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 C2XA97IA118Rib · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT WING NOSE RIB AT RIB 20 WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED A DOUBLER REPAIR AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Mar 31, 1997 · N12709 · Emb EMB120RT · Wing, Rib/BulkheadSDR C2XA97IA117Rib · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT WING NOSE RIB AT RIB 21 WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED A DOUBLER REPAIR AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Mar 31, 1997 · N12709 · Emb EMB120RT · Wing, Rib/BulkheadSDR COMA9710191Actuator · malfunctionFLAP CONTROL FAULT WARNING DURING TAKEOFF. REPLACED THE LEFT HAND OUTBOARD FLAP ACTUATOR.Mar 30, 1997 · N1105G · Emb EMB120RT · Trailing Edge Flap ActuatorSDR C2XA97CL031Outflow Valve · leakingCLE - FLT 3295 - CREW REPORTED, THAT THE AIRCRAFT WOULD NOT HOLD PRESSURIZATION IN AUTO OR MANUAL MODES. AIRCRAFT RETURN TO FIELD. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE ELECTRO-PNEUMATIC OUTFLOW VALVE IAW EMB-120 MM 21-30-03. OPERMar 30, 1997 · N15721 · Emb EMB120RT · Pressure Regulator/Outflow ValveSDR ASOA97018Pressure Line · leakingFLT 7395 - EN ROUTE EVV-ATL, LOST GREEN HYDRAULIC SYSTEM PRESSURE. CREW DECLARED AN EMERGENCY AND LANDED SAFELY IN ATL WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED LEFT GREEN SYSTEM MAIN PRESSURE LINE TO RESERVOIR. OPERATIONAL AND LEAK CHECKS WERE GOOD, AMar 30, 1997 · N214AS · Emb EMB120RT · Hydraulic System, MainSDR ASOA97017Wire · chafedFLT 7721 - ON PREFLIGHT, FOUND THREE FORWARD EMERGENCY LIGHTS INOPERABLE. REPAIRED WIRING FOR FORWARD SECTION OF FLOOR EMERGENCY TRACK LIGHTING. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT RELEASED FOR FURTHER SERVICE. (M)Mar 30, 1997 · N223AS · Emb EMB120RT · Light System WiringSDR GLBA97053Brakes · req'd serviceHON - BRAKES REQUIRE AN EXCESSIVE AMOUNT OF FORCE TO SLOW AIRCRAFT. MAINTENANCE BLED BRAKE SYSTEM. (M)Mar 29, 1997 · N129AM · Emb EMB120RT · Landing Gear Brake SystemSDR COMA9710190Door · not latchedSERVICE DOOR WARNING CAME ON AFTER TAKEOFF. FOUND FUEL SERVICE DOOR UNLATCHED. SECURED LATCHES AND AIRCRAFT RETURNED TO SERVICE.Mar 28, 1997 · N1117H · Emb EMB120RT · Fluid Service DoorsSDR COMA9710189Flap Contl Unit · malfunctionFLAP ASYMMETRY WARNING DURING TAKEOFF ROLL. REPLACED THE FLAP CONTROL UNIT.Mar 28, 1997 · N189CA · Emb EMB120RT · Trailing Edge Flap Control SystemSDR GLBA97052Clamp · looseSUX - LEFT DUCT LEAK, PRECAUTIONARY SHUT-DOWN. MAINTENANCE SECURED LOOSE CLAMPS ON ENVIRONMENTAL CROSS-FEED LINE. (X)Mar 27, 1997 · N452UE · Emb EMB120RT · Engine Bleed Air SystemSDR GLBA97051Fire Loop · failedDEN - ENGINE/WHEEL WELL FIRE DETECTION SYSTEM INOP LIGHT ILLUMINATED. MAINTENANCE REPLACED LEFT ENGINE FIRE LOOP. (M)Mar 27, 1997 · N129AM · Emb EMB120RT · Fire DetectionSDR COMA9710209Frame · burnedON 2C TAS K 313-01Z, FUSELAGE FRAME 52 CANTED FRAME, UPPER HALF, WAS FOUND DAMAGED BY ARCING OF THE APU GENERATOR WIRE TERMINALS BOLTED TO THE FRAME. THE FRAME UPPER HALF WAS REPLACED PER SRM CHAP 51 STANDARD PRACTICES AND THE APU FIREWALL WAS REPAIRED PER SRMar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Main, FrameSDR COMA9710208Beam · corrodedON 2C TASK 5310-131/132-O1I, THE CABIN DOOR FLOOR SUPPORT FORWARD CENTER OMEGA BEAM WAS FOUND DAMAGED IN THREE PLACES, 1) CORROSION, 2) SMALL CRACK, 3) HOLE CAUSED BY CARPET TRIM SCREW IMPROPERLY INSTALLED. THE OMEGA BEAM WAS REPAIRED PER AERODESIGN REPORT NRMar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710207Frame · cougedON 4C TASK 5330-262-01I, FUSELAGE FRAME 44 WAS FOUND DAMAGED BY CARGO COMPARTMENT LINING SCREWS IMPROPERLY INSTALLED ON RT SIDE. FRAME 44 WAS REPAIRED PER AERODESIGN REPORT NR 2243-1,REV.IR, 3-26-97.Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Main, FrameSDR COMA9710206Angle · corrodedON 4C TASK 5320-152-01I, THE FUSELAGE DOOR FRAME, FOR THE RT AFT EMERGENCY EXIT LOWER ANGLE WAS FOUND CORRODED, WHERE THE EXIT DOOR LOWER GUIDE PIN RECEPTACLES (P/N 120-27743-001) ARE ATTACHED TO IT. THE RECEPTACLES AND THE ANGLE WERE REPLACED PER SRM CHAP 51Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710205Butt Strap · corrodedON 2C TASK 5320-141-03I, THE CABIN FLOORBEAM LT BUTT-STRAP WAS FOUND CORRODED. REPLACED PER SRM CHAP 51 STANDARD PRACTICES.Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710204Tee Section · corrodedON 2C TASK 5310-131-01I, THE CABIN FLOOR SUPPORT LT T-SECTION OF FRAME 20 WAS FOUND CORRODED. REPLACED PER SRM CHAP 51 STANDARD PRACTICES.Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710203Crossbeam · corrodedON 2C TASK 5310-131-01I, THE CABIN FLOOR SUPPORT LT CROSSBEAM AT FRAME 20 WAS FOUND CORRODED. REPLACED PER SRM CHAP 51 STANDARD PRACTICES.Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710202Sill · corrodedON 2C TASK 5310-131-01I, THE CABIN FLOOR SUPPORT FORWARD LT SILL WAS FOUND CORRODED. REPLACED PER SRM CHAP 51 STANDARD PRACTICES.Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710200Tee Section · corrodedON 2C TASK 5310-131-01I, THE CABIN FLOOR SUPPORT LT T-SECTION AT FRAME 16 WAS FOUND CORRODED. REPLACED PER SRM CHAP 51 STANDARD PRACTICES.Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710199Crossbeam · corrodedON 2C TASK 5310-132-01I, THE CABIN FLOOR SUPPORT RT CROSSBEAM AT FRAME 16 WAS FOUND CORRODED. REPLACED PER SRM CHAP 51 STANDARD PRACTICES.Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710198Butt Strap · corrodedON 2C TASK 5310-132-01I, THE FORWARD RT FLOOR BEAM BUTT STRAP WAS FOUND CORRODED. REPLACED PER SRM CHAP 51 STANDARD PRACTICES.Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710197Butt Strap · corrodedON 2C TASK 5310-131-01I, THE FORWARD LEFT FLOORBEAM BUTT-STRAP, WAS FOUND CORRODED. REPLACED PER SRM CHAP 51 STANDARD PRACTICES.Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710196Butt Strap · corrodedON 2C TASK 5310-131/132-01I, THE CABIN FLOORBEAM CENTER BUTT STRAP WAS FOUND CORRODED. REPLACED PER SRM CHAP 51 STANDARD PRACTICES.Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710195Butt Strap · corrodedON 2C TASK 5310-131/132O1I, THE FORWARD CABIN FLOOR SUPPORT CENTER BUTT STRAP WAS FOUND CORRODED. REPLACED PER AERODESIGN REPORT NR 1671-1, REV. A, 1-28-97.Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710194Angle · crackedON 2C TASK 5720-651-01I, THE RIGHT WING LOWER SKIN SUPPORT ANGLE, AT RIB 16, BETWEEN STRINGERS 8 AND 10, WAS FOUND CRACKED. THE ANGLE WAS REPLACED PER SRM CHAP 51 STANDARD PRACTICES.Mar 27, 1997 · N266CA · Emb EMB120RT · Wing Miscellaneous StructureSDR COMA9710193Angle · crackedON 2C TASK 5720-622-01I, THE RIGHT WING LOWER SKIN SUPPORT ANGLE WAS FOUND CRACKED AT RIB 8, BETWEEN STRINGERS 10 AND 11. THE ANGLE WAS REPLACED PER SRM CHAP 51 STANDARD PRACTICES.Mar 27, 1997 · N266CA · Emb EMB120RT · Wing Miscellaneous StructureSDR COMA9710192Wire · looseTAKEOFF TRIM WARNING DURING TAKEOFF ROLL. REPAIRED LOOSE WIRING AT THE ELEVATOR TRIM TAB PROXIMITY SENSORS.Mar 27, 1997 · N161CA · Emb EMB120RT · Elevator Tab Control SystemSDR C2XA97CL029Computer · failedRIC - FLT 3053 - CREW REPORTED, THAT ON TAKEOFF AT 80 KNOTS THE STICK PUSHER AND SHAKER ACTIVATED AND THE STALL WARNING LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED WITHOUT INCIDENT. THE AIRCRAFT WAS RELEASED IAW MEL 27-36-2, AFTER ARRIVING AT A MAINTENANCE BAMar 26, 1997 · N40717 · Emb EMB120RT · Stall Warning SystemSDR ASOA97016Oil System · req'd serviceFLT 7400 - DURING CLIMB-OUT FYV-DFW, LEFT ENGINE OIL PRESSURE MOMENTARILY WENT OT 35-45 PSI. THE CREW DECLARED AN EMERGENCY AND RETURNED TO FYV WHERE LANDING WAS MADE SAFELY AND WITHOUT FURTHER INCIDENT. LOCAL MECHANIC SERVICED THE LEFT ENGINE WITH 4 QUARTS Mar 26, 1997 · N502AS · Emb EMB120RT · Turbine Engine Oil SystemSDR COMA9710188Relay Box · malfunctionedLANDING GEAR DID NOT RETRACT WHEN SELECTED UP AFTER TAKE OFF. COULD NOT DUPLICATE DISCREPANCY. REPLACED THE LANDING GEAR RELAY BOX FOR TROUBLESHOOTING.Mar 24, 1997 · N137H · Emb EMB120RT · Landing Gear Retraction/Extension SystemSDR COMA9710185Fire Module · failedRT ENGINE FIRE WARNING LIGHT ON. REPLACED DEFECTIVE FIRE DETECTION CONTROL MODULE.Mar 24, 1997 · N179CA · Emb EMB120RT · Fire DetectionSDR GLBA97044Flap Selector · failedORD - FLAPS WILL NOT GO PAST 25 DEGREES WHEN FLAPS 45 DEGREES SELECTED. MAINTENANCE REPLACED FLAP SELECTOR. (M)Mar 22, 1997 · N128AM · Emb EMB120RT · Trailing Edge Flap Control SystemSDR COMA9710187Air Speed Ind · inaccurate20 KNOT DIFFERENCE BETWEEN PILOTS AND CO-PILOTS AIRSPEED INDICATORS. REPLACED PILOTS AIR SPEED INDICATOR.Mar 22, 1997 · N196CA · Emb EMB120RT · Airspeed/Mach IndicatorSDR COMA9710186Engine · high oil consumRIGHT ENGINE OIL PRESSURE DROPPED TO 52 PSI. OIL CONSUMPTION WAS EXCESSIVE. REPLACED ENGINE.Mar 21, 1997 · N259CA · Emb EMB120RT · Engine (Turbine/Turboprop)SDR MASA97019Hydraulic Line · crackedAIR SHUTTLE 5610 - CLT-GNV - EN ROUTE LOST ALL GREEN HYDRAULIC FLUID AND PRESSURE. MANUALLY EXTENDED LANDING GEAR PER QRH AND DIVERTED TO JAX. AIRCRAFT LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE FOUND HYDRAULIC LINE TO BE CRACKED. REMOVED AND REPLACED HMar 20, 1997 · N270UE · Emb EMB120RT · Hydraulic System, MainSDR COMA9710184Displ Proc Unit · malfunctionTHE NR 1 DPU FLAG ON DURING TAKEOFF. REPLACED THE NR 1 DPU-86H.Mar 20, 1997 · N257CA · Emb EMB120RT · Central DisplaySDR COMA9710183Ahrs · malfunctionBOTH HEADING INDICATORS ARE 30 TO 40 DEGREES OFF DURING TAKEOFF. REPLACED THE NR 1 AHRS.Mar 20, 1997 · N257CA · Emb EMB120RT · Integrated Flight SystemSDR C2XA97CL028Relay Box · failedCLE - FLT 3092 - CREW REPORTED, THAT AFTER TAKEOFF THE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED THE LANDING GEAR SYSTEM THEN REMOVED AND REPLACED THE GEAR RELAY BOX IAW EMB-120MM 32-31-02. THE LANDING GEAR CONTROL HAMar 20, 1997 · N16719 · Emb EMB120RT · Landing Gear Retraction/Extension SystemSDR C2XA97CL024Bulb · failedCLE - DURING A SCHEDULED INSPECTINO THE FORWARD CEILING MOUNTED EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE LIGHT ASSEMBLY, THEN REMOVED AND REPLACED THE BULB. OPERATIONAL CHECKS WERE SATISFACTORY IAW EMB 120 MM 33-51-01. AIRCRAFMar 19, 1997 · N16702 · Emb EMB120RT · Emergency LightingSDR COMA9710182Relay Box · failedLANDING GEAR DID NOT EXTEND WHEN SELECTED DOWN FOR LANDING. ALTERNATE EXTENSION SYSTEM WAS USED. REPLACED THE LANDING GEAR RELAY BOX. PART TOTAL CYCLES, 18,624.Mar 18, 1997 · N462CA · Emb EMB120RT · Landing Gear Retraction/Extension SystemSDR COMA9710180Bearing Insert · wornPROPELLER ASSEMBLY REMOVED FROM AIRCRAFT FOR SCHEDULED ENGINE CHANGE. ASSEMBLY WAS RECEIVED IN THE PROPELLER SHOP DUE TO BLADES BEING EXCESSIVELY LOOSE CAUSING AN IMBALANCE SITUATION. FOUND BEARING INSERT WORN IN AN OVAL FASHION, MEASURING FROM 0.0665 - 0.09Mar 18, 1997 · N189CA · Emb EMB120RT · Propeller AssemblySDR COMA9710179Bearing Insert · wornPROPELLER ASSEMBLY REMOVED FROM AIRCRAFT FOR SCHEDULED ENGINE CHANGE. ASSEMBLY WAS RECEIVED IN THE PROPELLER SHOP DUE TO BLADES BEING EXCESSIVELY LOOSE CAUSING AN IMBALANCE SITUATION. FOUND BEARING INSERT WORN IN AN OVAL FASHION, MEASURING FROM 0.0725 - 0.09Mar 18, 1997 · N189CA · Emb EMB120RT · Propeller AssemblySDR COMA9710178Bearing Insert · wornPROPELLER ASSEMBLY REMOVED FROM AIRCRAFT FOR SCHEDULED ENGINE CHANGE. ASSEMBLY WAS RECEIVED IN THE PROPELLER SHOP DUE TO BLADES BEING EXCESSIVELY LOOSE CAUSING AN IMBALANCE SITUATION. FOUND BEARING INSERT WORN IN AN OVAL FASHION, MEASURING FROM 0.0775 (WALL Mar 18, 1997 · N189CA · Emb EMB120RT · Propeller AssemblySDR COMA9710181Connector · brokenLANDING GEAR WOULD NOT RETRACT. REPLACED DEFECTIVE WIRING CONNECTOR AT RT MLG UPLOCK.Mar 17, 1997 · N255CA · Emb EMB120RT · Landing Gear Retraction/Extension SystemSDR ASOA97015Frame · corrodedDURING SCHEDULED MAINTENANCE, FOUND CORROSION ON FRAME 21 BETWEEN STRINGERS 20 LEFT AND 18 LEFT. REPAIRS MADE IAW THE SRM AND EO 120-53-0056. RII WAS COMPLETED SATISFACTORILY AND THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)Mar 17, 1997 · N281AS · Emb EMB120RT · Fuselage Main, FrameSDR WTAA970048Striker Plate · out of adjustSFO - CARGO DOOR LIGHT ON TAKEOFF ROLL. TAKEOFF ABORTED. MAINTENANCE DEFERRED CARGO DOOR LIGHT PER MEL 52-70-1. OPENED DMI 47777. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEANED DEFERRAL BY ADJUSTING CARGO DOOR AFT MICROSWITCH STRIKER PLATEMar 16, 1997 · N122AM · Emb EMB120RT · Door Warning SystemSDR WTAA970047Door · unlatchedSFO - LEFT ENGINE COWLING INSPECTION DOOR REPORTED OPEN AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE SECURED PANEL ON LEFT ENGINE INBOARD UPPER COWLING AFT OF PROPELLER. AIRCRAFT RETURNED TO SERVICE. (M)Mar 16, 1997 · N270YV · Emb EMB120RT · Engine Cowling SystemSDR COMA9710173Trim Tab Sensor · defectiveTAKEOFF TRIM AURAL WARNING SOUNDED DURING TAKEOFF. REPLACED THE ELEVATOR TRIM TAB PROXIMITY SENSOR.Mar 15, 1997 · N162CA · Emb EMB120RT · Elevator Tab Control SystemSDR WTAA970046Battery · dischargedSMX - EMERGENCY LIGHT AT ROW 4 FORWARD THROUGH GALLEY FAIL TO ILLUMINATE. MAINTENANCE DEFERRED EMERGENCY LIGHTING PER MEL 33-50-1. OPENED DMI 77715. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL BY REPLACING EMERGENCY LIGHT BATTERMar 14, 1997 · N284YV · Emb EMB120RT · Emergency Lighting
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