Embraer EMB-120ER
Service difficulty reports · 8,287
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 = 'EMB120ER' 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 = 'EMB120ER' 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 ASOA03185Lamp · burned outDURING A GROUND INSPECTION IN ATL, THE RIGHT AFT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT AFT EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)SDR SWIA200311916Actuator · malfunctionedNACELLE FLAPS DROP SLIGHTLY (UNCOMMANDED). REPLACED LEFT NACELLE FLAP ACTUATOR WITH SERVICEABLE UNIT IAW MM 27-50-00. OPS CHECK GOOD. NO HYDRAULIC LEAKS NOTED. S/N OFF: 0187.SDR SWIA200312019Clip · crackedLEFT AND RIGHT FRAME 9 CLIPS CRACKED IN COCKPIT. FOUND DURING C-CHECK INSPECTION. COMPLIED WITH SB 120-53-0073.SDR SWIA200312018Skin · crackedCRACK ON SKIN SUPPORT LEFT SIDE OF COCKPIT BEHIND DV WINDOW. FOUND DURING C-CHECK INSPECTION. REPLACED SKIN SUPPORT LEFT SIDE OF COCKPIT AFT OF DV WINDOW PER MM 53-00-00 AND 51-00-00.SDR SWIA200312017Bracket · crackedBLUE HYDRAULIC SYSTEM PACK LOWER BRACKET CRACKED FOUND DURING C-CHECK INSPECTION. INSTALLED NEW LOWER SUPPORT BRACKET FOR BLUE SYSTEM HYDRAULIC PACK.SDR SWIA200312016Floorbeam · corrodedCORROSION ON FLOORBEAM IN LAVATORY AREA. FOUND DURING C-CHECK INSPECTION. REMOVED AND REPLACED BUTT STRAP WITH SERVICEABLE UNIT, LAV TO CARGO, RIGHT SIDE.SDR SWIA200312015Floorbeam · corrodedCORROSION ON LEFT INBOARD FLOORBEAM AND SEAT TRACK AT FORWARD END OF SEAT TRACK. FOUND DURING C-CHECK INSPECTION. REPAIRED CORROSION ON LEFT INBOARD FLOORBEAM AND SEAT TRACK AT FORWARD END OF SEAT TRACK. REPAIRED FLOORBEAM IAW SRM 53-00-03 AND REPAIRED SEATSDR SWIA200311918Plunger · out of adjustDURING TAKEOFF RIGHT MAIN LANDING GEAR WOULD NOT RETRACT. CYCLED GEAR DOWN AND RECEIVED ALL GEAR DOWN INDICATIONS. RETURNED TO LAX. ADJUSTED RIGHT GEAR DOOR PLUNGER. SWUNG GEAR NUMEROUS TIMES. OPS CHECKS GOOD.SDR SWIA200311917Controller · malfunctionedPAX 02 MASKS DEPLOYED IN FLIGHT CLIMBING THROUGH 8,000 FEET. NOTICED DELTA-P WAS AT 7,000 FT AND THE CABIN WAS LESS THAN ZERO. REMOVED AND REPLACED ALTITUDE CONTROLLER IAW MM 21-30-01. OPS CHECK GOOD, NO DEFECTS NOTED.SDR SWIA200311915Warning Light · illuminatedIN FLIGHT CLIMBING THROUGH 7,000 FEET, THE FLAP DISAGREEMENT LIGHT ILLUMINATED. COULD NOT CLEAR VIA QRH. RETURNED TO SLC. INSPECTED FLAPS. NO DEFECTS FOUND. PERFORMED FLAP FUNCTIONAL CHECKS IAW MM 27-50-00. OPERATIONAL CHECKS SATISFACTORY. NO DEFECTS NOSDR SWIA200312067Skin · crackedANGLE BEHIND CAPTAIN'S DV WINDOW CUTOUT CRACKED. DISCOVERED DURING C-CHECK. REPLACED BRACKET IAW SRM 120 51-10-02.SDR SWIA200312066Frame · crackedAT FRAME 13, BELOW FLOOR COCKPIT ENTRY DOOR, BOTH FRAME DOUBLERS CRACKED. DISCOVERED DURING C-CHECK. DOUBLERS APPLIED TO AREAS MENTIONED IAW SRM 120 51-10-02.SDR SWIA200312065Bracket · crackedRIGHT INBOARD LOWER FLAPWELL, INBOARD ROLLER BRACKET CRACKED. DISCOVERED DURING C-CHECK. REPLACED AFFECTED BRACKET IAW EMB120 SRM 51-10-02.SDR ASOA03179Light · inoperativeFLT 4132 - DURING A GROUND INSPECTION IN DFW, THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)SDR SWIA200311913Wire · brokenRED EMERGENCY LIGHTS ON FLOOR (BOTH) AT MAIN CABIN DOOR ARE INOP. REWIRED BROKEN WIRES ON FORWARD EMERGENCY RED LIGHTS ON THE FLOOR. OPS CHECKS GOOD.SDR GLBA2003051Pressure Switch · failedSMOKE IN CABIN, R&R PRESS SWITCH ON P2S OPS CHECK GOODSDR SWIA200311896Relay · malfunctionedDURING FLIGHT, RIGHT MAIN ''A'' GREEN LIGHT ILLUMINATED. GEAR WOULD NOT EXTEND - ALL THREE GEAR RED LIGHTS ILLUMINATED EXCEPT RIGHT ''A'' RED WITH HANDLE DOWN. AFTER 5 MINUTES THE PROBLEM FIXED ITSELF AND THE GEAR LOWERED NORMALLY. REPLACED LANDING GEAR RELSDR SWIA200311897Actuator · leakingUPON DEPLOYING FLAPS 15 DEGREES, FLAPS DISAGREEMENT LIGHT CAME ON, FOLLOWED BY LOW LEVEL LIGHT FOR RT/BLUE HYDRAULIC PUMP, LOW PRESS, MAIN PUMP LOW PRESS AND ELECTRIC PUMP LIGHT. UPON POSTFLIGHT, FOUND SIGNIFICANT FLUID LEAK. REMOVED AND REPLACED RIGHT NACSDR SWIA200311898Actuator · malfunctionedNACELLE FLAPS SLOW TO RESPOND WHEN FLAP HANDLE POSITIONED UP, AND WE GET A DISAGREEMENT ON THE FLAP ANNUNCIATOR PANEL. INSTALLED SERVICEABLE LEFT NACELLE FLAP ACTUATOR. OPS CHECKS GOOD/LEAK CHECKS GOOD. NO FURTHER FAULTS NOTED.SDR SWIA200311890Actuator · failedAFTER TAKEOFF, DISCOVERED WE HAD VERY LIMITED RIGHT RUDDER AUTHORITY. RIGHT RUDDER PEDAL WOULD ONLY DEPRESS ABOUT 1 1/2 INCHES. LEFT PEDAL TRAVEL NORMAL AND ALL COCKPIT INDICATIONS NORMAL. INSPECTED RUDDER FOR FREEDOM OF MOVEMENT, CHECKED GOOD. BLUE SYSTEMSDR SWIA200311887Actuator · malfunctionedCONTROL FAULT RECEIVED ON OUTBOARD FLAPS. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR IAW MM 27-53-01 AND 27-53-05. NO LEAKS NOTED. OPS CHECK GOOD.SDR SWIA200311878Ballast · burned outTHERE WAS AN ODOR OF SMOKE IN THE CARGO AREA AND IN THE AFT CABIN. THE SMOKE DETECTOR IN THE LAVATORY WENT OFF WHILE BOARDING PASSENGERS. INVESTIGATED AFT CABIN, FOUND LIGHT IN LAVATORY BALLAST BURNED OUT AND RELEASED SMOKE INTO AFT CABIN AND LAV. REPLACED SDR SWIA200311873Actuator · leakingON DEPARTURE OUT OF SLC HAD FLAP, ADVANCED SWS AND CONTROL FAULT LIGHTS FLASHING. PERFORMED QRH. DID NOT CLEAR THE PROBLEM. RETURNED TO SLC. FOUND LEFT NACELLE FLAP ACTUATOR LEAKING. INSTALLED NEW ACTUATOR IAW MM 27-50-00.SDR SWIA200311886Annunciator · malfunctionedBOTH OUTBOARD FLAPS FLUTTER UP TO 5 DEGREES WHEN IN THE 15 DEGREE AND 25 DEGREE POSITIONS. NO FAILURE INDICATED ON THE FLAP CONTROL PANEL. REPLACED FCU AND ANNUNCIATOR WITH VERSION II. OPS CHECK GOOD.SDR SWIA200311884Battery · malfunctionedEMERGENCY LIGHTS EXIT LIGHT ARE INOP ABOVE 5C AND 5A. REMOVED AND REPLACED NR 2 MID EMERGENCY LIGHT BATTERY PACK IAW MM 33-50-02. OPS CHECK GOOD.SDR SWIA200311875Structure · damagedSEVERAL LOOSE RIVETS FOUND ON UNDERSIDE OF RT NACELLE FLAP TRAILING EDGE. ALSO UNUSUAL LARGE DRAIN HOLE IN UNDERSIDE AT UPPER CORNER. FOUND DURING LINE INSPECTION. REMOVED AND REPLACED RIGHT NACELLE FLAP IAW MM 27-50-02.SDR SWIA200311874Light · inoperativeWIRES PULLED OUT OF EMERGENCY EXIT LIGHTS ON LEFT ROW. REPLACED AFT MOST EMERGENCY FLOOR LIGHT ASSEMBLY. OPS CHECK GOOD.SDR SWIA200311871Control Unit · malfunctionedFLAP CONTROL FAULT IN CRUISE. ONE SEGMENT NAC FLASHING, REST OK. FLAP CONTROL FAULT WHEN 25 DEGREES OF FLAPS SELECTED AT APPROXIMATELY 15 DEGREES OF FLAPS, REMAINDER OK. REMOVED AND REPLACED FLAP CONTROL UNIT IAW EMB120 MM 27-50-06. OPS CHECK GOOD.SDR SWIA200311893Servo · bindingRUDDER PEDALS MAKE A LOUD GRINDING NOISE WHEN THEY ARE MOVED. REMOVED RUDDER TO INSPECT. FOUND SERVO TO MAKE GRINDING NOISE AND ALSO FOUND IT TO BE BINDING. REPLACED SERVO WITH SERVICEABLE UNIT. AUTOPILOT OP CHECKS GOOD.SDR SWIA200311866Fuse · blownEMERGENCY LIGHTS AT ROW 6 DOOR, AND FLOOR LIGHTS BETWEEN ROW 3 AND 6, FOUND INOPERATIVE DURING F/A PREFLIGHT CHECKS. REPLACED ROW 6 EMERGENCY LIGHTS FUSE. OPS CHECK GOOD.SDR SWIA200311864Computer · malfunctionedON TAKEOFF ROLL AT 90 KTS (INTERMITTENTLY) AND LANDING ROLL TRIM FAIL ILLUMINATION ON MAP AND MASTER CAUTION SYSTEM. REMOVED FIRST OFFICER'S AUTOPILOT COMPUTER AND INSTALLED A SERVICEABLE UNIT. OPS CHECK GOOD.SDR SWIA200311858Landing Gear · malfunctionedLEFT MAIN LANDING GEAR INDICATION REMAINS RED ON RETRACTION AND SEEMS TO HANG. MAINTENANCE SWUNG GEAR APPROXIMATELY 20 TIMES. NO DEFECTS NOTED. PERFORMED MAIN AND NOSE LANDING GEAR EXTENSION/RETRACTION HYDRAULIC CIRCUIT TEST AS PER 32-32-00. OPS CHECK GOODSDR ASOA03129Stringer · crackedDURING AN 'A' CHECK IN TXK, THE RIGHT WING STRINGER NR 10 LOCATED CLOSE TO RIB NR 3 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RIGHT WING STRINGER NR 10 CLOSE TO RIB NR 3 IAW SRM 57-20-03. (M)SDR SWIA200311852Actuator · malfunctionedON DEPARTURE, RT MAIN GEAR DISAGREEMENT. A & B LIGHTS REMAIN ON AND RIGHT MAIN GEAR WOULD NOT RETRACT AS OBSERVED BY TOWER. RECYCLED THE GEAR 3 TIMES BEFORE RIGHT MAIN GEAR WOULD RETRACT. A & B DISAGREEMENT LIGHTS THEN EXTINGUISHED. RETURNED TO SLC. REPLASDR SWIA200311851Relay · malfunctionedAFTER TAKEOFF WITH AUTOPILOT SELECTED TO CAPTAIN'S SIDE, TRIM FAIL ILLUMINATED ON MAP MOMENTARILY, BUT THEN EXTINGUISHED. AUTOPILOT WAS ENGAGED; ON DESCENT PLANE PITCHED DOWN AND LIGHT CAME ON AGAIN. REPLACED TRIM PROXIMITY RELAY K0393. BOTH AUTOPILOT FLIGHSDR SWIA200311843Battery · malfunctionedEMERGENCY LIGHTS DO NOT ILLUMINATE DURING TEST. REMOVED AND REPLACED FORWARD EMERGENCY LIGHT BATTERY IAW EMB 120 MM 33-50-1.SDR SWIA200311850Computer · malfunctionedAUTOPILOT AND CAPTAIN'S FLIGHT DIRECTOR PITCHES UP AND DOWN 300 FT PRIOR TO LEVEL OFF. REPLACED AUTOPILOT COMPUTER APC-65B WITH SERVICEABLE UNIT. TESTED AND OPS CHECK GOOD.SDR SWIA200311835Fcu · malfunctionedFLAP CONTROL FAULT FOR INBOARD FLAPS UPON RETRACTING FLAPS AFTER LANDING. REMOVED AND REPLACED FLAP ANNUNCIATOR PANEL AND FCU FOR TROUBLESHOOTING. RAN FLAPS UP AND DOWN SEVERAL TIMES. OPS CHECK GOOD AT THIS TIME.SDR SWIA200311832Wire Harness · damagedAFTER TAKEOFF AND GEAR RETRACTION, RECEIVED GEAR INDICATIONS, LOUD NOISE AND VIBRATION FROM THE NOSE THAT INCREASED WITH AIRSPEED. RETURNED TO LAX. PERFORMED GEAR RETRACTION. FOUND THAT GEAR DOORS WOULD NOT CLOSE DUE TO A FAULTY NOSE GEAR A-HARNESS. REMOVESDR SWIA200311833Connector · damagedFLAP CONTROL FAULT INDICATED FOR INBOARD FLAPS. FLAPS WOULD NOT RETRACT ON THE GROUND. REMOVED AND REPLACED CONNECTOR FOR LEFT INBOARD FLAP ACTUATOR WITH A NEW PART. OPS CHECK OF FLAPS PERFORMED SATISFACTORY. P/N ON MS3476L12-10S.SDR SWIA200311829Servo · malfunctionedTHE AUTOPILOT PITCHES UP AND DOWN DURING CLIMBOUT AND IN LEVEL FLIGHT ON BOTH FLIGHT DIRECTORS. REPLACED ELEVATOR SERVO WITH SERVICEABLE UNIT. OPS CHECK GOOD.SDR SWIA200311828Bracket · crackedFOUND CRACK IN INBOARD RIGHT FLAP ROLLER BRACKET. INSTALLED NEW BRACKET AND ROLLER ASSEMBLY IAW 54-20-00. ALL CHECKS OK.SDR GLBA2003030Warning Light · illuminatedLANDING LT GREEN A LIGHT ILLUM AFTER RETRACTION. SWING GEAR 10 TIMES, CND INSP PROX SENSORS GAP, NO DEFECTS.SDR SWIA200311824Light · inoperativeFLOOR LEVEL EMERGENCY LIGHTS FORWARD OF ROW THREE INOP. REPLACED A BAD FUSE. OPS CHECK GOOD.SDR SWIA200311820Fcu · malfunctionedON TAXI OUT, UPON SELECTING FLAPS 15 RECEIVED A CONTROL FAULT. INSTALLED SERVICEABLE FLAP SELECTOR AND FLAP CONTROL UNIT. GROUND OPS CHECK GOOD. P/N: 120-64207-615, S/N OFF: 148978-304, S/N ON: 120237.SDR SWIA200311814Warning Horn · malfunctionedON TAKEOFF ROLL HAD A TRIPLE CHIME AND AUTO FEATHER AURAL WARNING WITH THE SWITCH IN THE ARMED POSITION AND THE ARMED LIGHT ON. ABORTED TAKEOFF. REMOVED AND REPLACED AURAL WARNING UNIT IAW 31-53-02. OPS CHECK GOOD.SDR SWIA200311817Wire · brokenCENTER EMERGENCY LIGHTS DO NOT TURN ON. FOUND BROKEN WIRE ON EMERGENCY LIGHT FLOOR TRACK. REPAIRED BROKEN WIRE IAW EMB120 WM 20-00-00. OPS CHECK GOOD.SDR ASOA03080Ejector Valve · inoperativeFLT 4910 - DURING TAKEOFF FROM DFW-ICT, THE NR 1 AND NR 2 LEADING EDGE DE-ICE TIMERS FAILED ON BOTH THE LEFT AND RIGHT OUTBOARD WING. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE AFT EJECTORSDR ASOA03072Seal · looseFLT 4955 - DURING CLIMB-OUT FROM DFW-AEX, AT APPROXIMATELY 25,000 FT CABIN PRESSURIZATION STARED TO CLIMB RAPIDLY. THE CREW MADE AN EMERGENCY DESCENT AND LEVELED OFF AT APPROXIMATELY 9,000 FEET. THE AIRCRAFT LANDED SAFELY IN AEX. S/D - MAINTENANCE RE-INSTALSDR SWIA200311822Warning Light · illuminatedEEC LEFT FAILURE ON TAKEOFF ROLL. ABORTED TAKEOFF. RAN VARIOUS EEC-RELATED TESTS, COULD NOT DUPLICATE DISCREPANCY. OPS CHECK GOOD AT THIS TIME. NO DEFECTS NOTED LEFT ENGINE.
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