Embraer EMB-120RT

Service difficulty reports · 5,310

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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 GLBA96123Sequence Vlv · dirtyCIU - GEAR WILL NOT RETRACT. CLEANED RT FORWARD OUTBOARD GEAR DOOR SEQUENCE VALVE PLUNGER WHICH WAS STUCK. CYCLED GEAR SEVERAL TIMES. (M)Jun 23, 1996 · N267UE · Emb EMB120RT · Landing Gear Door Retract SectionSDR COMA9610203Hyd Hose · chafedLANDING GEAR FAILED TO EXTEND FOR LANDING. EMERGENCY EXTENSION PROCEDURES FAILED, AIRCRAFT MADE GEAR UP LANDING. INSPECTION REVEALED THE LEFT GREEN HYD SYSTEM RESERVOIR WAS EMPTY. FOUND LEFT ENGINE DRIVEN HYD PUMP PRESSURE HOSE CHAFED THROUGH CAUSING HYD FLJun 23, 1996 · N168CA · Emb EMB120RT · Hydraulic System, MainSDR COMA9610202Valve · failedEMERGENCY EXTENSION PROCEDURE FAILED, AIRCRAFT MADE GEAR UP LANDING. SUSPECT LANDING GEAR DOORS STAYED CLOSED RESTRICTING EXTENSION OF LANDING GEAR. REMOVED LANDING GEAR DOOR SOLENOID VALVE PER NTSB INVESTIGATOR.Jun 23, 1996 · N168CA · Emb EMB120RT · Landing Gear Door Retract SectionSDR COMA9610201Check Valve · failedTHE GREEN SYSTEM AUX HYD PUMP CYCLES ON AND OFF WITH MAIN PRESSUE AT 0 PSI. SUSPECT THE ENGINE PUMP CHECK VALVE TO BE AT FAULT LETTING AUX HYD PRESSURE TO REACH THE HIGH PRESSURE SWITCH CAUSING THE AUX HYD PUMP TO CYCLE ON AND OFF. THE RESERVIOR ASSY WHERE TJun 23, 1996 · N168CA · Emb EMB120RT · Hydraulic System, MainSDR ASOA96024Nozzle O-Ring · cutDURING CLIMB THROUGH 11,500 FEET, PNS-ATL, CREW GOT A FIRE BELL, LIGHT, AND T6 WARNING. THE CREW SHUT DOWN THE RIGHT ENGINE, FEATHERED THE PROP AND PULLED THE FIRE HANDLE. THE FIRE WARNING EXTINGUISHED AND THE CREW RETURNED TO PNS WHERE LANDING WAS MADE SAFEJun 23, 1996 · N503AS · Emb EMB120RT · Fuel Injector NozzleSDR COMA9610186Separator · crackedLT BLEED AIR DUCT LEAK WARNING CAME ON AFTER TAKEOFF. REPLACED THE LT BLEED AIR WATER SEPARATOR.Jun 22, 1996 · N254CA · Emb EMB120RT · Pneumatic Distribution SystemSDR COMA9610187Pcu · malfunctionLEFT ENGINE PROPELLER RPM WAS ONLY 98 PERCENT WHEN SET FOR MAX RPM. REPLACED THE LT PROPELLER CONTROL UNIT.Jun 21, 1996 · N249CA · Emb EMB120RT · Propeller Controlling SystemSDR ASOA96023Rccb · failedIN CRUISE FLIGHT OAJ-ATL, CREW ENCOUNTERED AN ELECTRICAL SMELL COMING FROM THE CIRCUIT RELAY CONSOLE ON THE FIRST OFFICERS SIDE. CREW COMPLIED WITH THE POH PROVISIONS AND DIVERTED INTO FLO. ATL MECHANIC ISOLATED THE PROBLEM TO THE RIGHT PROP HEAT RCCB AND DEJun 20, 1996 · N218AS · Emb EMB120RT · Propeller Controlling SystemSDR 96ZZZX5458Brush · excess wornBRUSHES FAILED PREMATURELY. BRUSHES WORN 85 PERCENT, BRUSH SHUNTS BROKEN OFF BRUSHES. BRUSHES BURNED, ARMATURE OVERHEATED, SUBMITTER STATED POOR DESIGN OF BRUSH. RECOMMENDED RE-DESIGN OF BRUSH.Jun 20, 1996 · N261CA · Emb EMB120RT · Starter-GeneratorSDR COMA9610185Hyd Pump · failedLEFT ENGINE DRIVEN HYDRAULIC PUMP FAILED. REPLACED HYDRAULIC PUMP.Jun 19, 1996 · N159A · Emb EMB120RT · Hydraulic Pump (Electric/Engine), MainSDR WTAA960131Skin · bird strikeFAT - CREW REPORTED, BIRD STRIKE BELOW CAPTAINS WINDOW. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M)Jun 18, 1996 · N120AM · Emb EMB120RT · Fuselage Main, Plate/SkinSDR COMA9610184Actuator · damagedTHE BLUE HYDRAULIC SYSTEM QUANTITY FELL TO ZERO DURING FLIGHT. THE RIGHT NACELLE FLAP ACTUATOR WAS THE CAUSE OF THE HYDRAULIC LEAK. TWO OF THE 4 NAS 1351-3H8P SCREWS THAT SECURE THE SOLENOID VALVE SHEARED ALLOWING THE ACTUATOR TO LEAK PROFUSELY. REPLACED ACJun 18, 1996 · N243CA · Emb EMB120RT · Trailing Edge Flap ActuatorSDR ASOA96022Skin · corrodedUPON INSPECTION, FOUND CORROSION ON FRAME 21 BETWEEN STRINGERS 21 RT TO 20 LT. REPAIR DETERMINDED TO BE A MAJOR REPAIR IAW SP663. REPAIRS WILL BE MADE IAW THE SRM AND EO 120-53-0044. (M)Jun 18, 1996 · N261AS · Emb EMB120RT · Fuselage Main, Plate/SkinSDR ASOA96021Skin · corrodedUPON INSPECTION, FOUND CORROSION ON FRAMES 21 AND 23 AT STRINGERS 21 RIGHT TO 20 LEFT. REPAIR DETERMINED TO BE A MAJOR REPAIR IAW SP663. REPAIRS MADE IAW THE SRM AND EO 120-53-0043. ALL WAS COMPLETED SATISFACTORILY AND THE AIRCRAFT WAS RELEASED FOR SERVICE.Jun 18, 1996 · N264AS · Emb EMB120RT · Fuselage Main, Plate/SkinSDR COMA9610183Connector · defectiveLEFT ENGINE LOW HYDRAULIC PRESSURE WARNING DURING CLIMB. REPAIRED WIRING CONNECTOR JO807 IN LT ENGINE NACELLE.Jun 17, 1996 · N159A · Emb EMB120RT · Hydraulic Pressure IndicatorSDR WTAA960130Oil Press Light · illuminatedSFO - LOW OIL PRESSURE LIGHT CAME ON DURING TAKEOFF. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE INSPECTED BOTH ENGINES FOR LEAKS AND CHAFED WIRES. NO DEFECTS NOTED. LOW OIL PRESSURE WARNING LIGHT SYSTEM OPERATIONAL CHECK NORMAL DURING ENGINE GROUND RUN.Jun 16, 1996 · N285UE · Emb EMB120RT · Engine Oil PressureSDR GLBA96118Connector · loose pinORD - GEAR HANDLE LOCK WOULD NOT RELEASE AFTER TAKEOFF FROM ORD. COULD NOT RAISE GEAR. FOUND CANNON PLUG ON LANDING GEAR RELAY BOX HAD A LOOSE PIN. SECURED PIN AND RETURNED TO SERVICE. (X)Jun 15, 1996 · N451UE · Emb EMB120RT · Landing Gear Retraction/Extension SystemSDR COMA9610216Floor Beam · corrodedDURING 2C INSPECTION, THE FLOOR BEAM NEXT TO THE ELEVATOR CONTROL COLUMN LEFT WAS FOUND WITH SURFACE CORROSION. CLEANED, TREATED AND PAINTED AREA PER M/M 51-21-04.Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA9610215Floor Beam · corrodedDURING 2C INSPECTION, THE FLOOR BEAM NEXT TO THE ELEVATOR CONTROL COLUMN RIGHT WAS FOUND WITH SURFACE CORROSION. CLEANED, TREATED AND PAINTED AREA PER M/M 51-21-04.Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA9610214Butt Strap · corrodedDURING 2C INSPECTION, SEVERAL RIVETS WERE FOUND LOOSE OR WITH CORROSION AT ENTRY FLOOR, LT BUTT STRAP. REMOVED AND REPLACED WITH ORIGINAL TYPE AND SIZE RIVETS, 19 TOTAL PER EMB 120 SRM CHAPTER 51.Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610213Cross Beam · corrodedDURING 2C INSPECTION, FOUND PASSENGER FLOOR SUPPORT CROSSBEAM T-SECTION CORRODED AT FUSELAGE FRAME 16. REMOVED CORRODED T-SECTION, LOCATED, DRILLED AND INSTALLED NEW PART PER EMB 120 SRM STANDARD PRACTICES.Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610212Support Section · corrodedDURING 2C INSPECTION, FOUND PASSENGER SEAT LEFT HAND SIDE WALL SEAT TRACK SUPPORT SECTION CORRODED ON SURFACE. CLEANED, TREATED, PAINTED CORRODED AREA PER EMB 120 M/M 51-21-04, OK FOR SERVICE.Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610211Support Section · corrodedDURING 2C INSPECTION, FOUND PASSENGER SEAT RIGHT HAND SIDE WALL SEAT TRACK SUPPORT SECTION CORRODED ON SURFACE. CLEANED, TREATED, PAINTED CORRODED AREA PER EMB 120 M/M 51-21-04, OK FOR SERVICE.Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610210Seat Track · corrodedDURING 2C INSPECTION, FOUND SEAT TRACKS FOR RIGHT HAND SIDE PASSENGERS SEATS TO BE CORRODED. REMOVED CORRODED SEAT TRACKS AND REPLACED WITH SERVICEABLE TRACKS.Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR COMA9610209Stringer · corrodedDURING 2C INSPECTION, FOUND STRINGERS IN LOWER FUSELAGE AREA BELOW LAV TO HAVE SURFACE CORROSION. CLEANED LIGHT CORROSION, TREATED AND PAINTED PER M/M 51-20-04.Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR COMA9610208Butt Strap · corrodedDURING 2C INSPECTION, FOUND BUTT STRAPS TO HAVE SURFACE CORROSION. CLEANED, TREATED AND PAINTED AREA PER EMB M/M 51-21-04.Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610207Bolt · rustedDURING 2C INSPECTION, FOUND FORWARD INBOARD CORNER OF BATTERY COMPARTMENT AT FRAME 4 TO HAVE SIGNS OF CORROSION. FURTHER INSPECTION FOUND NOSE GEAR FORWARD DOOR, AFT HINGE, HARDWARE TO BE CORRODED. REPLACED HARDWARE AND CLEANED BATTERY COMPARTMENT.Jun 15, 1996 · N130G · Emb EMB120RT · Battery Box StructureSDR COMA9610206Track · corrodedDURING 2C INSPECTION, FOUND GALLEY FLOOR ATTACHMENT TRACK TO BE CORRODED. REMOVED CORRODED TRACK AND REPLACED WITH A SERVICEABLE TRACK.Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR COMA9610205Floor Beam · corrodedDURING 2C INSPECTION, FOUND SURFACE CORROSION ON FLOOR BEAM THAT GALLEY FLOOR ATTACHMENT TRACK MOUNTS TO. REMOVED SURFACE CORROSION TREATED AREA AND PAINTED TO SERVICEABLE CONDITION.Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA9610204Seat Track · corrodedDURING 2C INSPECTION, FOUND SEAT TRACKS FOR LEFT HAND SIDE PASSENGER SEATS TO BE CORRODED. REMOVED CORRODED SEAT TRACKS AND REPLACED WITH SERVICEABLE TRACKS.Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR WTAA960129Windshield · birdstrikeSBA - CREW REPORTED, BIRD STRIKE ON CAPTAINS WINDSHIELD LOWER CENTER. MX ACCOMPLISHED BIRD STRIKE INSPECTION. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M)Jun 14, 1996 · N216YV · Emb EMB120RT · Flight Compartment WindowsSDR GLBA96135Drain Line · out of positionORD - RIGHT POWER LEVER HANGS UP DURING TAKEOFF. MAINTENANCE FOUND LOOSE DRAIN LINE CAUSING LINKAGE TO HANG-UP. SECURED LINE AND OPS GOOD. (M0Jun 14, 1996 · N267UE · Emb EMB120RT · Nacelle/Pylon StructureSDR GLBA96120Retract Mech · malfunctionedSPI - LANDING GEAR WOULD NOT RETRACT UNTIL TILLER WAS DEPRESSED AND RELEASED. MAINTENANCE COMPLETED SEVERAL GEAR SWINGS AND COULD NOT DUPLICATE. (M)Jun 14, 1996 · N451UE · Emb EMB120RT · Landing Gear Retraction/Extension SystemSDR COMA9610180Computer · defectiveCOPILOTS STICK SHAKER ACTIVATED DURING TAKEOFF ROLL. REPLACED THE STALL WARNING COMPUTER.Jun 14, 1996 · N1110J · Emb EMB120RT · Stall Warning SystemSDR COMA9610179Servo · defectiveWHEN AUTOPILOT DISENGAGED DURING APPROACH PHASE OF FLIGHT, THE RUDDER CONTROLS JAMMED AND EXCESSIVE FORCE WAS REQUIRED TO MOVE RUDDER CONTROLS. REPLACED DEFECTIVE RUDDER SERVO.Jun 14, 1996 · N179CA · Emb EMB120RT · Rudder Control SystemSDR COMA9610182Roller · wornFLAP DISAGREEMENT WARNING CAME ON DURING LANDING APPROACH. REPLACED THE RT INBD FLAP ROLLERS.Jun 13, 1996 · N189CA · Emb EMB120RT · Trailing Edge FlapsSDR COMA9610181Servo · malfunctionPILOTS STICK SHAKER IS ON CONTINUOUSLY. REPLACED THE PILOTS STICK SHAKER.Jun 13, 1996 · N164D · Emb EMB120RT · Stall Warning SystemSDR COMA9610230Ballscrew Servo · defectiveAD-94-22-12. WHILE PERFORMING HAMILTON STANDARD SB 14RF-9-61-A53 REV. S, FOUND THE SPLINES OF THE BALLSCREW SERVO WERE WORN BEYOND LIMITS PRIMARILY ON THE RIGHT SIDE OF THE SPLINES. ACTION TAKEN: SENT PCU OUT TO HAMILTON STANDARD FOR FURTHER EVALUATION.Jun 12, 1996 · N164D · Emb EMB120RT · Propeller Controlling SystemSDR COMA9610178Spline · defectiveWHILE PERFORMING AD-94-22-12 HAMILTON STANDARD S/B 14RF9-61-A53 REV S. FOUND THE SPLINES OF THE BALLSCREW SERVO WORN BEYOND LIMITS PRIMARILY ON THE RIGHT SIDE OF THE SPLINES. SENT PCU OUT TO HAMILTON STANDARD FOR FURTHER EVALUATION.Jun 12, 1996 · N164D · Emb EMB120RT · Propeller Controlling SystemSDR COMA9610175Prox Sensor · out of adjustTAKEOFF TRIM WARNING SOUNDED DURING TAKEOFF ROLL. ADJUSTED THE ELEVATOR TRIM TAB PROXIMITY SENSORS. ACFT RETURNED TO SERVICE.Jun 12, 1996 · N462CA · Emb EMB120RT · Central WarningSDR C2XA96IA152Light · inoperativeCLE - DURING A ROUTINE CHECK OF EMERGENCY LIGHTING SYSTEM, LEFT AFT EXTERIOR EMERGENCY LIGHT FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED LIGHT ASSEMBLY, OPERATIONAL CHECKED GOOD, AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)Jun 12, 1996 · N12703 · Emb EMB120RT · Emergency LightingSDR ASOA96019Stringer · crackedDURING INSPECTION, FOUND THE LEFT WING NR 10 STRINGER INBOARD OF NACELLE AND RIGHT WING STRINGER NR 8 INBOARD OF NACELLE CRACKED. DETERMINED TO BE A MAJOR REPAIR IAW SP663 AND FAR 43 APPENDIX A. REPAIRS WILL BE MADE IAW SRM 57-20-03, FIGURE 201. (M)Jun 12, 1996 · N227AS · Emb EMB120RT · Wing, Longeron/StringerSDR 96ZZZM1047Stringer · crackedDURING INSPECTION, FOUND THE LEFT WING NR 10 STRINGER INBOARD OF NACELLE AND RIGHT WING STRINGER NR 8 INBOARD OF NACELLE CRACKED. DETERMINED TO BE A MAJOR REPAIR IAW SP663 AND FAR 43 APPENDIX A. REPAIRS WILL BE MADE IAW SRM 57-20-03, FIGURE 201. REFERENCE AJun 12, 1996 · N227AS · Emb EMB120RT · Wing, Longeron/StringerSDR WTAA960127Bulbs · failedPSP - RIGHT MAIN LANDING GEAR INDICATOR 'A' AND 'B' SYSTEM FAILED DURING APPROACH. CREW DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED 4 BULBS IN RIGHT MAIN LANDING GEAR INDICATOR. BOTH 'A' AND 'B' SYSTEM INDICATION NORMAL DURING GROUND CJun 11, 1996 · N250YV · Emb EMB120RT · Landing Gear Position and WarningSDR COMA9610177Bolt · brokenON PREFLIGHT INSPECTION, MECHANIC NOTICED TWO BOLTS MISSING FROM THE RIGHT MAIN INBOARD WHEEL ASSEMBLY. BOLTS ARE PRESUMED TO HAVE BROKEN AND FALLEN OUT. WHEEL/TIRE ASSEMBLY WAS REMOVED AND REPLACED.Jun 11, 1996 · N130G · Emb EMB120RT · Wheel/Ski/FloatSDR COMA9610176Wow Sensor · failedLANDING GEAR HANDLE COULD NOT BE SELECTED TO UP POSITION. REPLACED THE RT MLG, WEIGHT ON WHEELS PROXIMITY SENSOR.Jun 11, 1996 · N159A · Emb EMB120RT · Landing Gear Position and WarningSDR ASOA96020Hyd Pump · defectiveAT APPROXIMATELY 16,000 FEET ON CLIMB-OUT GSO-ATL, SIMULTANEOUS 'LOW LEVEL' AND 'MAIN PUMP LOW PRESSURE' LIGHTS ILLUMINATED ON HYDRAULIC PANEL AND 'HYD' LIGHT ON MAP. CREW DECLARED AN EMERGENCY AND LANDED SAFELY WITH ZERO FLAPS IN ATL. REMOVED AND REPLACED RJun 11, 1996 · N243AS · Emb EMB120RT · Hydraulic Pump (Electric/Engine), MainSDR WTAA960124Fuel Filter Ind · illuminatedSBA - RT ENGINE FUEL FILTER LIGHT ILLUMINATED ON TAKEOFF. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE REMOVED AND INSPECTED RIGHT ENGINE HIGH PRESSURE FUEL FILTER. FUEL FILTER LIGHT INDICATED NORMAL DURING ENGINE GROUND RUN. AIRCRAFT RETURNED TO SERVICE.Jun 9, 1996 · N250YV · Emb EMB120RT · Fuel Flow IndicatingSDR COMA9610174Flap Selector · malfunctionFLAP CONTROL FAULT WARNING ON CWP. REPLACED FLAP SELECTOR CONTROL.Jun 9, 1996 · N189CA · Emb EMB120RT · Trailing Edge Flap Control SystemSDR COMA9610173Solenoid · failedPOWER LEVER, FLIGHT IDLE STOP, CIRCUIT BREAKERS WERE TRIPPED. REPLACED THE RT POWER LEVER FLIGHT IDLE STOP SOLENOID, RESET LT BREAKER.Jun 9, 1996 · N267CA · Emb EMB120RT · Power Lever
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