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 WTAA970045Speed Transducer · wornSMX - BRAKES FAILED DURING TAXI TO GATE. EMERGENCY BRAKES USED. MAINTENANCE DEFERRED ANTI-SKID SYSTEM PER MEL 32-42-2. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL BY REPLACING NR 4 WHEEL SPEED TRANSDUCER. OPERATIONAL CHECK SATIMar 14, 1997 · N276UE · Emb EMB120RT · Brake Anti-Skid SectionSDR COMA9710177Stop Tab · bentPROPELLER ASSEMBLY REMOVED FROM AIRCRAFT FOR HUB MAJOR INSPECTION. UPON INITIAL RECEIVING INSPECTION THE FEATHER STOP TAB S/N 248 WAS FOUND TO BE BENT APPROXIMATELY 0.125. PITCHLOCK SCREW WAS REMOVED FROM ASSEMBLY AND HELD FOR PROPOSED FUTURE REPAIR.Mar 14, 1997 · N156CA · Emb EMB120RT · Propeller AssemblySDR COMA9710176Bearing Insert · wornPROPELLER ASSEMBLY REMOVED FROM AIRCRAFT FOR HUB MAJOR INSPECTION. UPON INITIAL RECEIVING INSPECTION THE BLADE PIN BEARING INSERT WAS FOUND TO BE WORN IN AN OVAL FASHION. FURTHER INSPECTION SHOWED THAT THE INSERT HAD WORN TO .083 AT THE THINNEST POINT AND .0Mar 14, 1997 · N156CA · Emb EMB120RT · Propeller AssemblySDR COMA9710175Bearing Insert · wornPROPELLER ASSEMBLY REMOVED FROM AIRCRAFT FOR HUB MAJOR INSPECTION. UPON INITIAL RECEIVING INSPECTION THE BLADE PIN BEARING INSERT WAS FOUND TO BE IN AN OVAL FASHION. FURTHER INSPECTION SHOWED THAT THE INSERT HAD WORN TO .082 AT THE THINNEST POINT AND .099 ATMar 14, 1997 · N156CA · Emb EMB120RT · Propeller AssemblySDR COMA9710172Fuel Control · out of adjustTORQUE AND NP FLUCTUATIONS + OR - 5 PERCENT RT ENGINE. SWITCHED THE ENGINE ELECTRONIC CONTROL TO MANUAL AND ENTERED IN DEFERRED MAINTENANCE LOG.Mar 14, 1997 · N243CA · Emb EMB120RT · Fuel Control/Turbine EnginesSDR COMA9710171Antenna · failedWEATHER RADAR IS INOP. REPLACED THE RADAR ANTENNA.Mar 14, 1997 · N156CA · Emb EMB120RT · Weather Radar SystemSDR C2XA97IA102Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT WALL FORWARD 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)Mar 14, 1997 · N22727 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA97IA101Beam · corrodedIAH - DURING C-CHECK INSPECTION, THE FLIGHT ATTENDANTS SEAT INBOARD VERTICLE BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Mar 14, 1997 · N22727 · Emb EMB120RT · Passenger Compartment EquipmentSDR COMA9710174Lead · brokenRT PROPELLER DE-ICE SYSTEM INOP. REPLACED DEFECTIVE ELECTRICAL LEAD ON RT PROPELLER.Mar 13, 1997 · N130G · Emb EMB120RT · Propeller/Rotor Anti-Ice/De-Ice SystemSDR COMA9710170Ahrs · malfunctionYELLOW HEADING FLAP IN VIEW ON PILOT AND COPILOT EHS1. REPLACED THE NR 1 AHRS.Mar 13, 1997 · N258CA · Emb EMB120RT · Integrated Flight SystemSDR WTAA970043Hi Speed Warning · activatedLAX - HIGH SPEED WARNING ON TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY ON GROUND. OPERATIONAL CHECK GOOD. AIRCRAFT RELEASED FOR TEST FLIGHT. NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (Mar 11, 1997 · N271YV · Emb EMB120RT · Central WarningSDR COMA9710169Press Regulator · leakingRIGHT BLEED AIR DUCT LEAK WARNING CAME ON AFTER TAKEOFF. REPLACED THE RT DEICE SYSTEM PRESSURE REGULATOR.Mar 11, 1997 · N254CA · Emb EMB120RT · Airfoil Anti/De-ice SystemSDR C2XA97CL022Bulb · failedCLE - DURING A SCHEDULED INSPECTION, THE EXTERIOR EMERGENCY LIGHTS BOTH FORWARD AND AFT ON THE RIGHT SIDE OF THE FUSELAGE WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULBS IN BOTH FORWARD AND AFT EXTERIOR EMERGENCY LIGHTS IAW EMB Mar 11, 1997 · N16710 · Emb EMB120RT · Emergency LightingSDR C2XA97CL021Actuator · failedPIT - FLT 3610 - CREW REPORTED, RECEIVED A FLAP CONTROL FAULT IN FLIGHT WHICH WOULD NOT RESET. AIRCRAFT LANDED IN PIT WITHOUT INCIDENT. THE AIRCRAFT WAS MAINTENANCE FERRIED TO CLE, WHERE MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD FLAP ACTUATOR IAW EMMar 10, 1997 · N47722 · Emb EMB120RT · Trailing Edge Flap ActuatorSDR WTAA970041Actuator · out of adjustLAX - LANDING GEAR WILL NOT LOCK IN THE UP POSITION. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE ADJUSTED LEFT MAIN LANDING GEAR RETRACTION ACTUATOR. LANDING GEAR EXTENTION AND RETRACTION. OPERATIONAL CHMar 9, 1997 · N268UE · Emb EMB120RT · Landing Gear Retraction/Extension SystemSDR COMA9710168Hydraulic Syst · reqd serviceTHE LT (GREEN) HYDRAULIC SYSTEM LOW QUANTITY WARNING WAS ON DURING GEAR RETRACTION. THE RESERVOIR QUANTITY WAS AT THE BOTTOM OF THE GREEN RANGE. SERVICED HYDRAULIC SYSTEM TO FULL LEVEL, SYSTEM OPERATION NORMAL.Mar 7, 1997 · N156CA · Emb EMB120RT · Hydraulic System, MainSDR WTAA970039Fuel Door · unsecuredLAX - SERVICE DOOR WARNING LIGHT ILLUMINATED ON TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE RESECURED FUEL DOOR CAMLOCK. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M)Mar 5, 1997 · N284UE · Emb EMB120RT · Fluid Service DoorsSDR COMA9710167Flap Warning · activatedFLAP ASYMMETRY WARNING WHEN FLAPS SELECTED TO 15 DEGREES DURING APPROACH. COULD NOT DUPLICATE DISCREPANCY. FLAP SYSTEM OPERATIONAL TEST NORMAL.Mar 5, 1997 · N189CA · Emb EMB120RT · Trailing Flap Position Indicating SystemSDR C2XA97IA099Buttstrap · corrodedIAH - DURING C-CHECK INSPECTION, THE CENTER BUTTSTRAP AT FRAME 38 TO 44 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Mar 5, 1997 · N15713 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA97IA098Buttstrap · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT BUTTSTRAP FROM FRAME 38 TO 44 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Mar 5, 1997 · N15713 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA97IA097T-Profile · corrodedIAH - DURING C-CHECK INSPECTION, THE T-PROFILE AT FRAME 40 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Mar 5, 1997 · N15713 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA97IA096Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT 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)Mar 5, 1997 · N15713 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA97IA095Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT 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)Mar 5, 1997 · N15713 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA97IA094Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT WALL 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)Mar 5, 1997 · N15713 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA97IA093Buttstrap · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT BUTTSTRAP FROM FRAMES 38 TO 40 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Mar 5, 1997 · N15713 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA97IA092Buttstrap · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT BUTTSTRAP FROM FRAMES 34-38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE BUTTSTRAP AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Mar 5, 1997 · N15713 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA97IA091T-Profile · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT T-PROFILE AT FRAME 38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF T-PROFILE AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Mar 5, 1997 · N15713 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA97IA090Floorbeam · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT FLOORBEAM AT FRAME 38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF THE FLOORBEAM AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Mar 5, 1997 · N15713 · Emb EMB120RT · Fuselage Main, Floor BeamSDR C2XA97IA089T-Profile · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT CENTER T-PROFILE AT FRAME 38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Mar 5, 1997 · N15713 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA97IA088Buttstrap · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT BUTTSTRAP FROM FRAME 34 TO 38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE BUTTSTRAP AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Mar 5, 1997 · N15713 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA97IA087Crease Beam · corrodedIAH - DURING C-CHECK INSPECTION, THE CREASE BEAM AT FRAME 38 TO 40 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF CREASE BEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Mar 5, 1997 · N15713 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA97IA086Crease Beam · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT WALL 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)Mar 5, 1997 · N15713 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR ASOA97012Seal · defectiveEN ROUTE ATL-MYR - AT FL 190, THE CABIN STARTED TO CLIMB. THE CREW ATTEMPTED TO REGAIN CONTROL CABIN PRESSURE TO NO AVAIL. DESCENDED TO 8,000 FEET AND RETURNED TO ATL. REMOVED RTV FROM LEFT BOTTOM AIRSTAIR DOOR SEAL AND SHIMMED RIGHT SIDE OF AIRSTAIR DOOR. Mar 5, 1997 · N130AM · Emb EMB120RT · Passenger/Crew DoorsSDR ASOA97011Ahrs · defectiveFIFTY MILES SOUTH OF EVV AT 20,000 FEET, DESCENDING FOR APPROACH, NR 1 AHRS FAILED, RADAR FAILED, NR 2 AHRS SHOWED 20 DEGREES OFF. CAPTAIN DECLARED AND EMERGENCY AND HAT ATC GIVE HIM RADAR VECTORS INTO EVV. FIVE MILES OUT ON FINAL APPROACH, ALL SYSTEMS RETURMar 5, 1997 · N237AS · Emb EMB120RT · Integrated Flight SystemSDR GLBA97032Engine · low oilFSD - RIGHT ENGINE OIL PRESSURE DROPPED DOWN TO 30 PSID IN FLIGHT. MAINTENANCE SERVICED WITH ONE QUART ENGINE OIL. COMPLETED THREE PERFORMANCE RUNS WITHOUT OIL PRESSURE PROBLEMS. (M)Mar 4, 1997 · N267UE · Emb EMB120RT · Turbine Engine Oil SystemSDR C2XA97CL020Transponder · inoperativeCLE - FLT 3058 - CREW REPORTED, THAT THE NR 2 TRANSPONDER WAS INOPERATIVE, WITH NO FUNCTION OPERATING AT ALL. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE NR 2 TRANSPONDER, ALL OPERATIONAL CHECKS WERE SATISFACTMar 4, 1997 · N27707 · Emb EMB120RT · ATC Transponder SystemSDR C2XA97CL019Actuator · faultedCLE - FLT 3186 - CREW REPORTED, THAT AFTER TAKEOFF AND FLAPS SELECTED TO THE FULL UP POSITION THEY RECEIVED A FLAP ASYMMETRY ON THE INBOARD PAIR. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE LEFT INBOARD FLAP AMar 4, 1997 · N26714 · Emb EMB120RT · Trailing Edge Flap ActuatorSDR COMA9710166Annunciator · malfunctionedDURING CRUISE FLIGHT, FLAP AND STALL WARNING CAPTIONS ILLUMINATED ON THE M.A.P. REPLACED THE FLAP CONTROL UNIT AND ANNUNCIATOR UNIT. PART TOTAL CYCLES, 4,260.Mar 3, 1997 · N264CA · Emb EMB120RT · Central DisplaySDR COMA9710165Skin · dentedDURING INSPECTION, FOUND A DENT IN THE RIGHT WING LOWER SKIN BETWEEN RIBS 24 AND 25 AFT OF THE AUXILIARY SPAR. CUT OUT DENT AND INSTALLED A FILLER OF THE SAME THICKNESS, INSTALLED AN INTERNAL DOUBLER MADE OF 0.040 INCH 2024-T3 AND AN EXTERNAL DOUBLER MADE OF Mar 3, 1997 · N159A · Emb EMB120RT · Wing, Plate/SkinSDR COMA9710164Sensor · defectiveLANDING GEAR CONTROL HANDLE SAFETY LOCK DID NOT RELEASE AFTER TAKEOFF. REPLACED THE RIGHT HAND MLG WEIGHT ON WHEELS PROXIMITY SENSOR.Mar 3, 1997 · N243CA · Emb EMB120RT · Landing Gear Position and WarningSDR C2XA97CL018Switching Valve · dirtyCLT - FLIGHT 4231 - CREW REPORTED THAT THEY HAD SMOKE IN THE COCKPIT. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED BOTH ENGINES AND BLEED AIR SYSTEMS, ALL OPERATIONAL CHECKS WERE SATISFACTORY IAW EMB 120 MM 21-60-00, 36-00-00 AND 36-10-00. AIRCRAFT RELMar 2, 1997 · N12703 · Emb EMB120RT · Fuel Controlling SystemSDR COMA9710163Selector Control · malfunctionWHEN LANDING GEAR SELECTED UP, THE LEFT HAND MLG INTRANSIT LIGHTS REMAINED ON. REPLACED THE SELECTOR CONTROL ASSY.Feb 28, 1997 · N164D · Emb EMB120RT · Landing Gear SelectorSDR COMA9710158Annunciator · malfunctionFLAP CONTROL FAULT WARNING WHENEVER FLAPS ARE SELECTED FROM 15 TO 25 DEGREES. REPLACED THE FLAP ANNUNCIATOR UNIT. PART TOTAL CYCLES, 12,475.Feb 26, 1997 · N249CA · Emb EMB120RT · Trailing Flap Position Indicating SystemSDR C2XA97IA068Latch · wornIAH - FLT 3799 - PILOT REPORTED, THAT THE LEFT MAIN LANDING GEAR FORWARD OUTBOARD DOOR OPENED IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE DOOR LATCH AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Feb 26, 1997 · N16724 · Emb EMB120RT · Landing Gear Door Retract SectionSDR GLBA97033Wire · brokenSUX - EXIT LIGHT ON OVERHEAD BIN ROW 8 INOPERATIVE. MAINTENANCE SPLICED BROKEN WIRE. (M)Feb 25, 1997 · N279UE · Emb EMB120RT · Light System WiringSDR COMA9710159Door · not latchedSERVICE DOOR WARNING DURING TAKEOFF. FOUND THE FUEL SINGLE POINT SERVICE DOOR UNLATCHED. SECURED DOOR LATCHES AND AIRCRAFT CONTINUED SERVICE.Feb 25, 1997 · N130G · Emb EMB120RT · Fluid Service DoorsSDR COMA9710162Autofeather Sys · malfunctionedDURING APPROACH TO TLH, THE RIGHT HAND ENGINE AUTOFEATHER SYSTEM ACTIVATED. COULD NOT DUPLICATE DISCREPANCY. INSPECTION OF AUTOFEATHER SYSTEM FOUND NO DEFECTS.Feb 24, 1997 · N179CA · Emb EMB120RT · Propeller Feathering/ReversingSDR COMA9710161Fan · overheatELECTRICAL SMOKE ODOR COMING FROM AVIONICS VENT. REPLACED THE LEFT HAND AVIONICS COOLING FAN.Feb 24, 1997 · N189CA · Emb EMB120RT · Air Distribution FanSDR COMA9710160Prox Sensor · failedAFTER TAKEOFF AND GEAR SELECTED UP, THE LEFT HAND MLG 'A' LIGHT REMAINED ON. LANDING GEAR DID NOT RETRACT UNTIL EMERGENCY SYSTEM WAS ACTIVATED. REPLACED THE LEFT HAND MLG DOWNLOCK PROXIMITY SENSOR.Feb 24, 1997 · N200CD · Emb EMB120RT · Landing Gear Retraction/Extension SystemSDR COMA9710157Roller · dirtyFLAP DISAGREEMENT WARNING WHEN FLAPS RETRACTED AFTER TAKE OFF. REPLACED OUTBOARD FLAP ROLLERS.Feb 23, 1997 · N266CA · Emb EMB120RT · Trailing Edge Flaps
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