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 COMA9610319Latch · failedON POST FLIGHT, FOUND RT O/B FWD GEAR DOOR HANGING DOWN. REPLACED RT O/B DOOR LATCH.Oct 31, 1996 · N268CA · Emb EMB120RT · Landing Gear Door Retract SectionSDR COMA9610318Indication · malfunctionedFLAP DISAGREEMENT AFTER TAKEOFF. INSPECTED FLAPS, NO DEFECTS NOTED.Oct 31, 1996 · N462CA · Emb EMB120RT · Trailing Flap Position Indicating SystemSDR COMA9610315Roller · wornFLAP DISAGREEMENT WARNING WHEN FLAPS RETRACTED. REPLACED THE RT OUTBOARD FLAP ROLLERS.Oct 29, 1996 · N156CA · Emb EMB120RT · Trailing Edge FlapsSDR COMA9610313Battery · dischargedSEVERAL EMERGENCY LIGHTS ARE DIM OR INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY.Oct 29, 1996 · N259CA · Emb EMB120RT · Emergency LightingSDR COMA9610317Stringer · corrodedC2 INSPECTION FOUND A SMALL AREA OF CORROSION ON FWD FUSELAGE STRINGER 21L BETWEEN FS 3293 AND 3596.5. THE DAMAGED AREA OF THE STRINGER WAS REMOVED AND REPAIRED PER AERODESIGN REPORT NR 1990-3, REV IR, DATED 10-26-96.Oct 28, 1996 · N256CA · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR COMA9610316Skin · gougedC2 INSPECTION FOUND THE LOWER FUSELAGE CENTER SECTION SKIN TO BE GOUGED BY THE RIGHT WING DE-ICE PRESSURE REGULATOR. THE DAMAGED SKIN WAS REPAIRED PER SRM 53-00-01, FIGURE 201, SHEET 3, PAGE 204. THE DE-ICE PRESSURE REGULATOR WAS REPOSITIONED FOR PROPER CLEAOct 28, 1996 · N256CA · Emb EMB120RT · Fuselage Main, Plate/SkinSDR COMA9610314Ahc 85 · failedCOPILOT'S AHRS FAILED. REPLACED THE AHC-85.Oct 28, 1996 · N179CA · Emb EMB120RT · Integrated Flight SystemSDR C2XA96CL035Eec · failedCLE - FLT 3003 - CREW REPORTED THAT AT 17,500 FEET THEY COULD NOT GET MORE THAN 4 PERCENT TORQUE AND 700 DEGREES EGT WITH POWER LEVER FULL FORWARD. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE NR 1 ENGINE ELECTRONICOct 26, 1996 · N12709 · Emb EMB120RT · Fuel Control/Turbine EnginesSDR COMA9610310Auto Pilot · malfunctionedDURING AUTO PILOT TEST THE ELEVATOR TRIM RUNS WILD. AUTO PILOT SYSTEM PLACED ON DEFERRED MAINTENANCE LIST.Oct 25, 1996 · N1110J · Emb EMB120RT · Autopilot SystemSDR GLBA96207Panel · leakingDEN - FUEL LEAK AT LEFT INBOARD WING DEFUEL PANEL. MAINTENANCE SECURED SCREWS ON PANEL. (M)Oct 23, 1996 · N281UE · Emb EMB120RT · Wing, Plate/SkinSDR COMA9610312Atuator · malfunctionFLAP DISAGREEMENT WARNING DURING LANDING APPROACH. REPLACED THE RT FLAP OUTBD ACTUATOR.Oct 23, 1996 · N179CA · Emb EMB120RT · Trailing Edge Flap ActuatorSDR COMA9610311Battery · dischargedAFT EMERGENCY LIGHTS ARE INOP. REPLACED EMERGENCY BATTERY.Oct 23, 1996 · N263CA · Emb EMB120RT · Emergency LightingSDR C2XA96IA270Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT SIDE 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)Oct 21, 1996 · N16731 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA96IA269Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, FOUND THE RIGHT SIDEWALL 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)Oct 21, 1996 · N16731 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA96IA268Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT FLOOR AFT 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)Oct 21, 1996 · N16731 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA96IA267Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT FLOOR FORWARD 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)Oct 21, 1996 · N16731 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA96IA266Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT AFT FLOOR 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)Oct 21, 1996 · N16731 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA96IA265Seat Track · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT FLOOR FORWARD 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)Oct 21, 1996 · N16731 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA96IA264Floor Beam · crackedIAH - DURING C-CHECK INSPECTION, THE FLOOR SUPPORT AT FRAME 16 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACD THE AFFECTED FLOOR BEAM AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Oct 21, 1996 · N16731 · Emb EMB120RT · Fuselage Main, Floor BeamSDR C2XA96IA263Buttstrap · corrodedIAH - DURING C-CHECK INSPECTION, THE CENTER BUTTSTRAP FROM FRAME 35 TO 44 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Oct 21, 1996 · N16731 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA96IA262Buttstrap · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT BUTTSTRAP FROM FRAME 33 TO 44 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Oct 21, 1996 · N16731 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA96IA261Floor Beam · corrodedIAH - DURING C-CHECK INSPECTION, THE FLOOR SUPPORT FROM FRAME 39 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)Oct 21, 1996 · N16731 · Emb EMB120RT · Fuselage Main, Floor BeamSDR C2XA96IA260T-Profile · corrodedIAH - DURING C-CHECK INSPECTION, THE T-PROFILE FROM FRAME 36 TO 38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-PROFILE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Oct 21, 1996 · N16731 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710433Lamp · failedTHE AFT LAMP OF THE CABIN FLOOR PATH EMERGENCY LIGHTING IS INOP. REPLACED LAMP.Oct 20, 1996 · N263CA · Emb EMB120RT · Emergency LightingSDR ASOA96047Connector · dirtyIN BOUND TRI-ATL, CREW EXPERIENCED A FLAP CONTROL FAULT. SYSTEM WAS RESET PER THE POH AND APPROXIMATELY 5 MINUTES LATER, THE FAULT LIGHT ILLUMINATED AGAIN. THE CREW CHOSE TO DECLARE AN EMERGENCY AND LANDED ZERO FLAPS IN ATL. LANDING WAS MADE SAFELY AND WITHOct 19, 1996 · N237AS · Emb EMB120RT · Trailing Edge Flap ActuatorSDR COMA9610308Wire · chafedLT BLEED AIR DUCT LEAK WARNING CAME ON DURING CLIMB. REPAIRED CHAFED WIRING AT DUCT LEAK SENSOR.Oct 18, 1996 · N200CD · Emb EMB120RT · Pneumatic System WiringSDR WTAA960180Door · not closedFAT - OUTBOARD FUEL DOOR OPENED DURING TAKEOFF. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND SECURED FUEL DOOR. AIRCRAFT RETURNED TO SERVICE. (M)Oct 17, 1996 · N284UE · Emb EMB120RT · Fluid Service DoorsSDR COMA9610309Flap Contl Unit · malfunctionFLAP CONTROL FAULT WARNING, INBD FLAPS ARE FAILED. REPLACED THE FLAP CONTROL UNIT.Oct 17, 1996 · N152CA · Emb EMB120RT · Trailing Edge Flap Control SystemSDR ASOA96046Oil Pump · faliedAPPROXIMATELY 60 MILES OUT ON APPROACH ICT-DFW, RIGHT NP BEGAN FLUCTUATING FROM 83 PECENT TO 87 PERCENT. ATTEMPTED 100 PERCENT NP, AND NP ROSE TO 101.5 PERCENT. CAPTAIN BROUGHT THE POWER LEVER BACK TO CONTROL THE NP, FLUCTUATION CONTINUED (WENT TO 105 PERCEOct 16, 1996 · N130AM · Emb EMB120RT · Propeller Controlling SystemSDR COMA9610307Flap · chafingNACELLE FLAP DISAGREEMENT WARNING WHEN FLAPS LOWERED. FOUND RT NACELLE FLAP CHAFING AT THE OUTBD HINGE. REPLACED FLAP.Oct 15, 1996 · N1105G · Emb EMB120RT · Leading Edge DevicesSDR COMA9610306Flap Selector · malfunctionFLAP CONTROL FAULT WARNING. REPLACED THE FLAP SELECTOR UNIT.Oct 15, 1996 · N152CA · Emb EMB120RT · Trailing Edge Flap Control SystemSDR COMA9610304Latch · brokenLT MLG FORWARD DOOR LATCH IS BROKEN, DOOR HANGS OPEN. REPLACED THE DOOR LATCH ASSY.Oct 12, 1996 · N161CA · Emb EMB120RT · Landing Gear Door Retract SectionSDR COMA9610303Actuator · malfunctionedAFTER LANDING, WHEN FLAPS SELECTED UP, THE LT INBD FLAP INDICATED 15 DEGREES AND THE RT INBD FLAP INDICATED 45 DEGREES. COULD NOT DUPLICATE DISCREPANCY. REPLACED THE RT INBD FLAP ACTUATOR FOR TROUBLESHOOTING.Oct 12, 1996 · N179CA · Emb EMB120RT · Trailing Edge Flap ActuatorSDR GLBA96198Actuator · out of adjustORD - LEFT MAIN LANDING GEAR WILL NOT RETRACT. BOTH A AND B RED LIGHTS REMAIN ON AFTER GEAR SELECTED UP. MAINTENANCE ADJUSTED LEFT AND RIGHT MLG ACTUATORS AND UPLOCK INDICATOR SWITCHES. TEST FLIGHT SATISFACTORY. (M)Oct 11, 1996 · N128AM · Emb EMB120RT · Landing Gear Retraction/Extension SystemSDR COMA9610302Indication · malfunctionedAFTER TOUCHDOWN, FLAP ASYMMETRY WARING. FLAP WERE SET AT 45 DEGREES, LEFT INBD FLAP INDICATED 25 DEGREES. COULD NOT DUPLICATE DISCREPANCY, OPERATIONAL CHECK OF FLAP SYSTEM NORMAL.Oct 11, 1996 · N179CA · Emb EMB120RT · Trailing Flap Position Indicating SystemSDR GLBA96206Engine · failedDLH - LOST NR 1 ENGINE SHORTLY AFTER TAKEOFF. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE. OPERATIONAL AND PERFORMANCE CHECKS GOOD. (M)Oct 10, 1996 · N451UE · Emb EMB120RT · Engine (Turbine/Turboprop)SDR 96ZZZX5316Bearing Race · crackedCRACK INDICATION IN BLADE FILLET AND BUTT AREA OF SHANK ON BOTH SIDES OF GOUGE LINE IN FILLET AREA FROM EDGE OF SPLIT RACES.Oct 10, 1996 · N503AS · Emb EMB120RT · Propeller Blade SectionSDR COMA9610305Steering · failedNOSE WHEEL STEERING FAILED. AIRCRAFT DEPARTED RUNWAY. COULD NOT DUPLICATE DISCREPANCY. WEIGHT ON WHEELS PROXIMITY SENSORS WERE REPLACED FOR TROUBLESHOOTING. AIRCRAFT FLIGHT CHECK SATISFACTORY.Oct 9, 1996 · N254CA · Emb EMB120RT · Landing Gear Steering SystemSDR COMA9610301T Section · corrodedFOUND FUSELAGE FLOOR SUPPORT STRUCTURE T-SECTION CORRODED IN FWD CABIN AREA. REMOVED CORRODED T-SECTION AND INSTALLED NEW PART PER REPORT NR 2057-1, REV. IR, DATED 10-6-96. AIRCRAFT TOTAL CYCLES, 19,871.Oct 9, 1996 · N152CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610300Butt Strap · corrodedFOUND FUSELAGE FLOOR SUPPORT STRUCTURE FORWARD LT BUTT STRAP CORRODED. REMOVED CORRODED BUTT STRAP AND INSTALLED NEW PART PER EMB120 SRM STANDARD PRACTICES, CH 51-40-02. AIRCRAFT TOTAL CYCLES, 19,871.Oct 9, 1996 · N152CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610299Butt Strap · corrodedFOUND FUSELAGE FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP CORRODED. REMOVED CORRODED BUTT STRAP AND INSTALLED NEW PART PER REPORT NR 1671-1, REV. IR, DATED 10-22-95. AIRCRAFT TOTAL CYCLES, 19,871.Oct 9, 1996 · N162CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR WTAA960177Relay Box · failedSFO - LEFT MAIN GEAR WARNING ON CLIMB-OUT. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE REPLACED LANDING GEAR RELAY BOX. GEAR RETRACTION SYSTEM OPERATIONAL CHECK NORMAL. TEST FLIGHT SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M)Oct 8, 1996 · N122AM · Emb EMB120RT · Landing Gear Position and WarningSDR COMA9610298Sign · missingEMERGENCY EXIT SIGN AT ROW 5 IS MISSING. REPLACED EMERGENCY EXIT SIGN.Oct 8, 1996 · N205CA · Emb EMB120RT · Emergency LightingSDR COMA9610296Switch · failedPILOTS PEDAL STEER DISCONNECT SWITCH IS INOP. REPLACED SWITCH.Oct 7, 1996 · N263CA · Emb EMB120RT · Landing Gear Steering SystemSDR COMA9610295Actuator · leakingRT ENGINE NACELLE, WING AND PROPELLER ARE COVERED WITH OIL. REPLACED THE PROPELLER ACTUATOR ASSY.Oct 7, 1996 · N161CA · Emb EMB120RT · Propeller Controlling SystemSDR ASOA96045Hyd Line · rupturedWHILE COMPLETING THE TAKEOFF CHECKLIST DFW-ILE, THE CAPTAIN NOTICED THE LEFT HYDRAULIC PRESSURE GAUGE WAS INDICATING 1500 LBS. THE ELECTRIC PUMP WAS TURNED ON AND THE PRESSURE RETURNED TO NORMAL. A FEW MINUTES LATER THE PRESSURE DROPPED TO ZERO AND THE CREW Oct 6, 1996 · N237AS · Emb EMB120RT · Hydraulic System, MainSDR COMA9610297Valve · defectiveAFTER TAKEOFF, THERE WAS A 1,500 LB FUEL IMBALANCE. AIRCRAFT RETURNED TO FIELD. REPLACED DEFECTIVE RIGHT WING FUEL PILOT VALVE.Oct 5, 1996 · N248CA · Emb EMB120RT · Aircraft Fuel Distribution SystemSDR COMA9610294Relay Box · malfunctionLANDING GEAR RETRACTED NORMALLY AND INDICATED UP, BUT THE LANDING GEAR AURAL WARNING SOUNDED CONTINUOUSLY. REPLACED THE LANDING GEAR RELAY BOX.Oct 4, 1996 · N266CA · Emb EMB120RT · Landing Gear Position and WarningSDR C2XA96IA253Angle · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT NACELLE FRAME 2 ATTACH ANGLE WAS FOUND TO BE CRACKED. MX REMOVED AND REPLACED THE ANGLE AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Oct 2, 1996 · N12705 · Emb EMB120RT · Nacelle/Pylon StructureSDR C2XA96IA252Angle · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT NACELLE FRAME 2 ATTACH ANGLE WAS FOUND TO BE CRACKED. MX REMOVED AND REPLACED THE FRAME AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Oct 2, 1996 · N12705 · Emb EMB120RT · Nacelle/Pylon Structure
Back to Embraer EMB-120RT