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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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)SDR 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 FLSDR 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.SDR 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 TSDR 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 SAFESDR COMA9610186Separator · crackedLT BLEED AIR DUCT LEAK WARNING CAME ON AFTER TAKEOFF. REPLACED THE LT BLEED AIR WATER SEPARATOR.SDR COMA9610187Pcu · malfunctionLEFT ENGINE PROPELLER RPM WAS ONLY 98 PERCENT WHEN SET FOR MAX RPM. REPLACED THE LT PROPELLER CONTROL UNIT.SDR 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 DESDR 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.SDR COMA9610185Hyd Pump · failedLEFT ENGINE DRIVEN HYDRAULIC PUMP FAILED. REPLACED HYDRAULIC PUMP.SDR WTAA960131Skin · bird strikeFAT - CREW REPORTED, BIRD STRIKE BELOW CAPTAINS WINDOW. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M)SDR 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 ACSDR 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)SDR 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.SDR COMA9610183Connector · defectiveLEFT ENGINE LOW HYDRAULIC PRESSURE WARNING DURING CLIMB. REPAIRED WIRING CONNECTOR JO807 IN LT ENGINE NACELLE.SDR 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.SDR 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)SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR COMA9610208Butt Strap · corrodedDURING 2C INSPECTION, FOUND BUTT STRAPS TO HAVE SURFACE CORROSION. CLEANED, TREATED AND PAINTED AREA PER EMB M/M 51-21-04.SDR 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.SDR COMA9610206Track · corrodedDURING 2C INSPECTION, FOUND GALLEY FLOOR ATTACHMENT TRACK TO BE CORRODED. REMOVED CORRODED TRACK AND REPLACED WITH A SERVICEABLE TRACK.SDR 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.SDR 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.SDR WTAA960129Windshield · birdstrikeSBA - CREW REPORTED, BIRD STRIKE ON CAPTAINS WINDSHIELD LOWER CENTER. MX ACCOMPLISHED BIRD STRIKE INSPECTION. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M)SDR 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. (M0SDR GLBA96120Retract Mech · malfunctionedSPI - LANDING GEAR WOULD NOT RETRACT UNTIL TILLER WAS DEPRESSED AND RELEASED. MAINTENANCE COMPLETED SEVERAL GEAR SWINGS AND COULD NOT DUPLICATE. (M)SDR COMA9610180Computer · defectiveCOPILOTS STICK SHAKER ACTIVATED DURING TAKEOFF ROLL. REPLACED THE STALL WARNING COMPUTER.SDR 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.SDR COMA9610182Roller · wornFLAP DISAGREEMENT WARNING CAME ON DURING LANDING APPROACH. REPLACED THE RT INBD FLAP ROLLERS.SDR COMA9610181Servo · malfunctionPILOTS STICK SHAKER IS ON CONTINUOUSLY. REPLACED THE PILOTS STICK SHAKER.SDR 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.SDR 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.SDR COMA9610175Prox Sensor · out of adjustTAKEOFF TRIM WARNING SOUNDED DURING TAKEOFF ROLL. ADJUSTED THE ELEVATOR TRIM TAB PROXIMITY SENSORS. ACFT RETURNED TO SERVICE.SDR 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)SDR 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)SDR 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 ASDR 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 CSDR 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.SDR COMA9610176Wow Sensor · failedLANDING GEAR HANDLE COULD NOT BE SELECTED TO UP POSITION. REPLACED THE RT MLG, WEIGHT ON WHEELS PROXIMITY SENSOR.SDR 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 RSDR 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.SDR COMA9610174Flap Selector · malfunctionFLAP CONTROL FAULT WARNING ON CWP. REPLACED FLAP SELECTOR CONTROL.SDR COMA9610173Solenoid · failedPOWER LEVER, FLIGHT IDLE STOP, CIRCUIT BREAKERS WERE TRIPPED. REPLACED THE RT POWER LEVER FLIGHT IDLE STOP SOLENOID, RESET LT BREAKER.
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