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 SWIA200110197Control Arm · malfunctionedNOSE WHEEL STEERING PULLS LEFT WITH OR WITHOUT TILLER ENGAGED. ABORTED TAKEOFF BELOW 80 KNOTS. CENTERED FEEDBACK POT AND REPLACED NOSE WHEEL STEERING TILLER. OPS CHECK GOOD ON TAXI.SDR SWIA200110178Control Unit · malfunctionedTAXI OUT RECEIVED FLAP CONTROL FAULT ANNUNCIATION ON OUTBOARD PAIR, ONE ROW OF LIGHTS. RETURNED TO GATE.REPLACED FLAP CONTROL UNIT. OPS CHECK GOOD.S/N ON: 0016 S/N OFF: 156SDR SWIA200110179Engine · malfunctionedLEFT ENGINE LOST POWER INFLIGHT, PRECAUTIONARY ENGINE SHUT DOWN CHECK COMPLETED.REMOVED AND REPLACED LEFT ENGINE ASSY WITH SERVICEABLE UNIT. COMPLIED WITH ALL ITEMS ON ENGINE INSTALLATION CARD. NO DEFECTS NOTED. OPS CHECKS GOOD ON ENGINE RUNSPN ON: PW118 SN SDR SWIA200110159Uplock Sensor · dirtyRIGHT 'A' RED GEAR LIGHT DID NOT EXTINGUISH AFTER TAKEOFF. ALL GEAR DOORS REMAINED OPEN WITH GEAR SELECTED IN UP POSITION. CYCLED AS PER QRH.CLEANED AND INSPECTED RIGHT MAIN UPLOCK SENSORS AND SWUNG GEAR 20+ TIMES. NO FAULTS FOUND.SDR SWIA200110248Angle · crackedCRACK AND PULLED RIVET IN VERTICAL STABILIZER TO EMPENNAGE SUPPORT ANGLE LEFT SIDE. REPLACED LEFT L-FORWARD PROFILE PER PART II OF SB 120-053-0074 AND EMBRAER AUTHORIZATION GST-3216/01. P/N: SB120-53-0074 KIT 1.SDR SWIA200110247Shear Tie · crackedFORMER CRACKED JUST AFT OF PILOT'S DIRECT VISION WINDOW AFT CENTER. REMOVED AND REPLACED CRACKED BRACKET WITH NEW SERVICEABLE BRACKET OF SAME P/N FOR THIS LOCATION. ALL WORK PERFORMED IN ACCORDANCE WITH THE SRM 51-70-00. ALL CHECKS GOOD. P/N: 120-12545-00SDR COMA0110141Computer · faultyFLIGHT #5027. DURING CLIMB-OUT OF MCO RECEIVED HEADING AND PITCH CAPTIONS, RE-SETTING THE HEADING MONITOR CLEARED THE PITCH CAPTION, BUT HEADING CAPTION REMAINED.REPLACED THE AHC-85.SDR SWIA200110148Selector Switch · malfunctionedON TAXI CHECK, WHEN FLAPS 15 DEGREES WERE SELECTED THE MAP LIGHT ''FLAPS'' AND ''ADV SWS'' ILLUMINATED WITH AN ASSOCIATED CONTROL FAULT ON FLAP WARNING PANEL WITH FLASHING NACELLE BARS.RESET FLAP SYSTEM. RE-RACKED FCU. REPLACED FLAP SELECTOR. OPERATED FLAP SDR COMA0110140Skin · dentedCREW REPORTS DENT ON RIGHT SIDE OF FUSELAGE BETWEEN FRAME 18 AND FRAME 19 AFTER DEBRIS STRUCK RIGHT PROPELLER.DAMAGED AREA WAS CUT OUT. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED. WORK DONE IN ACCORDANCE WITH EMBRAER STRUCTURES REPAIR MANUAL CHAPTER 53-0SDR ASOA01153SServo · wornFLT 4810 - DURING FLIGHT, REPORTED THAT THE A/C WAS HARD TO CONTROL. WHEN THE AUTOPILOT WAS DISCONNECTED, THE ELEV AND RUDDER WERE HEAVY AS IF THEY WERE STILL CONNECTED TO THE AUTOPILOT. PULLED THE AUTOPILOT CIRCUIT BREAKERS, BUT THIS DIDN`T FIX THE PROBLEM. DSDR COMA0110137Computer · faultyFLIGHT #5005. DURING TAXI OUT RECEIVED A HEADING COMPUTER WARNING, AIRCRAFT RETURNED TO THE GATE.REPLACED THE AHC-85.SDR SWIA200110134Flap Track · dirtyON APPROACH TO OXR, HAD FLAP DISAGREEMENT (INBOARD FLAPS TWO BARS). RETURNED TO LAX.CLEANED FLAP TRACKS. CYCLED FLAPS, COULD NOT DUPLICATE.SDR COMA0110139Indicator · faultyFLIGHT #5053. DURING APPLICATION OF POWER FOR TAKE OFF AT MCO THE #2 NH ANALOG INDICATION FAILED, AIRCRAFT RETURNED TO THE GATE.REPLACED THE NH/NL INDICATOR.SDR COMA0110136Indicator · faultyFLIGHT #5053. DURING APPLICATION OF POWER FOR TAKE OFF AT MCO THE #2 NH ANALOG INDICATION FAILED, AIRCRAFT RETURNED TO THE GATE.REPLACED THE NH/NL INDICATOR.SDR SWIA200110125Annunciator · malfunctionedFLAPS SET 45 DEGREES ON FINAL, CONTINUITY FAULT ILLUMINATED FOR OUTBOARD PAIR OF FLAPS.REPLACED ANNUNCIATOR/I WITH VERSION II PER MM 27-50-00. OPS CHECK OK ON GROUND TESTS.SDR SWIA200110129Switch · malfunctionedFORWARD DOOR ACTUATOR LT ON IN FLIGHT. LIGHT EXTINGUISHES ON THE GROUND. COULD NOT GET MAIN CABIN DOOR OPEN NORMALLY ON GROUND. USED EMERGENCY OVERRIDE. REMOVED AND REPLACED PASSENGER DOOR SWITCH AT FLIGHT ATTENDANT'S STATION. SYSTEM OPS CHECK GOOD.SDR SWIA200110137Connector · malfunctionedON DESCENT WITH A/P SELECTED TO FIRST OFFICER AND ENGAGED, AIRCRAFT PITCHED OVER. NO AURAL WARNING, NO LIGHTS ON MAP. NOTED CAPTAIN'S RMI FLAGGED AT THE TIME OF HARD OVER. REMOVED AND REPLACED NR 2 DPU CONNECTOR V1 AND V2. DPU SYSTEM OPS CHECK GOOD IAW MM SDR SWIA200110121Selector Switch · malfunctionedFLAP CONTROL FAULT DURING FLAP RETRACTION AND AGAIN WHEN SETTING FLAPS TO 25 DEGREES FOR LANDING. ALL LIGHT BARS FLASHING. QRH RESET PROCEDURE WORKED BOTH TIMES.REMOVED AND REPLACED FLAP SELECTOR IAW MM 27-51-00. OPS CHECK GOOD ON GROUND.SDR SWIA200110119Seal · leakingON DEPARTURE FA REPORTED A LOUD SQUEAL COMING FROM FLOOR LEVEL EXIT AT ROW 9.REPAIRED EMERGENCY EXIT DOOR SEAL AS REQUIRED. PRESSURIZATION CHECK TO 4 PSI. ALL CHECKS GOOD.SDR SWIA200110167Frame · crackedLEFT NACELLE FRAME 1 CRACKED AT INBOARD TORSION MOUNT.REPLACED LEFT NACELLE FRAME 1 IAW SB120-54-0036 PART 2.SDR SWIA200110166Frame · crackedRIGHT NACELLE FRAME 1 CRACKED AT OUTBOARD TORSION MOUNT.REPLACED RIGHT NACELLE FRAME 1 IAW SB120-54-0036 PART 2.SDR SWIA200110165Stringer · crackedCRACKED LOWER STRINGER IN FUEL BAY LEFT WING AT NR 2 FUEL ACCESS PANEL BAY FWD.REPAIRED IAW EMB120 SRM 57-20-03.SDR SWIA200110164Stringer · crackedCRACKED LOWER STRINGER IN FUEL BAY LEFT WING AT NR 2 FUEL ACCESS PANEL BAY AFT.REPAIRED IAW EMB120 SRM 57-20-03.SDR SWIA200110163Stringer · crackedRIGHT MOST INBOARD FUEL PANEL FORWARD STRINGER CRACKED. REPAIRED IAW EMB120 SRM 57-20-03 AS OUTLINED.SDR SWIA200110162Bearing · corrodedRIGHT NACELLE FLAP HINGE BEARINGS 2 EA. CORRODED AND WORN.REPLACED NACELLE FLAP WITH SERVICEABLE FLAP ASSEMBLY AS NEEDED.P/N: 120-40327-002 S/N OFF: 120212SDR SWIA200110161Swivel · corrodedNOSE GEAR AFT DOORS RODS AND SWIVELS WORN AND CORRODED.REMOVED AND REPLACED NOSE LANDING GEAR AFT DOORS RODS AND SWIVELS WITH SERVICEABLE PARTS AS REQUIRED.SDR SWIA200110106Actuator · erraticRT NACELLE FLAP POT IS ERRATIC.REMOVED AND REPLACED RIGHT NACELLE FLAP ACTUATOR. OPS CHECKS GOOD IAW MM 27-50-08.SDR SWIA200110108Computer · malfunctionedUNCOMMANDED PITCH UP WITH AP ENGAGED, AP DISCONNECTED. PERFORMED QRH, RE-ENGAGED AP, AND EXPERIENCED UNCOMMANDED PTICH ROLL. AP DEFERRED ON FO SIDE. MEL 22-11-1 REPLACED NR 2 AUTOPILOT COMPUTER IAW MM 22-10-00. OPS CHECK GOOD.SDR SWIA200110099Circuit Breaker · trippedON APPROACH TO PDX, EMERGENCY DC BUS 2 FAILED WHEN FLAPS WERE SELECTED 15 DEGREES.REMOVED AND REPLACED EMERGENCY DC BUS 2 CIRCUIT BREAKER IAW WM 20-00-07. NO DEFECTS NOTED.SDR SWIA200110098Buss · failedON APPROACH TO SEA THE ''EMERGENCY BUS OFF" LIGHT ON OVERHEAD PANEL LIGHT CAME ON, AND ON THE MAP PANEL THE AMBER APU, ELECTRIC, POWER OFF, DEICE AND BRAKES LIGHTS CAME ON. FOLLOWED QRH PROCEDURE TO AFM 3-8 PROCEDURE - EMERGENCY DC BUS FAILED.RESET EMERGENCY SDR SWIA200110120Annunciator · malfunctionedRECEIVED FLAP CONTROL FAULT WARNING WHEN SELECTING FLAPS TO 15 DEGREES. RESET WAS SUCCESSFUL AFTER PRESSING RESET TWICE.REPLACED FLAP ANNUNCIATOR IAW MM 27-50-05. OPS CHECK GOOD.SDR COMA0110134Computer · malfunctionedDURING LANDING APPROACH INTO MCO WHEN FLAPS WERE SELECTED FROM 25 TO 45 DEGREES AUDIBLE FLAP CAUTION ACTIVATED, CREW DECLARED AN EMERGENCY AND LANDED SAFELY. INTERROGATED THE FLAP COMPUTER AND FOUND NUMEROUS FAULT CODES. CLEARED FAULT CODES, PERFORMED OPERATSDR COMA0110133Flap TrackDURING LANDING APPROACH INTO EYW WHEN FLAPS WERE SELECTED FROM 25 TO 45 DEGREES, FLAP DISAGREE CAUTION ACTIVATED.REPLACED THE FLAP ROLLERS FOR THE LEFT INBOARD FLAP AND THE RIGHT OUTBOARD FLAP.SDR COMA0110135Proximity Switch · malfunctionedTAKE OFF TRIM AURAL WARNING.REPLACED DEFECTIVE ELEV. TRIM PROXIMITY SENSOR.SDR COMA0110132Light · brokenEMERGENCY LIGHT AT ROW 5 IS BROKEN.REPLACED LIGHT ASSY.SDR COMA0110131Proximity Switch · malfunctionedTAKE OFF TRIM AURAL WARNING. REPLACED DEFECTIVE ELEV. TRIM PROXIMITY SENSOR.SDR SWIA200110068Switch · failedON TAXI, FLAPS SELECTED 15 DEGREES. FLAP INDICATOR GOES FROM 15 DEGREES TO 0 DEGREES EVERY MINUTE. GREEN BARS DISAPPEAR WHEN FLAPS ARE AT 0 DEGREES. THEY REAPPEAR AT FLAP 15. NO MAP INDICATION, JUST ONE CHIME ALERT. AS WE TAXIED BACK, ADVANCED SWS/FLAP ONSDR SWIA200110067Warning System · activatedABORTED TAKEOFF - TRIPLE CHIME - AURAL WARNING - BRAKES, FLAPS, AUTO FEATHER OCCURRED DURING TAKEOFF ROLL. REPLACED AND SECURED AURAL WARNING UNIT. PERFORMED OPS CHECK OF AUTO FEATHER SYSTEM. OPS CHECK GOOD. SN ON 0419 SN OFF 0224.SDR SWIA200110045Window Post · crackedCRACK FOUND IN RIGHT POST BETWEEN DIRECT VIEW WINDOW AND WINDSHIELD.FABRICATED AND INSTALLED DOUBLER IAW SB120-053-0010/3-18-88.SDR SWIA200110066Control Unit · failedDURING CRUISE, ASWS & FLAP LIGHTS ON MAP & ASYMMETRY DISSAGREEMENT, CONTROL FAULT LIGHTS ON OVERHEAD. PANEL FLAP INDICATOR FLUCTUATING 0 DEGREES - 45 DEGREES SEVERAL TIMES INTERMITTENTLY. INSTALLED SERVICEABLE FCU. OPS CHECK GOOD.SDR SWIA200110019Flap Track · defectiveFLAP DISAGREEMENT AFTER TAKEOFF WHEN MOVING FLAPS FROM 15 DEGREES TO 0 DEGREES. APPEARS TO BE NACELLE FLAPS REPEATEDLY. PERFORMED FLAP INSPECTION AND FLAP TROUBLESHOOTING. REMOVED LEFT INBOARD FLAP. REPLACED ALL ROLLERS IAW 27-50-12 AND REPLACED OUTBOARD TSDR GLBA2001145Controller · failedPRESSURIZATION WOULD NOT REACH MAX DIFFERENTIAL. REPLACED ELECTRONIC CONTROLLER AND OUTFLOW VALVE, OPS CHECKED SYSTEM SATISFACTORY.SDR GLBA2001144Connector · looseWOULD NOT PRESSURIZE. INSPECTED FOUND LOOSE CONNECTION ON MANUAL CONTROL. SECURED CONNECTOR, OPS CHECKED SATISFACTORY.SDR SWIA20019996Brake Assy · failedNR 2 BRAKE LOCKED UPON LANDING. REPLACED NR 2 BRAKE ASSEMBLY, ALSO BRAKE CONTROL VALVE. AIRCRAFT RESTORED TO NORMAL. ALL CHECKS GOOD.SDR SWIA972661Valve · leakingDURING CLIMB OUT, DUCT LEAK LIGHT ILLUMINATED FOR RIGHT ENGINE. COMPLIED WITH QRH, NO CHANGE. CLOSED BLEEDS, ALSO THE PACKS. THE LIGHT DID NOT EXTINGUISH UNTIL POWER ON THE RIGHT ENGINE WAS PULLED TO FLIGHT IDLE. RETURNED TO MEDFORD. GAINED ACCESS TO ALL DUSDR GLBA2001138Outflow Valve · obstructedCABIN ALTITUDE CLIMBED WHILE AT ALTITUDE (26000) DEPLOYED MASKS. FOUND DEBRIS STUCK IN THE OUTFLOW VALVE. CLEAN VALVE, OPS CHECKED SATISFACTORY.SDR SWIA972664Terminal · failedRIGHT WINDSHIELD REPORTED NOT FUNCTIONING & BURN SMELL NOTED IN COCKPIT. FOUND BURNED POWER TERMINAL ON RIGHT WINDSHIELD. REMOVED AND REPLACED RIGHT WINDSHIELD PER MM 56-10-01. REMOVED & REPLACED POWER WIRE PER WM 30-41-00. WINDSHIELD HEAT OPS CHECK GOOD. SDR SWIA972663Receptacle · meltedON CLIMB OUT FROM EUGENE, NOTICED BURNING SMELL LIKE BURNING RUBBER IN FLIGHT DECK. SMELL CONTINUED, COULD NOT ISOLATE. NO VISABLE SMOKE. DIVERTED TO PDX. RAN AIRCRAFT FOR 30 MINUTES, COULD NOT DUPLICATE. FOUND FORWARD COFFEE POT ELECTRICAL RECEPTACLE MELTSDR SWIA972645Annunciator · failedON CLIMB OUT FLAP ASYMMETRY AND CONTROL FAULT. FLAP HANDLE WAS IN UP POSITION. ALL PAIRS SHOWED IN DOWN POSITION. COMMAND BAR SHOWED DOWN. RETURNED TO FIELD. REPLACED FLAP ANNUNCIATOR IAW MM 27-50-05. OPS CHECK GOOD ON GROUND. P/N: 306900-1005 S/N ON: SDR SWIA972643Indicator · failed''HIGH SPEED'' AURAL WARNING/TRIPLE CHIME SOUNDED ON TAKEOFF ROLL - IAS APPROXIMATELY 40 KNOTS. TAKEOFF ABORTED. REMOVED AND REPLACED PILOT'S AIRSPEED INDICATOR IAW MM 34-14-00 TO START HISTORY. COULD NOT DUPLICATE BEFORE REPLACEMENT. OPS AND LEAK CHECK GOO
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