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 COMA9810115Sign · brokenEXIT SIGN AT ROW 5A IS BROKEN. REPLACED EXIT SIGN.May 10, 1998 · N152CA · Emb EMB120RT · Emergency LightingSDR MASA98100Bulb · failedFLT 5275 - TPA-GNV - AFTER ARRIVAL IN GNV, THE CREW REPORTED AN OVERHEAD EMERGENCY EXIT LIGHT AT ROW 6A WAS INOP. MAINTENANCE REMOVED AND REPLACED THE BULB, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)May 8, 1998 · N180YV · Emb EMB120RT · Emergency LightingSDR COMA9810114Battery · dischargedEMERGENCY FLOOR PATH LIGHTING VERY DIM. REPLACED EMERGENCY BATTERY.May 8, 1998 · N168CA · Emb EMB120RT · Emergency LightingSDR WTAA980076Air Regulator · leakingACV - RIGHT ENGINE DUCT LEAK LIGHT ILLUMINATED AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE REPLACED RIGHT AIR REGULATOR. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M)May 5, 1998 · N455UE · Emb EMB120RT · Pneumatic Distribution SystemSDR WTAA9880075Radome · bird strikeFAT - BIRD STRIKE TO NOSE CONE AREA. AIRCRAFT REMAINS IN MAINTENANCE FOR REPAIRS. (M)May 4, 1998 · N251YV · Emb EMB120RT · Aerodynamic FairingsSDR COMA9810113Battery · dischargedCABIN EMERGENCY LIGHTS FAIL AFTER 15 SECONDS OF USE. REPLACED EMERGENCY LIGHTS BATTERY.May 4, 1998 · N243CA · Emb EMB120RT · Emergency LightingSDR WTAA980074Hmu · failedSBA - AT 14,000 FT, LEFT ENGINE TORQUE DROPPED TO ZERO AND T6 DROPPED TO 200-300 DEGREES. CREW SHUT DOWN ENGINE AND RETURNED TO THE STATION WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT ENGINE HMU. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICEMay 3, 1998 · N193YV · Emb EMB120RT · Fuel Controlling SystemSDR GLBA98069Lamp Socket · failedYAW DAMPENER LIGHT BULB FELL OUT OF SOCKET. SHORTED OUT TO GROUND. SMOKE CAME INTO COCKPIT. RETURNED TO GATE. YAW DAMPENER LIGHT BULB REMOVED FROM DEFECTIVE SOCKET AND MEL'D. (X)Apr 29, 1998 · N452UE · Emb EMB120RT · Flight Compartment LightingSDR COMA9810111De-Ice Boot · wornRIGHT ENGINE INLET DE-ICE SYSTEM FAILURE DURING CRUISE FLIGHT. REPLACED LEFT AND RIGHT ENGINE INLET DE-ICE BOOTS.Apr 29, 1998 · N152CA · Emb EMB120RT · Air Intake Anti/De-Ice SystemSDR C2XA98IA016Light · inoperativeIAH - FLT 3798 - PILOT REPORTED THAT THE FORWARD LEFT AND AFT RIGHT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE BULBS AND RELEASED THE AIRCRAFT. THE DISCREPANCY REPEATED ON FLIGHT 210B, CLL 1-7-99 WHERE MAINTENANCE PLACED Apr 27, 1998 · N16724 · Emb EMB120RT · Emergency LightingSDR ASOA98036Bolt · corrodedDURING C-CHECK INSPECTION, FOUND CORROSION AT THE AFT HINGE OF THE A/S/D. THE DOOR WAS REMOVED AND THE ATTACHMENT BOLT FOUND TO HAVE SEVERE PITTING. REMOVED AND REPLACED HINGE ATTACHMENT BOLT. (M)Apr 27, 1998 · N238AS · Emb EMB120RT · Passenger/Crew DoorsSDR ASOA98035Actuator · crackedDURING C-CHECK INSPECTION, FOUND AIRSTAIR DOOR ACTUATOR ROD SHEARED. INVESTIGATION REVEALED A CRACK ABOUT HALFWAY THROUGH THE THREADED AREA. REMOVED AND REPLACED ACTUATOR. (M)Apr 27, 1998 · N238AS · Emb EMB120RT · Passenger/Crew DoorsSDR 98ZZZX1897Actuator · shearedDURING RE-INSTALLATION OF THE PASSENGER/CREW ENTRANCE DOOR PREVIOUSLY REMOVED FOR OTHER MAINTENANCE ON ATLANTIC SOUTHEAST EMB120 AIRCRAFT, SN 53, THE FORWARD DOOR ACTUATOR ROD WAS FOUND SHEARED. INVESTIGATION REVEALED A CRACK ABOUT ONE-HALF WAY THROUGH THE THApr 27, 1998 · N238AS · Emb EMB120RT · Passenger/Crew DoorsSDR 98ZZZX1728Bolt · corrodedDURING ATLANTIC SOUTHEAST AIRLINES 'C' CHECK TASK CARD C-95, RUST WAS NOTED AT THE AFT HINGE OF THE PASS/CREW ENTRANCE DOOR. THE DOOR WAS REMOVED AND THE ATTACHMENT BOLT WAS FOUND TO HAVE SEVERE PITTING CORROSION. THE BOLT HAS BEEN REMOVED FROM SERVICE. RECApr 27, 1998 · N238AS · Emb EMB120RT · Passenger/Crew DoorsSDR WTAA980073Pin · failedACV - RIGHT MAIN GEAR FAILED TO INDICATE UP WITH ASSOCIATED VIBRATION AND SLIGHT YAW TO THE RIGHT. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. FOUND RIGHT LANDING GEAR ACTUATOR PIN ASSEMBLY AT LANDING GEAR BROKEN. MAINTENANCE REPLACED RIGHT GEAR ACTUATORApr 25, 1998 · N221YV · Emb EMB120RT · Landing Gear ActuatorSDR GLBA98068Fire Loop · chafedLT WHEEL WELL FIRE DETECTION ILLUMINATED. AIRCRAFT RETURNED TO GATE. REPLACED FIRE LOOP. (M)Apr 24, 1998 · N281UE · Emb EMB120RT · Fuselage Main, BulkheadSDR COMA9810110Apu · smokingFLIGHT DECK FILLED WITH SMOKE DURING PRE-FLIGHT INSPECTIONS, APU WAS OPERATING, NO PASSENGERS ON BOARD. DEFERRED APU PER MEL 49-00-1.Apr 24, 1998 · N189CA · Emb EMB120RT · APU Bleed Air SystemSDR C2XA98IA140Wire Harness · chafedIAH - DURING FLIGHT 3950 FROM VCT TO IAH, THE NUMBER 2 ENGINE EXPERIENCED A TORQUE SURGE FOLLOWED BY A LOSS OF POWER. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REPAIRED THE NR 2 ENGINE EEC WIRE HARNESS, AND THE AIRCRAFT WAS APPROVED FOR REApr 24, 1998 · N58733 · Emb EMB120RT · Engine Fuel System WiringSDR COMA9810108T/O Warning · malfunction'TRIM' AURAL WARNING DURING TAKEOFF. REPLACED THE AUDIO WARNING UNIT.Apr 22, 1998 · N205CA · Emb EMB120RT · Central WarningSDR MASA98092Battery · dischargedDURING ROUTINE MAINTENANCE, FOUND AFT EMERGENCY LIGHT BATTERY WEAK. REMOVED AND REPLACED BATTERY. (M)Apr 21, 1998 · N289UE · Emb EMB120RT · Emergency LightingSDR COMA9810109Control Valve · malfunctionLEFT AND RIGHT OUTBOARD WING DE-ICE CAUTION WARNINGS AFTER TAKEOFF. REPLACED THE DE-ICE EJECTOR CONTROL VALVE.Apr 21, 1998 · N249CA · Emb EMB120RT · Airfoil Anti/De-ice SystemSDR ASOA98033Seal · blownON CLIMB-OUT FYV-DFW, CABIN BEGAN CLIMBING IN EXCESS OF 1000 FPM AT 16,000 FT. AS CABIN CONTINUED TO CLIMB, CREW INITIATED THE AUTOMATIC PRESSURIZATION INOP CHECKLIST. THE PROCEDURE DID NOT WORK AS THE CABIN WAS STILL CLIMBING AT 22,000 FEET. OXYGEN MASKS WApr 21, 1998 · N504AS · Emb EMB120RT · Cargo/Baggage DoorsSDR MASA98091Light · crackedDURING ROUTINE MAINTENANCE, FOUND EMERGENCY EXIT SIGN HOUSING CRACKED (AT LEFT OVERWING EMERGENCY EXIT). REMOVED AND REPLACED EMERGENCYEXIT SIGN ASSEMBLY. (M)Apr 20, 1998 · N289UE · Emb EMB120RT · Emergency LightingSDR MASA98089Light · inoperativeDURING ROUTINE MAINTENANCE, FOUND LT LOWER EXTERIOR EMERGENCY LIGHT BULB WOULD NOT ILLUMINATE. REMOVED AND REPLACED EXTERIOR EMERGENCY LIGHT ASSEMBLY. (M)Apr 20, 1998 · N289UE · Emb EMB120RT · Emergency LightingSDR COMA9810112Wheel · crackedMAIN WHEEL ASSEMBLY WAS REMOVED FROM AIRCRAFT BY MECHANIC DUE TO LOW PRESSURE. TIRE SHOP FOUND INBOARD (P/N 300-604-1) WAS MISSING A SECTION OF WHEEL FLANGE APPROXIMATELY 12 INCHES LONG. WHEEL ASSEMBLY HAS GONE THRU 45 TIRE CHANGES SINCE NEW. WHEEL ASSEMBLYApr 20, 1998 · N241CA · Emb EMB120RT · Wheel/Ski/FloatSDR COMA9810107Wheel · crackedMAIN WHEEL ASSEMBLY WAS REMOVED FROM AIRCRAFT BY MECHANIC DUE TO LOW PRESSURE. TIRE SHOP FOUND INBOARD (P/N 300-604-1) WAS MISSING A SECTION OF WHEEL FLANGE APPROXIMATELY 12 INCHES LONG. WHEEL ASSEMBLY (P/N 3-1446-1) WHEEL ASSEMBLY HAS GONE THROUGH 45 TIRE CApr 20, 1998 · N241CA · Emb EMB120RT · Wheel/Ski/FloatSDR MASA98088Bulb · goodDURING ROUTINE MAINTENANCE, FOUND FORWARD EMERGENCY LIGHT BULB HAD COME LOOSE FROM THE SOCKET. CLEANED LIGHT SOCKET ASSEMBLY AND REINSTALLED BULB. (M)Apr 19, 1998 · N289UE · Emb EMB120RT · Emergency LightingSDR ASOA98031Acm · inoperativeAFTER TAKEOFF ATL-ILM, THE CREW NOTICED A BURNING OIL TYPE SMELL COMING FROM THE AIR CONDITIONING SYSTEM, FOLLOWED BY THE LAVATORY SMOKE DETECTOR GOING OFF. THE CREW SHUT OFF THE AIR CONDITIONING SYSTEM, DECLARED AN EMERGENCY AND RETURNED TO ATL WHERE LANDINGApr 19, 1998 · N501AS · Emb EMB120RT · Cabin Cooling SystemSDR COMA9810106Fitting · wornDURING LEFT ENGINE CHANGE, FOUND THE INBOARD, FORWARD SUPPORT ROD, FORWARD ATTACH BEARING TO HAVE EXCESSIVE PLAY. REPLACED INBOARD, FORWARD NACELLE SUPPORT ROD FORWARD FITTING.Apr 18, 1998 · N254CA · Emb EMB120RT · Nacelle/Pylon, Attach FittingsSDR COMA9810105Fitting · wornDURING LEFT ENGINE CHANGE, FOUND PLAY IN ONE BEARING OF THE INBOARD NACELLE SUPPORT ROD CLUSTER FITTING. REPLACED INBOARD NACELLE SUPPORT ROD CLUSTER FITTING.Apr 18, 1998 · N254CA · Emb EMB120RT · Nacelle/Pylon, Attach FittingsSDR COMA9810104Fitting · wornDURING LEFT ENGINE CHANGE, FOUND THE SECOND FROM AFT NACELLE SUPPORT ROD ATTACH FITTING ON THE INBOARD SIDE TO HAVE EXCESSIVE PLAY AT THE BEARING. REPLACED THE FITTING.Apr 18, 1998 · N254CA · Emb EMB120RT · Nacelle/Pylon, Attach FittingsSDR COMA9810103Fitting · wornDURING LEFT ENGINE CHANGE, FOUND THE MOST AFT, INBOARD NACELLE SUPPORT ROD ATTACH BEARING TO HAVE EXCESSIVE PLAY. REPLACED THE FITTING.Apr 18, 1998 · N254CA · Emb EMB120RT · Nacelle/Pylon, Attach FittingsSDR ASOA98030Relay Panel · looseON FINAL APPROACH DHN-ATL, EXPERIENCED EMERGENCY BUS 1 FAILURE. CREW EXECUTED A GO-AROUND AND PROCEEDED WITH CHECKLIST. WHILE CIRCLING TO LAND, RIGHT ENGINE NP FELL TO 50 PERCENT WITH ENGINE PRODUCING POWER. CREW ELECTED TO LEAVE ENGINE RUNNING, DECLARE AN Apr 18, 1998 · N227AS · Emb EMB120RT · AC Power Distribution SystemSDR WTAA980068Air Data Sensor · failedFAT - AURAL WARNING, GROUND PROXIMITY WARNING AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION. MAINTENANCE DEFERRED GPWS. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL BY REPLACING AIR DATA SENSOR NR 3. GPWS TEST NORMAL. LEAK CHECK Apr 17, 1998 · N250YV · Emb EMB120RT · Air Data ComputerSDR COMA9810102Leak Warning · activatedRIGHT HAND DUCT LEAK WARNING DURING TAKEOFF. COULD NOT DUPLICATE PROBLEM.Apr 15, 1998 · N263CA · Emb EMB120RT · Pneumatic Indicating SystemSDR C2XA98IA136Butt Strap · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT BUTT STRAP WAS FOUND TO BE CORRODED FROM FRAME 39 TO 46. MAINTENANCE REMOVED AND REPLACED THE BUTT STRAP IAW EMB-120 SRM 51-40-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Apr 15, 1998 · N16718 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA135Butt Strap · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT BUTT STRAP BETWEEN FRAMES 39 AND 46 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE BUTT STRAP IAW EMB-120 SRM 51-40-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Apr 15, 1998 · N16718 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA134Stringer · crackedIAH - DURNG C-CHECK INSPECTION, THE PREVIOUS REPAIR AT STRINGER 10 OF THE LEFT WING WAS FOUND TO BE CRACKED BETWEEN RIBS 7 AND 8. MAINTENANCE REMOVED AND REPLACED THE REPAIR DOUBLER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5710-01010 Apr 15, 1998 · N16718 · Emb EMB120RT · Wing, Longeron/StringerSDR C2XA98IA133Drag Angle · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT DRAG ANGLE ON THE VERTICLE STABILIZER WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5530-01013 AND THE AIRCRAFT WAS APPROVED FOR RETURNApr 15, 1998 · N16718 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA132T-Profile · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT T-PROFILE AT FRAME 36 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE IAW EMB 120 SRM 51-40-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Apr 15, 1998 · N16718 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA131Butt Strap · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT CENTER BUTT STRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 30 AND 34. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IAW EMB-120 SRM 51-20-04 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (Apr 15, 1998 · N16718 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA130Stringer · corrodedIAH - DURING C-CHECK INSPECTION, STRINGER 21 LEFT WAS FOUND TO BE CORRODED BETWEEN FRAMES 41 AND 42. MAINTENANCE REMOVED THE DAMAGED SECTION OF STRINGER AND PERFORMED A SPLICE REPAIR IAW EMB120 SRM 53-00-03 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 15, 1998 · N16718 · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR C2XA98IA129Butt Strap · corrodedIAH - DURING C-CHECK INSPECTION, THE CENTER BUTT STRAP AT FRAMES 25-30 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB-120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Apr 15, 1998 · N16718 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA128Support · crackedIAH - DURING C-CHECK INSPECTION, THE CENTER FLOOR SUPPORT WAS FOUND TO BE CRACKED AT FRAME 13. MAINTENANCE PERFORMED A SPLICE REPAIR IAW EMB120 SRM 51-21-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Apr 15, 1998 · N16718 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA127Support · corrodedIAH - DURING C-CHECK INSPECTION, THE FLOOR SUPPORT BEAM AT FRAME 16 LEFT WAS FOUND TO BE CORRODED. MAINTENANCE PERFORMED DOUBLER REPAIR IAW EMB120 SRM 51-10-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Apr 15, 1998 · N16718 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA126Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT AFT FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK IAW EMB-120 SRM 53-01-05 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Apr 15, 1998 · N16718 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA98IA125Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT FORWARD SEAT TRACK WAS FOUND TO BE CORRODED FROM FRAME 17 THROUGH FRAME 25. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK IAW EMB120 SRM 53-01-05 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Apr 15, 1998 · N16718 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA98IA124Support · crackedIAH - DURING C-CHECK INSPECTION, THE VERTICLE SUPPORT AT FRAME 13 RIGHT WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB120 SRM 51-10-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Apr 15, 1998 · N16718 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA123Support · crackedIAH - DURING C-CHECK INSPECTION, THE VERTICLE FLOOR SUPPORT AT FRAME 13 LEFT WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB-120 SRM 51-10-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Apr 15, 1998 · N16718 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA122Support · corrodedIAH - DURING C-CHECK INSPECTION, THE FLOOR SUPPORT BEAM AT FRAME 43 UNDER THE LEFT CENTER BUTT STRAP WAS FOUND TO BE CORRODED. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Apr 15, 1998 · N16718 · Emb EMB120RT · Fuselage Miscellaneous Structure
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