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.

SDR COMA9610275Engine · failedTHE RIGHT ENGINE HAS HIGH NH SPEED AND LOW TORQUE. REPLACED THE RIGHT ENGINE.Sep 6, 1996 · N258CA · Emb EMB120RT · Engine (Turbine/Turboprop)SDR COMA9610273Indicator · failedTHE RT NP INDICATOR FAILED DURING TAKEOFF. REPLACED NP INDICATOR.Sep 5, 1996 · N268CA · Emb EMB120RT · Propeller Indication SystemSDR 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 RESep 5, 1996 · N233AS · Emb EMB120RT · Air Distribution FanSDR 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. BSep 4, 1996 · N196CA · Emb EMB120RT · Turbine SectionSDR 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 Sep 4, 1996 · N58733 · Emb EMB120RT · Fuel HeaterSDR COMA9610272Battery · dischargedAFT SECTION OF CABIN EMERGENCY LIGHTING IS INOPERATIVE. REPLACED EMERGENCY LIGHTING BATTERY. PART TOTAL CYCLES, 13,088.Sep 3, 1996 · N152CA · Emb EMB120RT · Emergency LightingSDR COMA9610271Battery · dischargedEMERGENCY FLOOR LIGHTING FORWARD OF ROW 4 IS INOPERATIVE. REPLACED EMERGENCY BATTERY. PART TOTAL CYCLES, 11,712.Sep 3, 1996 · N254CA · Emb EMB120RT · Emergency LightingSDR 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, AIRCRASep 2, 1996 · N16729 · Emb EMB120RT · Landing Gear Steering SystemSDR COMA9610270Actuator · malfunctionFLAP CONTROL FAULT WARNING DURING FLIGHT WITH FLAPS AT ZERO. REPLACED THE LT OUTBD FLAP ACTUATOR.Aug 31, 1996 · N1117H · Emb EMB120RT · Trailing Edge Flap ActuatorSDR GLBA96184Prox Switch · inoperativeMQT - LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. MAINTENANCE REMOVED AND REPLACED RIGHT MAIN PROXIMITY SWITCH. OPS NORMAL. (M)Aug 30, 1996 · N267UE · Emb EMB120RT · Landing Gear Retraction/Extension SystemSDR COMA9610269Computer · malfunctionHEADING FLAG ON EHSI WILL NOT RESET. REPLACED THE NR 2 AHRS COMPUTER.Aug 30, 1996 · N264CA · Emb EMB120RT · Integrated Flight SystemSDR 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 WERAug 30, 1996 · N16729 · Emb EMB120RT · Landing Gear Steering SystemSDR COMA9610268Actuator · malfunctionFLAP ASYMMETRY WARNING WHEN FLAPS SELECTED TO 25 DEGREES. REPLACED THE RT INBD FLAP ACTUATOR.Aug 29, 1996 · N159A · Emb EMB120RT · Trailing Edge Flap ActuatorSDR COMA9610267Skin · crackedLT OUTBD FLAP WAS CRACKED AT SEVERAL PLACES ON TRAILING EDGE. REPLACED FLAP.Aug 29, 1996 · N268CA · Emb EMB120RT · Trailing Edge FlapsSDR COMA9610265Door Assy · brokenEMERGENCY LANDING GEAR EXTEND COMPARTMENT DOOR HINGE WAS BROKEN. REPAIRED BROKEN HINGE.Aug 29, 1996 · N179CA · Emb EMB120RT · Service DoorsSDR COMA9610264Bolt · brokenRT MLG DOOR HINGE BOLT WAS BROKEN. REPLACED BROKEN BOLT.Aug 29, 1996 · N189CA · Emb EMB120RT · Landing Gear DoorsSDR 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. PERFOAug 29, 1996 · N211AS · Emb EMB120RT · Landing Gear Position and WarningSDR 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 DOORAug 29, 1996 · N127AM · Emb EMB120RT · Cargo/Baggage DoorsSDR 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.Aug 28, 1996 · N267CA · Emb EMB120RT · Landing Gear Retraction/Extension SystemSDR COMA9610263Flap Contl Unit · malfunctionFLAP DISAGREE WARNING AFTER TAKEOFF. REPLACED THE FLAP CONTROL UNIT. PART TOTAL CYCLES, 2,052.Aug 27, 1996 · N205CA · Emb EMB120RT · Trailing Edge Flap Control SystemSDR 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.Aug 27, 1996 · N254CA · Emb EMB120RT · Hydraulic Pump (Electric/Engine), MainSDR 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.Aug 27, 1996 · N257CA · Emb EMB120RT · Turbine Engine Reduction GearSDR 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)Aug 26, 1996 · N120AM · Emb EMB120RT · Engine (Turbine/Turboprop)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 HARAug 25, 1996 · N152CA · Emb EMB120RT · DC Power Distribution SystemSDR COMA9610259Flap Annunciator · malfunctionFLAP CONTROL FAULT WARNING DURING TAKEOFF. REPLACED THE FLAP ANNUNCIATOR PANEL.Aug 23, 1996 · N189CA · Emb EMB120RT · Trailing Flap Position Indicating SystemSDR COMA9610258Control Unit · malfunctionFLAP CONTROL FAULT WARNING DURING TAKEOFF. REPLACED FLAP CONTROL BOX.Aug 23, 1996 · N244CA · Emb EMB120RT · Trailing Edge Flap Control SystemSDR COMA9610251Oil Bypass Line · failedRT ENGINE LOST OIL PRESSURE DURING FLIGHT. ENGINE SECURED AND ACFT DIVERT TO DAY. REPLACED LEAKING OIL COOLER BYPASS LINE.Aug 23, 1996 · N1105G · Emb EMB120RT · Engine Oil Distribution (Airframe Furnished)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 Aug 22, 1996 · N15732 · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR 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 Aug 22, 1996 · N15732 · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR 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 Aug 22, 1996 · N15732 · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR 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)Aug 22, 1996 · N15732 · Emb EMB120RT · Fuselage Main, Plate/SkinSDR 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)Aug 22, 1996 · N15732 · Emb EMB120RT · Fire Bottle, PortableSDR 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)Aug 22, 1996 · N15732 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 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)Aug 22, 1996 · N15732 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR 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)Aug 22, 1996 · N15732 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR 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)Aug 22, 1996 · N15732 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR 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)Aug 22, 1996 · N15732 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR 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)Aug 22, 1996 · N15732 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR 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)Aug 22, 1996 · N15732 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR 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)Aug 22, 1996 · N15732 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 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 RETURAug 22, 1996 · N15732 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 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)Aug 22, 1996 · N15732 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 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)Aug 22, 1996 · N15732 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 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)Aug 22, 1996 · N15732 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 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)Aug 22, 1996 · N15732 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 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)Aug 22, 1996 · N15732 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 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)Aug 22, 1996 · N15732 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR 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)Aug 22, 1996 · N15732 · Emb EMB120RT · Fuselage Main, Floor BeamSDR 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)Aug 22, 1996 · N15732 · Emb EMB120RT · Fuselage Main, Floor BeamSDR 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)Aug 22, 1996 · N15732 · Emb EMB120RT · Fuselage Miscellaneous Structure
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