDR WTAA960116Selector · malfunctionedFAT - LT MLG AND NLG GEAR B-LIGHT ILLUMINATES INTERMITTENTLY IN-FLIGHT. MAINTENANCE DEFERRED B-INDICATION SYSTEM PER MEL 32-60-1. AIRCRAFT RETURNED TO SERVICE. SUBSEQUENTLY, CLEARED DEFERRAL BY REPLACMENT OF GEAR HANDLE ASSEMBLY. (X)SDR GLBA96106Uplock Sensor · failedLAN - CREW REPORTED GEAR INTRANSIT LIGHTS REMAINED ILLUMINATED AND GEAR DOORS DID NOT RETRACT. THEY MADE AN AIR TURNBACK AND LANDED UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED RT MLG UPLOCK SENSOR AND ADJUSTED ALL UPLOCK TARGETS. OPS CHECK WAS GOOD. (X)SDR COMA9610161Fitting · crackedLT NACELLE FLAP HINGE ATTACH FITTING FOUND CRACKED DURING INSPECTION. REPLACED CRACKED FITTING.SDR COMA9610159Actuator · out of adjustWHEN LANDING GEAR SELECTED UP, THE LT MLG REMAINED DOWN FOR 5 MINUTES BEFORE RETRACTING. ADJUSTED RETRACT ACTUATOR TO M/M SPECIFICATIONS AND ACFT RETURNED TO SERVICE.SDR COMA9610158Propeller · leakingLEFT ENGINE LEAKED A LARGE AMOUNT OF OIL DURING TAXI FROM HANGAR TO GATE. REPLACED THE LT PROPELLER ASSY.SDR C2XA961A132Rim · crackedIAH - DURING PILOT PRE-FLIGHT, FOUND THE NR 2 MAIN WHEEL ASSEMBLY OUTER HALF WHEEL RIM CRACKED AND SEPARATING. MX REMOVED AND REPLACED WHEEL ASSY. (M)SDR COMA9610160Hydraulic Pump · failedGREEN HYDRAULIC SYSTEM ELECTRIC PUMP, FAILED. REPLACED THE GREEN SYSTEM ELECTRIC HYDRAULIC PUMP.SDR C2XA961A133Fuse · failedIAH - DURING 1A, 3A INSPECTION, BOTH LEFT AND RIGHT LOWER EXTERIOR EMERGENCY EXIT LIGHTS FOUND TO BE INOPERATIVE. MX REMOVED AND REPLACED THE AFT EMERGENCY EXIT LIGHT POWER SUPPLY FUSE. (M)SDR WTAA960114Fuel Heater · failedRDD - RIGHT ENGINE OIL LIGHT ILLUMINATED IN FLIGHT. CREW SECURED NR 2 ENGINE AND DECLARED AN EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT. MX SUSPECTS POSSIBLE INTERNAL LEAKAGE IN FUEL/OIL HEATER. MX REPLACED FUEL/OIL HEATER. OIL QUANTITY AND PRESSURES NORSDR WTAA960113Battery Pack · dischargedFAT - FLOOR PROXIMITY EMERGENCY LIGHT PATH MARKING SYSTEM INOPERATIVE. DEFERRED BATTERY PACK PER MEL 33-30-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL BY REPLACING AFT EMERGENCY BATTERY PACK. SYSTEM OPERATIONAL CHECK NORMAL. SDR GLBA96105Actuator · failedMYR - CREW REPORTED A FLAP DISAGREEMENT FAULT AFTER TAKEOFF. THEY MADE AN AIR TURN-BACK AND LANDED UNEVENTFULLY. MAINTENANCE REPLACED LEFT OUTBOARD FLAP ACTUATOR. OPS CHECK WAS GOOD. (X)SDR ASOA96018Seal · defectiveIN FLT ATL-CRW - WHILE DESCENDING FROM 25,000 TO 24,00 FEET, CABIN RAPIDLY DEPRESSURIZED FOLLOWING A THUMP HEARD BY ALL 3 CREW MEMBERS. CAPTAIN DECLARED AN EMERGENCY, DESCENDED TO 10,000 FEET AND DIVERTED INTO TRI WHERE LANDING WAS MADE SAFELY AND WITHOUT INCSDR WTAA960111Bulb · failedLAX - NOSE LANDING GEAR DOWN AND LOCK 'GREEN' INDICATION DID NOT ILLUMINATE. MX REPLACED 4 BULBS. INDICATION NORMAL DURING GROUND CHECK. AIRCRAFT RETURNED TO SERVICE. (M)SDR COMA9610157Check Valve · leakingFUEL LEAKING FROM RT ENGINE NACELLE. REPLACED THE EPA TANK CHECK VALVE.SDR COMA9610154Latch · brokenRIGHT MLG OUTBOARD GEAR DOOR WILL NOT CLOSE. REPLACED BROKEN DOOR LATCH ASSY.SDR COMA9610156Warning Syst · activatedFLAP CONTROL FAULT WARNING WHEN SELECTED TO 25 DEGREES. RESET FLAP SYSTEM - NO FAULT CODES FOUND IN MEMORY. ACFT RETURNED TO SERVICE.SDR COMA9610155Tcas · malfunctionPILOT'S RED HEADING FLAG LIGHT ON ALONG WITH FAILURE OF TCAS. REPLACED THE AHC-85. PART TOTAL CYCLES, 13,044.SDR COMA9610153Skin · corrodedSEVERE CORROSION WAS FOUND DURING INSPECTION ON THE LOWER FUSELAGE SKIN AT FRAME 22 BETWEEN STRINGERS 21R AND 20R. THE CORROSION IS WHERE THE SKIN CONTACTS THE TITANIUM REINFORCING STRAP P/N 120-22409-001. THE DAMAGED AREA WAS REMOVED AND A REPAIR INSTALLED SDR ASOA96017Oil Cap · wornFLT 7925 - ON CLIMB-OUT GOT AURAL WARNING (3 BELLS), ENGINE OIL. OIL PRESSURE WAS FLUCTUATING BETWEEN 55 AND 30 PSID. SHUT ENGINE NR 2 DOWN. AN EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO DFW. THE AIRCRAFT WAS LANDED WITHOUT INCIDENT. CLEANED AND INSPESDR ASOA96016P3 Line · brokenLEVELING OFF AT 2000 FEET DEPARTING DFW, LEFT ENGINE SURGED SLIGHTLY AND SHUTDOWN COMPLETELY WITH AUTOFEATHER. NO LIMITATIONS WERE EXCEEDED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW WHERE A LANDING WAS MADE WITHOUT INCIDENT. UPON INSPECTIOSDR WTAA960108Selector · malfunctionedFAT - LANDING GEAR FAILED TO RETRACT ON INITIAL ATTEMPT. GEAR RETRACTION NORMAL ON THIRD ATTEMPT. MAINTENANCE UNABLE TO DUPLICATE DISCREPANCY ON GROUND. SUSPECT FAULTY LANDING GEAR SELECTOR. REPLACED SELECTOR. SYSTEM OPEATIONAL CHECK NORMAL DURING GEAR RESDR WTAA960106Brakes · malfunctionedSMF - NORMAL BRAKES FAILED DURING LANDING ROLL AND TAXI. MAINTENANCE CHECKED ANTI-SKID BRAKE TRANSDUCERS. NO DEFECTS NOTED. UNABLE TO DUPLICATE DISCREPANCY. BRAKE SYSTEMS CHECK NORMAL ON LOW SPEED AND HIGH SPEED TAXI BRAKE TESTS. AIRCRAFT RETURNED TO SERVSDR WTAA960104Connector · looseSMF - RIGHT ENGINE FILTER LIGHT ILLUMINATED ON TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. DEFERRED INDICATOR PER MEL 73-33-1. AIRCRAFT RETURNED TO SERVICE. MX SUBSEQUENTLY CLEARED DEFERRAL WITH CLEANING OF RIGHT ENGINE LOW PRESSURE FILTER CANNON PLUG ASDR COMA9610150Radar · malfunctionedRADAR DISPLAY IS ERRATIC AND ERRONEOUS. PLACED WEATHER RADAR SYSTEM ON DEFERRED MAINTENANCE LIST. ACFT RETURNED TO SERVICE.SDR COMA9610151Skin Support · crackedDURING 400FC INSPECTION, FOUND ONE RIVET AT FRAME 9 JUST BELOW RIGHT DIRECT WINDOW TO BE DEFORMED. FURTHER INSPECTION REVEALED SKIN SUPPORT TO BE CRACKED. REPLACED CRACKED SUPPORT.SDR COMA9610149Window · air leakCABIN WILL NOT HOLD PRESSURIZATION. ADJUSTED AND RESEALED PILOT'S DIRECT VISION WINDOW.SDR WTAA960103Prox Sensor · failedFAT - RIGHT MAIN LANDING GEAR 'B' SYSTEM INTRANSIT LIGHT REMAINS ILLUMINATED WITH GEAR DOWN. MX DEFERRED 'B' INDICATION SYSTEM PER MEL 32-60-1. AIRCRAFT RETURNED TO SERVICE. MX SUBSEQUENTLY CLEARED DEFERRAL BY REPLACING THE RIGHT MAIN LANDING GEAR 'B' DOWNL
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