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 COMA9610275Engine · failedTHE RIGHT ENGINE HAS HIGH NH SPEED AND LOW TORQUE. REPLACED THE RIGHT ENGINE.SDR COMA9610273Indicator · failedTHE RT NP INDICATOR FAILED DURING TAKEOFF. REPLACED NP INDICATOR.SDR ASOA96036Cooling Fan · inoperativeDURING TAXI-OUT ATL-AVL, EXPERIENCED RIGHT PACK FAILURE CAUSING SMOKE IN THE CABIN. AIRCRAFT RETURNED TO THE GATE AND DEBOARDED WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED THE RIGHT GROUND COOLING FAN. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RESDR COMA9610274Bolt · brokenNO NP OR TORQUE INDICATION AFTER ENGINE START. PROPELLER WAS NOT ROTATING. AFTER ENGINE SHUT DOWN THE PROPELLER COULD NOT BE TURNED BY HAND. WHEN ENGINE DISASSEMBLED, A BROKEN INTERSTAGE CASE BOLT WAS FOUND TO BE JAMMING THE 1ST STAGE POWER TURBINE DISK. BSDR C2XA96CL029O-Rings · cutBUF - FLT 3000 - CREW REPORTED THAT DURING CRUISE, THE RIGHT HAND ENGINE LOST OIL PRESSURE, AIRCRAFT DIVERTED TO BUF. MAINTENANCE INSPECTED O-RINGS IAW EMB-120 MM 73-12-00. OPERATIONAL AND LEAK CHECKS WERE GOOD IAW EMB-120 MM 71-00-00. AIRCRAFT RETURNED TO SDR COMA9610272Battery · dischargedAFT SECTION OF CABIN EMERGENCY LIGHTING IS INOPERATIVE. REPLACED EMERGENCY LIGHTING BATTERY. PART TOTAL CYCLES, 13,088.SDR COMA9610271Battery · dischargedEMERGENCY FLOOR LIGHTING FORWARD OF ROW 4 IS INOPERATIVE. REPLACED EMERGENCY BATTERY. PART TOTAL CYCLES, 11,712.SDR C2XA96CL025Switch · out of adjustCLE - FLT 3070 - CREW REPORTED, THAT THE NOSE WHEEL STEERING DISCONNECTS WHEN MAKING FULL LEFT TURNS USING THE TILLER. MAINTENANCE INSPECTED AIRCRAFT AND ADJUSTED THE NOSE WHEEL STEERING TILLER MICROSWITCH IAW EMB-120 MM 32-50-00. OPS CHECKS WERE GOOD, AIRCRASDR COMA9610270Actuator · malfunctionFLAP CONTROL FAULT WARNING DURING FLIGHT WITH FLAPS AT ZERO. REPLACED THE LT OUTBD FLAP ACTUATOR.SDR GLBA96184Prox Switch · inoperativeMQT - LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. MAINTENANCE REMOVED AND REPLACED RIGHT MAIN PROXIMITY SWITCH. OPS NORMAL. (M)SDR COMA9610269Computer · malfunctionHEADING FLAG ON EHSI WILL NOT RESET. REPLACED THE NR 2 AHRS COMPUTER.SDR C2XA96CL024Steering Handle · wornCLE - FLT 3216 - CREW REPORTED, THAT THE NOSE WHEEL STEERING DISCONNECTS WHEN MAKING FULL LEFT TURNS WITH THE TILLER AND RUDDER PEDALS. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE STEERING HANDLE IAW EMB-120 MM 32-50-01, OPERATIONAL CHECKS WERSDR COMA9610268Actuator · malfunctionFLAP ASYMMETRY WARNING WHEN FLAPS SELECTED TO 25 DEGREES. REPLACED THE RT INBD FLAP ACTUATOR.SDR COMA9610267Skin · crackedLT OUTBD FLAP WAS CRACKED AT SEVERAL PLACES ON TRAILING EDGE. REPLACED FLAP.SDR COMA9610265Door Assy · brokenEMERGENCY LANDING GEAR EXTEND COMPARTMENT DOOR HINGE WAS BROKEN. REPAIRED BROKEN HINGE.SDR COMA9610264Bolt · brokenRT MLG DOOR HINGE BOLT WAS BROKEN. REPLACED BROKEN BOLT.SDR ASOA96034Prox Sensor · defectiveFLT 7228 - AFTER TAKEOFF MEI-ATL - CYCLED THE GEAR UP AND THE GEAR DID NOT RETRACT. CREW DECLARED A PRECAUTIONARY EMERGENCY AND RETURNED TO MEI, WHERE LANDING WAS MADE SAFELY AND WITHOUT INCIDENT. REMOVED AND REPLACED LEFT 'A' UPLOCK PROXIMITY SENSOR. PERFOSDR ASOA96033Seal · tornFLT 7268 - ROA-ATL - DURING CRUISE FLIGHT AT 20,000 FEET, CABIN PRESSURIZATION STARTED TO CLIMB. CREW ELECTED TO MAKE AN EMERGENCY DESCENT TO 10,000 FEET AND CONTINUE TO ATL, WHERE LANDING WAS MADE SAFELY AND WITHOUT INCIDENT. REMOVED AND REPLACED CARGO DOORSDR COMA9610266Control Box · malfunctionWHEN LANDING GEAR SELECTED DOWN, THE INDICATION WAS BOTH DOWN LOCK GREEN AND RED UNSAFE AT THE SAME TIME. REPLACED THE LANDING GEAR CONTROL BOX.SDR COMA9610263Flap Contl Unit · malfunctionFLAP DISAGREE WARNING AFTER TAKEOFF. REPLACED THE FLAP CONTROL UNIT. PART TOTAL CYCLES, 2,052.SDR COMA9610262Pump · leakingBLUE (RT) HYDRAULIC SYSTEM LOW FLUID LEVEL WARNING DURING APPROACH. QUANTITY GAUGE INDICATED EMPTY. REPLACED THE RT ENGINE DRIVEN HYDRAULIC PUMP DUE TO INTERNAL LEAKAGE TO CASE DRAIN. PART TOTAL CYCLES, 5,227.SDR COMA9610261Prop Mtg Flange · corrodedTHE RT ENGINE PROPELLER MOUNTING FLANGE HAD PITTING INSIDE THE MOUNTING BOLT HOLES. DISCREPANCY FOUND DURING SCHEDULED PROPELLER MAINTENANCE. REPLACED THE RT ENGINE.SDR WTAA960168Engine · bird strikeSFO - BIRD STRIKE REPORTED ABOVE RIGHT ENGINE INTAKE ON DEPARTURE FROM SFO. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (X)SDR COMA9610260Circuit Breaker · damagedEMERGENCY BUS LOST POWER, CONTROL BUS INOP, RT ENGINE INSTRUMENTS INOP, COPILOTS EFIS AND COMM RADIO INOP, A LANDING GEAR INDICATION INOP. FOUND BUS BAR CONNECTION TO CIRCUIT BREAKER 0470 LOOSE WITH HEAT DAMAGE TO BREAKER. REPLACED C/B 0470 AND ATTACHING HARSDR COMA9610259Flap Annunciator · malfunctionFLAP CONTROL FAULT WARNING DURING TAKEOFF. REPLACED THE FLAP ANNUNCIATOR PANEL.SDR COMA9610258Control Unit · malfunctionFLAP CONTROL FAULT WARNING DURING TAKEOFF. REPLACED FLAP CONTROL BOX.SDR COMA9610251Oil Bypass Line · failedRT ENGINE LOST OIL PRESSURE DURING FLIGHT. ENGINE SECURED AND ACFT DIVERT TO DAY. REPLACED LEAKING OIL COOLER BYPASS LINE.SDR C2XA96IA212Stringer · corrodedIAH - DURING C-CHECK INSPECTION, STRINGER 18 ON THE RIGHT FUSELAGE WAS FOUND TO BE CORRODED BETWEEN FRAME 38.5 AND FRAME 40. MAINTENANCE REMOVED THE DAMAGED SECTION OF STRINGER AND PERFORMED A SPLICE REPAIR PER EMB SRM 53-00-01, AND THE AIRCRAFT WAS APPROVED SDR C2XA96IA211Stringer · corrodedIAH - DURING C-CHECK INSPECTION, STRINGER 19 ON THE RIGHT FUSELAGE WAS FOUND TO BE CORRODED BETWEEN FRAME 38.5 AND FRAME 40. MAINTENANCE REMOVED THE DAMAGED SECTION OF STRINGER AND PERFORMED A SPLICE REPAIR PER EMB SRM 53-00-01, AND THE AIRCRAFT WAS APPROVED SDR C2XA96IA210Stringer · corrodedIAH - DURING C-CHECK INSPECTION, STRINGER 20 ON THE RIGHT FUSELAGE WAS FOUND TO BE CORRODED FROM FRAME 38.5 TO FRAME 40. MAINTENANCE REMOVED THE DAMAGED SECTION OF STRINGER AND PERFORMED A SPLICE REPAIR PER EMB SRM 53-00-01, AND THE AIRCRAFT WAS APPROVED FOR SDR C2XA96IA209Skin · corrodedIAH - DURING C-CHECK INSPECTION, THE BELLY SKIN BETWEEN FRAMES 39 AND 41 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE BELLY SKIN FROM FRAME 38 TO FRAME 42, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA96IA208Fire Bottle · under weightIAH - DURING C-CHECK INSPECTION, THE TOILET TRASH COMPARTMENT FIRE BOTTLE WAS FOUND TO BE UNDER WEIGHT. MAINTENANCE REMOVED AND REPLACED THE FIRE BOTTLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA96IA207Angle · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT AND RIGHT WEB ATTACH ANGLES ON THE FLOOR SUPPORTS AT FRAME 13 WERE FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE ATTACH ANGLES, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA96IA206Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT AFT FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA96IA205Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT LOWER SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA96IA204Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT FORWARD SIDEWALL SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA96IA203Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT AFT FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA96IA202Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT FORWARD SIDEWALL SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA96IA201Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT FORWARD FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA96IA200Bracket · brokenIAH - DURING C-CHECK INSPECTION, THE CARGO DOOR TORSION ROD FORWARD BRACKET WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE BRACKET AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA96IA199Buttstrap · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT CENTER AND RIGHT FLOOR BUTTSTRAPS FROM FRAME 34 TO FRAME 38 WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED SECTIONS AND SPLICED IN SERVICEABLE SECTIONS OF BUTTSTRAPS AND THE AIRCRAFT WAS APPROVED FOR RETURSDR C2XA96IA198Crease Beam · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT HAND CREASE BEAM FROM FRAME 38 TO FRAME 44 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE CREASE BEAM AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA96IA197Crease Beam · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT CREASE BEAM FROM FRAME 34 TO FRAME 38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE CREASE BEAM AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA96IA196T-Profile · corrodedIAH - DURING C-CHECK INSPECTION, THE T-PROFILES AT FRAMES 36 RIGHT, 38 RIGHT AND CENTER WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE T-PROFILES, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA96IA195T-Profile · corrodedIAH - DURING C-CHECK INSPECTION, THE T-PROFILE ON FRAMES 36 AND 38 LEFT WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE T-PROFILES AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA96IA194T-Profile · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT T-PROFILE AT FRAME 40 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE PROFILE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA96IA193T-Profile · corrodedIAH - DURING C-CHECK INSPECTION, THE T-PROFILE AT FRAME 40, RIGHT CENTER, WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE RIGHT CENTER T-PROFILE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA96IA192Floor Beam · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT FLOOR BEAM FROM FRAME 38 TO 44 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR BEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA96IA191Floor Beam · corrodedIAH - DURING C-CHECK INSPECTION, THE CENTER FLOOR BEAM FROM FRAMES 38 TO 44 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOOR BEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA96IA190T-Profile · corrodedIAH - DURING C-CHECK INSPECTION, THE T-PROFILE AT FRAME 42 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE T-PROFILE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)
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