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 C2XA99CL014Control · failedCMH - FLT 3350 - CREW REPORTED THAT THE LEFT INBOARD FLAP HAD A UNCONTROLLED EXTENSION TO ASYMMETRY 25 DEGREES. AIRCRAFT DIVERTED TO CMH WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAP CONTROL UNIT IAW EMB-120MM 27-50-06, OPERATIONAL CHECSDR ASOA99024Angle · brokenDURING C-CHECK INSPECTION, THE FRAME 2 ANGLE ON LEFT ENGINE NACELLE WERE FOUND BROKEN. REMOVED AND REPLACED FRAME ANGLE ON LEFT ENGINE NACELLE. (M)SDR ASOA99023Frame · crackedDURING C-CHECK INSPECTION, NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES WERE FOUND TO HAVE CRACKS. REMOVED AND REPLACED NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES. (M)SDR SWIA971406Tscu · malfunctionedDURING CLIMB, RIGHT ENGINE WENT INTO AUTOFEATHER AT 1000 FT AGL WITH TORQUE ABOUT 144 PERCENT. RETURNED TO LAX. REPLACED RIGHT ENGINE TORQUE PROBE AND RIGHT ENGINE TSCU. MM INSPECTION STEPS WERE PERFORMED FOR OVER TORQUE OF PROPELLER AND ENGINE ON RIGHT SIDSDR SWIA971396Deice Syst · malfunctionedLEADING EDGE MIDDLE LEFT WING DEICE BOOT FAILS BOTH TIMERS. RETURNED TO SFO. SWAPPED LEFT AND RIGHT MIDDLE DEICE BOOT PRESSURE SWITCHES FOR TROUBLESHOOTING. COULD NOT DUPLICATE PROBLEM. LEADING EDGE DEICE SYSTEM, CHECKS GOOD.SDR SWIA971393B Nut · looseLEADING EDGE MIDDLE LEFT WING DEICE BOOT FAILS BOTH TIMERS. RETURNED TO FIELD. TIGHTENED LOOSE B-NUT AT LEFT MIDDLE LEADING EDGE DEICE BOOT PRESSURE SWITCH, OPS CHECKS GOOD.SDR COMA9960062Beam · corrodedDURING AN E5 PART A INSPECTION, CORROSION DAMAGE WAS FOUND ON THE UPPER SURFACE OF THE CENTER OMEGA BEAM AT FRAME 16. THE DAMAGE CONSISTS OF 1 HOLE AND 4 AREAS OF PITTING. THE HOLE WAS CLEANED UP, DEBURNED AND SHARP EDGES REMOVED. THE 4 AREAS OF PITTING WASSDR COMA9910033Sign · inoperativeROW EIGHT EXIT SIGN INOPERABLE. REPALCED EXIT SIGN.SDR SWIA971427Boot · failedLEFT ENGINE INLET DEICE BOOT FAILED IN FLIGHT, OUTSIDE AIR TEMP -50. RETURNED TO PDX. INSPECTED ENTIRE DEICE SYSTEM, TIGHTEN UP NUMEROUS LINES AND REPLACED BOTH WATER SEPARATORS. INFLATED ALL BOOTS WITH SHOP AIR AND INSPECTED. OPS CHECK DEICE SYSTEM, CHECKSDR SWIA971426Actuator · failedLEFT MAIN LANDING GEAR WOULD NOT RETRACT. RETURNED TO SMF. REMOVED AND REPLACED LEFT MAIN LANDING GEAR ACTUATOR IAW EMB 120 MM 32-32-10. OPS CHECK GOOD.SDR C2XA99CL012Seal · failedALB - FLT 3172 - CREW REPORTED THEY HAD A RAPID DEPRESSURIZATION FROM FL 250 WITH A TOTAL LOSS OF ALL PRESSURIZATION. AIRCRAFT DIVERTED SCHEDULED ROUTE AND LANDED IN ABL WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS MAINTENANCE FERRIED TO CLE AND THE CARGO DOORSDR C2XA99IA127Bulb · failedIAH - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE RIGHT FORWARD OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR SWIA971410Controller · malfunctionedCRUISE FLIGHT, FL210 WITH CABIN PRESSURE SET IN AUTO. CABIN RATE INDICATOR NEEDLE PEGGED ITSELF OFF THE SCALE IN A CLIMB UNTIL CABIN PRESSURE WAS 10,000 FT. AFTER SEVERAL CLIMBS/ DESCENT OSCILLATIONS AND EMERGENCY DESCENT INDICATED PROBLEM CORRECTED IN CONTRSDR SWIA971408Relay · malfunctionedGEAR DOORS STAY OPEN AFTER GEAR IS RETRACTED. RETURNED TO FAT. REPLACED RELAY BOX AND CANNON PLUG AT P1112. GROUND RUN NORMAL. ALSO, GEAR EXTENSION/RETRACTION NORMAL. REPLACED CONNECTOR AT P1112, OPS NORMAL.SDR COMA9910031Lens · missingEMERGENCY EXIT LIGHT COVER IS MISSING AT ROW 5. REPLACED LIGHT COVER.SDR SWIA971407Valve · out of adjustWHEN GEAR HANDLE WAS RETRACTED ALL 12 LIGHTS (RED AND GREEN) ILLUMINATED, EXCEPT RED LEFT A CIRCUIT LIGHT. GEAR WOULD NOT RETRACT, COULD NOT DUPLICATE PROBLEM ON GROUND. ADJUSTED RIGHT MAIN GEAR DOOR SEQUENCE VALVES. REMOVED AND REPLACED GEAR SELECTOR FOR TSDR COMA9910030Battery · dischargedAFT SECTION OF EMERGENCY FLOOR LIGHTING IS INOPERABLE. REPLACED EMERGENCY BATTERY.SDR COMA9910029Warning · malfunctionedFLAP CONTROL FAULT WARNING DURING TAKEOFF. COULD NOT DUPLICATE, OPERATIONAL CHECK OF FLAP SYSTEM WAS NORMAL.SDR COMA9910026Frame · crackedLEFT NACELLE, FRAME WEB NR 10 CRACKED AT INBOARD RADIUS OF THE FLANGE. REPAIRED BY SPLICING IN A NEW FLANGE PER AERODESIGN REPORT NR 1076-2 AND EMB120 SRM 51-40-02.SDR ASOA99017Switch · stuckFLT 9258 - DURING TEST FLIGHT OUT OF CKB, CREW NOTICED BOTH PARKING BRAKE LIGHTS CAME ON WITH ASSOCIATED GEAR PROBLEM (LANDING GEAR SYSTEM 'B', ALL 3 RED 'B' LIGHTS CAME ON UPON RETRACTION). CREW DECLARED AN EMERGENCY AND RETURNED TO CKB WHERE LANDING WAS MADSDR ASOA99020Angle · brokenDURING C-CHECK INSPECTION, THE FRAME 2 ANGEL ON LEFT AND RIGHT ENGINE NACELLES WERE FOUND BROKEN. REMOVED AND REPLACED FRAME ANGLES ON LEFT AND RIGHT NACELLES. (M)SDR ASOA99019Frame · crackedDURNG C-CHECK INSPECTION, NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES WERE FOUND TO HAVE CRACKS. REMOVED AND REPLACED NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES. (M)SDR COMA9910027Retract Mech · dirtyFLAP DISAGREEMENT WARNING ATER TAKEOFF. CLEANED DIRT FROM FLAP TRUCKS.SDR COMA9910028Sign · brokenEMERGENCY EXIT SIGN AT ROW 5 IS BROKEN. REPLACED SIGN ASSY.SDR COMA9910025Battery Pack · dischargedFORWARD SECTION OF CABIN EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED BATTERY PACK FOR THE FORWARD EMERGENCY LIGHTING.SDR COMA9910024Connector · looseDURING CLIMBOUT FROM MCO WITH GEAR SELECTED UP, RT GEAR RED LIGHT ILLUMINATED. AIRCRAFT RETURNED TO THE FIELD. REINSTALLED RT GEAR A AND B PROXIMITY SENSOR CONNECTOR.SDR COMA9910020Bushing · out of positionWHILE PERFORMING LANDING GEAR FREE-FALL CHECK, THE LEFT MAIN LANDING GEAR WOULD NOT GO TO THE LOCKED POSITION WITHOUT EXCEEDING THE MAX PULL LIMITS. FURTHER INVESTIGATION REVEALED THE OUTBOARD BUSHING FOR THE MAIN DRAG AND LOCKING STRUT HINGE PIN TO HAVE MIGRSDR COMA9910023Actuator · failedWHEN SELECTING FLAPS TO 45 DEGREES, THE FLAP DISAGREE CAUTION ACTIVATED. REPLACED THE EIGHT OUTBOARD FLAP ACTUATOR.SDR COMA9910022Door · not securedDOOR LIGHT ILLUMINATED DURING TAKEOFF ROLL, AIRCRAFT RETURNED TO THE GATE. SECURED FUEL SERVICE DOOR FASTENER.SDR COMA9910021Sign · brokenEMERGENCY EXIT SIGN AT 5A IS BROKEN. REPLACED EXIT SIGN AT 5A.SDR C2XA99CL010Sensor · failedGSO - FLT 3346 - CREW REPORTED THAT IN-FLIGHT, THEY RECEIVED A LEFT DUCT LEAK AURAL WARNING, AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED A DUCT TEMP SENSOR IAW EMB-120 MM 20-21-00, OPERATIONAL CHECKS WERE SATISFACTORYSDR ASOA99014SEngine · failedFLT 4825 - EN ROUTE DFW-AMA, A LOUD BANG WAS HEARD FOLLOWED BY AIRCRAFT VIBRATION, SMOKE IN CABIN AND COCKPIT, AND REDUCED POWER IN LEFT ENGINE (20 PERCENT TORQUE). CREW FOLLOWED THE ENGINE FAILURE CHECKLIST, DECLARED AN EMERGENCY AND DIVERTED TO SPS WHERE SISDR COMA9910019Warning · activatedDURING TAKEOFF ROLL, AUTOFEAHTER AURAL WARNING ACTIVATED. INSPECTED LT AND RT ENGINE SCU FOR CONDITION AND SECURITY. PERFORMED OPERATIONAL CHECK OF THE AUTOFEATHER SYSTEM, NO DEFECTS NOTED.SDR COMA9910017Actuator · leakingLT MLG DISAGREEMENT INDICATION WHEN LANDING GEAR RETRACTED. REPLACED THE LT MLG RETRACT ACTUATOR.SDR COMA9910016Battery · dischargedEMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY LIGHTS BATTERY.SDR COMA9910018Guide · corrodedDURING ROUTINE MAINTENANCE, THE UPPER CABLE GUIDE FITTING ON THE CARGO DOOR WAS FOUND TO HAVE SEVERE EXFOLIATION CORROSION. CORROSION WAS APPROX .1875 IN DEPTH OVER AN AREA OF 1X .50. THE FITTING WAS REPLACED WITH A SERVICEABLE FITTING AS PER EMB MAINTENANCESDR ASOA99013Seal · detachedFLT 4067 - EN ROUTE ATL-CRW, LOST PRESSURIZATION AT 25,000 FEET AND PERFORMED AN EMERGENCY DESCENT TO 10,000 FEET. OXYGEN MASKS WERE DEPLOYED IN THE CABIN. LANDING WAS MADE SAFELY AT CRW WITHOUT FURTHER INCIDENT. LOCAL MTC FOUND CARGO DOOR SEAL DETACHED FROSDR ASOA99012Angle · brokenDURING C-CHECK INSPECTION, THE FRAME 2 ANGLE ON LEFT AND RIGHT ENGINE NACELLES WERE FOUND BROKEN. REMOVED AND REPLACED FRAME ANGLES ON LEFT AND RIGHT ENGINE NACELLES. (M)SDR ASOA99011Support Bracket · separatedDURING C-CHECK INSPECTION, FS X14280 AND FS X14616 FUSELAGE FRAMES ATTACHED TO CARGO DOOR OPENING UPPER FRAME SUPPORT BRACKETS FOUND TO BE SEPARATED AT BOTH FRAME STATIONS. REMOVED AND REPLACES UPPORT BRACKETS. (M)SDR ASOA99010Frame · crackedDURING C-CHECK INSPECTION, NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES WERE FOUND TO HAVE CRACKS. REMOVED AND REPLACED NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES. (M)SDR 99ZZZX863Bracket · brokenFS X14280.0 AND FS X14615.0 FUSELAGE FRAMES ATTACH TO CARGO DOOR OPENING UPPER FRAME WITH SUPPORT BRACKETS P/N 120-19522-D01. BRACKETS UPSTANDING FLANGES SEPARATED COMPLETELY AT BOTH FRAME STATIONS. POSSIBLE CAUSE IS FRETTING CORROSION. CARGO BAY LINER AND ISDR 99ZZZX862Angle · brokenDURING C-CHECK INSPECTION, THE FRAME 2 ANGLE WAS FOUND BROKEN ON BOTH LEFT AND RIGHT NACELLES. REPLACED THE ANGLE AND WILL CONTINUE MONITORING IAW EXISTING C-CHECK INSPECTIONS.SDR 99ZZZX861Frame · crackedDURING ROUTINE MAINTENANCE CHECKS, A CRACK WAS FOUND ON BOTH ENGINE NACELLES' FRAME 1. THE CRACK IS LOCATED ON THE LOWER SIDE OF THE STIFFENING WEB BETWEEN THE TOP OUTBOARD MOUNTING BOLT HOLE AND THE OUTBOARD EDGE OF THE FRAME. RECOMMEND REPLACING BOTH FRAMESDR COMA9910015Valve · malfunctionedAIR CONDITIONING SYSTEM EMITS SMOKE. COULD NOT DUPLICATE DISCREPANCY. REPLACED THE RIGHT HAND ENGINE P2.5/3 SWITCHING VALVE FOR TROUBLESHOOTING.SDR C2XA99IA065Fuse · failedIAH - DURNG PREFLIGHT INSPECTION, THE AFT EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FUSE FOR THE AFFECTED LIGHTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA99IA064Wire · brokenIAH - DURING PREFLIGHT INSPECTION, TWO AISLE PATH EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED THE AFFECTED WIRES AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA99IA063Wire · brokenIAH - DURING PREFLIGHT INSPECTION, TWO AISLE PATH EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED THE AFFECTED WIRES AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR ASOA99009Fan · failedON TAXI OUT, CREW ADVISED THAT THE RIGHT PACK FAILED AND REPORTED SMOKE IN THE CABIN. AIRCRAFT RETURNED TO THE GATE AND DEBOARDED. ATL, MAINTENANCE REMOVED AND REPLACED THE RIGHT PACK GROUND COOLING FAN. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASDR ASOA99008Wire · chafedMAINTENANCE WAS ADVISED THAT THE FLIGHT ATTENDANT EMERGENCY LIGHTS TESTS SWITCH POPS THE EMERGENCY LIGHTS C/B. ATL, MAINTENANCE FOUND A CHAFED WIRE AT CANNON PLUG P0389 (AT NR 2 BATTERY PACK) AND REPAIRED WIRE AS NEEDED. OPERATIONAL CHECKS WERE GOOD AND THE AISDR COMA9910014Lamp · failedEMERGENCY FLOOR LIGHT AT CABIN DOOR IS INOPERABLE. REPALCED LIGHT BULB.
Back to Embraer EMB-120RT