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 COMA9810137Light · looseFORWARD EMERGENCY EXIT FLOOR LIGHT IS LOOSE. SECURED LIGHT ASSY TO FLOOR.Jun 17, 1998 · N257CA · Emb EMB120RT · Emergency LightingSDR CA980706021Connecting Pin · broken(CAN) WHILE TOWING AIRCRAFT, WITHOUT EXCEEDING THE TURN LIMITS, THE NOSE GEAR TORQUE ARM CONNECTING PIN BROKE. SUBMITTER STATED THAT THE PIN WAS CRACKED FOR SOME TIME. THIS PIN HAS A LIMITED SERVICE LIFE OF 90,000 CYCLES AND IS INSPECTED AT EACH LANDING GEARJun 17, 1998 · Emb EMB120RT · Nose/Tail Landing Gear Attach SectionSDR C2XA98IA211Battery Pack · dischargedIAH - DURING C-CHECK INSPECTION, THE FORWARD FLOOR EMERGENCY LIGHTS FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK FOR THE AFFECTED LIGHTS IAW EMB120 MM CH 33-50-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jun 17, 1998 · N47722 · Emb EMB120RT · Emergency LightingSDR C2XA98IA210Crease Beam · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT CREASE BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 39 AND 44. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTTSTRAP IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Jun 17, 1998 · N47722 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA209Buttstrap · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT CENTER BUTTSTRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 38-44. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTTSTRAP IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Jun 17, 1998 · N47722 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA208Buttstrap · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT CENTER BUTTSTRAP BETWEEN FRAMES 34 AND 38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE EFFECTED SECTION OF BUTTSTRAP IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (MJun 17, 1998 · N47722 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA207T-Profile · corrodedIAH - DURING C-CHECK INSPECTION, THE T-PROFILE AT FRAME 40 RIGHT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE EFFECTED T-PROFILE IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Jun 17, 1998 · N47722 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA206Tee · corrodedIAH - DURING C-CHECK INSPECTION, THE T-PROFILE AT FRAME 38 RIGHT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE EFFECTED T-PROFILE IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Jun 17, 1998 · N47722 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA205Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT AFT FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMVOED AND REPLACED THE EFFECTED SEAT TRACK IAW EMBL-120 SRM 51-21-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Jun 17, 1998 · N47722 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA98IA204Support · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT WING NUMBER TWO UPPER SKIN SUPPORT AT RIB 21 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE EFFECTED SKIN SUPPORT IAW EMB-120 SRM 51-40-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Jun 17, 1998 · N47722 · Emb EMB120RT · Wing Miscellaneous StructureSDR C2XA98IA200Angle · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT DRAG ANGLE ON THE VERTICLE STABILIZER WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED THE DAMAGED SECTION OF THE DRAG ANGLE AND INSTALLED A REPAIR SPLICE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATIOJun 17, 1998 · N47722 · Emb EMB120RT · Vertical StabilizerSDR C2XA98IA199Support · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICLE SUPPORT AT FRAME 13 WAS FOUND TO BE CRACKED. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED A DOUBLER REPAIR IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Jun 17, 1998 · N47722 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98IA198Support · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT VERTICLE SUPPORT AT FRAME 13 WAS FOUND TO BE CRACKED. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED A DOUBLER IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Jun 17, 1998 · N47722 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810139Mechanism · malfunctionedFLAP ASYMMETRY, INBOARD FLAPS WOULD NOT DEPLOY. COULD NOT DUPLICATE DISCREPANCY, SYSTEM OPERATIONAL CHECK SATISFACTORY.Jun 16, 1998 · N196CA · Emb EMB120RT · Trailing Edge Flap Control SystemSDR C2XA98IA203Fuse · failedIAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS AT ROW 6 WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FUSE AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Jun 14, 1998 · N59708 · Emb EMB120RT · Emergency LightingSDR C2XA98IA201Smoke Detector · malfunctionedIAH - DURING FLT 3952 - THE CREW REPORTED A FALSE LAVATORY SMOKE INDICATION. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE LAVATORY SMOKE DETECTOR PANEL AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Jun 14, 1998 · N16723 · Emb EMB120RT · Smoke DetectionSDR MASA98124Light · crackedDURING ROUTINE MAINTENANCE, FOUND LEFT FORWARD EMERGENCY EXIT LIGHT ASSEMBLY CRACKED. REMOVED AND REPLACED LIGHT ASSEMBLY. (X)Jun 8, 1998 · N180YV · Emb EMB120RT · Emergency LightingSDR COMA9810135Battery · dischargedEMERGENCY LIGHTS AFT OF ROW 6 ARE INOPERABLE. REPLACED EMERGENCY LIGHTS BATTERY.Jun 8, 1998 · N462CA · Emb EMB120RT · Emergency LightingSDR C2XA98IA299Butt Strap · corrodedIAH - DURING C-CHECK INSPECTION, FOUND THE RIGHT BUTT STRAP AT FRAME 40 CORRODED. MAINTENANCE REMOVED THE CORROSION AND INSTALLED A REINFORCING DOUBLER IAW EMB120ER SRM 51-10-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Jun 8, 1998 · N16723 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA98CL045Hose · rupturedCLE - FLT 3079 - CREW REPORTED THAT THE COCKPIT AND CABIN FILLED WITH SMOKE DURING TAXI OUT, AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED A BLOWN HOSE AND CLEANED OIL FROM THE RIGHT ACM. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY IAW EMB-12Jun 8, 1998 · N15713 · Emb EMB120RT · Cabin Cooling SystemSDR COMA9810136Control Unit · failedAIRCRAFT HAS NO BRAKES DURING LANDING ROLL. REPLACED THE BRAKE CONTROL UNIT.Jun 5, 1998 · N267CA · Emb EMB120RT · Landing Gear Brake SystemSDR COMA9810134Wire · brokenSTALL AURAL WARNING WILL NOT SILENCE. REPAIRED BROKEN WIRE AT CONNECTOR PO194 COPILOTS STICK SHAKER.Jun 4, 1998 · N259CA · Emb EMB120RT · Navigation System WiringSDR COMA9810133Solenoid · inoperativeDURING 1C INSPECTION TASK 35-09, THE ROW 4 OXYGEN DOOR LATCH MECHANISM FAILED TO OPEN THE DOOR AND RELEASE THE OXYGEN MASKS. REPLACED THE SOLENOID FOR ROW 4 OXYGEN DOOR.Jun 4, 1998 · N261CA · Emb EMB120RT · Passenger Oxygen SystemSDR COMA9810132Switch · malfunctionRIGHT HAND BLEED AIR OVERHEAT WARNING DURING FLIGHT. REPLACED THE BLEED AIR OVERHEAT SWITCH.Jun 4, 1998 · N261CA · Emb EMB120RT · Bleed Air Indicating SystemSDR COMA9810131Bleed Valve · malfunctionRIGHT HAND BLEED AIR OVERHEAT WARNING DURING FLIGHT. REPLACED THE HIGH PRESSURE BLEED VALVE.Jun 4, 1998 · N261CA · Emb EMB120RT · Compressor Bleed ValveSDR COMA9810130Battery · dischargedEMERGENCY LIGHTS BY CABIN DOOR ARE INOPERABLE. REPLACED EMERGENCY BATTERY.Jun 3, 1998 · N254CA · Emb EMB120RT · Emergency LightingSDR MASA98112Battery Pack · dischargedDURING MAINTENANCE, AFT EMERGENCY LIGHTS, RT AFT SIDE, FAILED TO TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CHECK GOOD. (M)Jun 1, 1998 · N221YV · Emb EMB120RT · Emergency LightingSDR C2XA98CL043Cooling Fan · failedCLE - FLT 3204 - CREW REPORTED THAT DURING TAXI OUT THEY OBSERVED SMOKE IN THE COCKPIT AND CABIN, AIRCRAFT RETURNED TO THE GATE WITHOUT FURTER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE RIGHT GROUND COOLING FAN IAW EMB-120 MM 2Jun 1, 1998 · N17728 · Emb EMB120RT · Air Distribution FanSDR 98ZZZX2561Gearbox · chafedON REDUCTION GEARBOX JUST IN FRONT OF RIGHT FORWARD ENGINE MOUNT FORWARD LOWER BOLT HOLE, THERE IS A CHAFE MARK .958 INCH BY .480 INCH. DEEPEST SPOT IS .098 INCH CAUSED BY MISLOCATED BONDING WIRE FROM NACELLE TO ENGINE.Jun 1, 1998 · N212AS · Emb EMB120RT · Turbine Engine Reduction GearSDR COMA9810129Ahrs · failedPILOTS AHRS FAILED. REPLACED NR 1 AHRS.May 28, 1998 · N269CA · Emb EMB120RT · Integrated Flight SystemSDR GLBA98088Stringer · crackedFUSELAGE SKIN FLEXING UNDER AFT PASSENGER DOOR. ACTUATOR SUPPORT BRACKET HAS LOOSE RIVETS. FURTHER INSPECTION REVEALS CORROSION ON NR 10 STRINGER AND BRACKET. REPAIRED NR 10 STRINGER IAW EMB-120 SRM 53-00-03. (X)May 27, 1998 · N452UE · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR C2XA98CL041Hub · broken studCLE - DURING A SCHEDULED PROPELLER HUB TIME CHANGE, THE FIRST HUB HAD AN ATTACHMENT STUD BREAK DURING TORQUING. REFER TO SDR NR C2XA98CL040. THE SECOND REPLACEMENT HUB ALSO HAD AN ATTACHMENT STUD BREAK DURING THE FINAL TORQUE PROCEDURE. THE HUB WAS REMOVED AMay 27, 1998 · N12703 · Emb EMB120RT · Propeller Hub SectionSDR C2XA98CL040Hub · brokenCLE - DURING A SCHEDULED TIME CHANGE ON THE RIGHT HAND ENGINE PROPELLER HUB, ONE OF THE ATTACHMENT STUDS BROKE WHILE THE FINAL TORQUE WAS BEING APPLIED. PLEASE REFER TO SDR NR C2XA98CL041 FOR FAILURE OF THE SECOND HUB. THE HUB WAS REMOVED AND REPLACED IAW HAMay 27, 1998 · N12703 · Emb EMB120RT · Propeller Hub SectionSDR WTAA980083Oil System · req serviceACV - OIL PRESSURE WARNING ON LEFT ENGINE DURING TAKEOFF ROLL. TAKEOFF ABORTED. MAINTENANCE SERVICED ENGINE OIL TO PROPER LEVEL. OPERATIONAL CHECKS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M)May 25, 1998 · N268UE · Emb EMB120RT · Turbine Engine Oil SystemSDR COMA9810128Roller · wornFLAPS WOULD NOT RETRACT AFTER TAKEOFF. REPLACED FLAP ROLLERS AT LEFT HAND OUTBOARD FLAP.May 25, 1998 · N244CA · Emb EMB120RT · Trailing Edge FlapsSDR COMA9810127Pump · inoperativeLEFT ENGINE ELECTRIC FEATHER PUMP IS INOP. REPLACED AUXILIARY FEATHER PUMP.May 21, 1998 · N256CA · Emb EMB120RT · Propeller Controlling SystemSDR COMA9810126Battery · dischargedFORWARD CABIN EMERGENCY LIGHTING IS INOP. REPLACED EMERGENCY BATTERY.May 21, 1998 · N152CA · Emb EMB120RT · Emergency LightingSDR COMA9810125Engine · damagedRT ENGINE HOT START, TEMP REACHED 978 DEGREES. REMOVED ENGINE FOR INSPECTION.May 20, 1998 · N259CA · Emb EMB120RT · Engine (Turbine/Turboprop)SDR COMA9810124Fcu · malfunctionFLAP AND ADVANCED SWS INDICATIONS ON MAP. REPLACED THE FLAP CONTROL UNIT.May 19, 1998 · N255CA · Emb EMB120RT · Trailing Edge Flap Control SystemSDR COMA9810123Battery · dischargedSOME OF THE CABIN EMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY BATTERY.May 17, 1998 · N247CA · Emb EMB120RT · Emergency LightingSDR MASA98104Lamp · failedFLT 7593 - GNV-JAX - AFTER ARRIVING IN JAX, CREW REPORTED ONE WHITE EMERGENCY FLOOR TRACK LIGHT INOP. MAINTENANCE REMOVED AND REPLACED A BULB. AIRCRAFT WAS RETURNED TO SERVICE. (M)May 15, 1998 · N340JS · Emb EMB120RT · Emergency LightingSDR COMA9810122Hose · leakingLOW OIL PRESSURE WARNING ON RIGHT HAND ENGINE INFLIGHT SHUTDOWN. REPLACED OIL COOLER HOSE ASSEMBLY THAT WAS LEAKING DUE TO CHAFING DAMAGE.May 14, 1998 · N255CA · Emb EMB120RT · Engine Oil CoolerSDR COMA9810121Solenoid · shortedFLIGHT IDLE STOP SOLENOID CIRCUIT BREAKER TRIPPED. REPLACED SOLENOID.May 14, 1998 · N241CA · Emb EMB120RT · Power LeverSDR COMA9810120Sign · looseEXIT SIGN LOOSE AT ROW 5A. REPLACED EXIT SIGN.May 13, 1998 · N205CA · Emb EMB120RT · Emergency LightingSDR COMA9810119Sign · brokenEMERGENCY EXIT SIGN AT ROW 8 BROKEN. REPLACED EXIT SIGN.May 13, 1998 · N254CA · Emb EMB120RT · Emergency LightingSDR C2XA98IA182Light · inoperativeIAH - DURING PREFLIGHT INSPECTION, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY IAW EMB-120 MM 33-50-00 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)May 13, 1998 · N16710 · Emb EMB120RT · Emergency LightingSDR WTAA980078Wire · brokenSFO - CARGO DOOR WARNING ACTIVATED ON TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE DEFERRED DOOR WARNING SYSTEM PER MEL 52-70-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL BY REPAIRING BROKEN WIRE ON CARGO DOOR MMay 12, 1998 · N284UE · Emb EMB120RT · Door System WiringSDR COMA9810118Sensor · malfunctionedWHEN LANDING GEAR RETRACTED, THE NLG DOWN LIGHTS AND INTRANSIT LIGHTS REMAINED ON. REPLACED THE NLG DOWN LOCK PROXIMITY SENSOR.May 12, 1998 · N244CA · Emb EMB120RT · Landing Gear Position and WarningSDR COMA9810117Sensors · malfunction'TAKE OFF TRIM' WARNING SOUNDED. REPLACED ELEVATOR TRIM PROXIMITY SENSORS.May 12, 1998 · N257CA · Emb EMB120RT · Elevator Control SystemSDR COMA9810116Box Control · malfunctionedWHEN LANDING GEAR EXTENDED BOTH GREEN AND RED INDICATOR LIGHTS ILLUMINATED, AND ANTI-SKID FAIL INDICATION. COULD NOT DUPLICATE DISCREPANCY. REPLACED LANDING GEAR CONTROL ASSEMBLY FOR TROUBLESHOOTING.May 11, 1998 · N269CA · Emb EMB120RT · Landing Gear Position and Warning
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