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 ASOA02022Cover · missingFLT 4010 - DURING GROUND INSPECTION IN ATL, THE WHITE EMERGENCY EXIT SIGN BY SEAT 5C WAS MISSING THE PLASTIC COVER. MAINTENANCE REPLACED THE EMERGENCY EXIT SIGN COVER. AIRCRAFT OK FOR SERVICE. (M)SDR SWIA200210553Connector · burnedUPON DESCENT F/A'S GALLEY ELECTRICAL PANEL LOST LIGHTING, FUNCTIONING AND WAS HOT TO THE TOUCH. ALL 3 CREW MEMBERS SMELLED SMOKE, BUT NO VISUAL. FOUND CANNON PLUG ON COFFEE POT BURNED. REPLACED COFFEE POT, OPS CHECK GOOD.SDR SWIA200210677Web · crackedNACELLE WEB ON INBOARD RIGHT NACELLE CRACKED. INSTALLED NEW INBOARD FITTING AFT OF FRAME 13 AT NACELLE STATION 2425, SRM 51-10-02 AND 51-40-02.SDR SWIA200210676Clip · crackedFRAME 9 SKIN CLIP CRACKED ON COPILOT'S SIDE.SDR ASOA02016Battery · dischargedFLT 4084 - DURING GROUND INSPECTION IN ATL, THE EMERGENCY LIGHTING BATTERY WAS FOUND BE INOPERATIVE, CAUSING THE EMERGENCY FLOOR LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTING BATTERIES IN THE NR 2 AND NR 3 POSITIONS. OPERASDR SWIA200210536Cap · loosePRIOR TO LEVEL OFF AT FL230 CAPTAIN ATTITUDE INDICATOR AND HEADING DISPLAY TUMBLED AND WOULD MOMENTARILY RESET AND THEN TUMBLE AGAIN. FOUND FUSE CAP TO NR 1 AHC85 LOOSE. RECONNECTED CAP HEADING. CHECKS GOOD.SDR C2XA02IA011Control Panel · faultyIAH- DURING FLIGHT 4375, A TEST FLIGHT, THE CREW NOTED THAT THE FLAP ASYMMETRY LIGHT GLOWS THEN THE FLAPS FAIL. MAINTENANCE REMOVED AND REPLACED THE FLAP ANNUNCIATOR PANEL, PERFORMED A OPERATIONAL TEST OF THE FLAP SYSTEM, NO DEFECTS NOTED. A TEST FLIGHT WASSDR C2XA02IA010Actuator · failedIAH- DURING FLIGHT 4375, A TEST FLIGHT, THE CREW NOTED THAT THE FLAPS FAIL INFLIGHT, CONTROL FAULT WITH FLAPS AT ZERO DEGREES. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND INBOARD FLAP ACTUATOR, PERFORMED A OPERATIONAL CHECK OF THE FLAP SYSTEM, NO DEFECTSSDR C2XA02IA009Roller · damagedIAH- FLIGHT 3664DURING TAKEOFF THE CREW NOTED A FLAP CONTROL FAULT,AND, ABORTED THE TAKEOFF. IAH-MAINTENANCE INSPECTEDTHE FLAPS,AND, FOUND THE BEARING ON THE RIGHT INBOARD FLAP, INBOARD END TO BE DAMAGED. MAINTENANCE REMOVED and REOPLACEDTHE BEARING,PERFORMSDR C2XA02IA008Tank · odorIAH- AT THE GATE THE CREW NOTED THAT A GAS FUME SMELL IN THE CABIN WITH THE APU RUNNING. MAINTENANCE DRAINED THE APU EPA TANK, PERFORMED A OPERATIONAL CHECK OR THE APU, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA02IA003Battery · dischargedIAH- MAINTENANCE, WHILE PERFORMING A SERVICE CHECK THE MECHANIC NOTED THAT THE MIDDLE CABIN EMERGENCY LIGHTS FAILED TO ILLUMINATE. IAH- MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND MIDDLE EMERGENCY BATTERY PACK, PERFORMED A OPERATIONAL CHECK OF THE EMERGESDR SWIA200210563Deice System · malfunctionedLEFT OUTBOARD WING DEICE BOOT INOP LIGHT IN ICING CONDITIONS. RETURNED TO SFO. RE-CHECKED INFLATION OF LEFT AND RIGHT OUTBOARD WING BOOTS. FOUND GOOD. SWAPPED LEFT AND RIGHT OUTBOARD WING BOOT PRESSURE SWITCHES FOR TROUBLESHOOTING. RAN ENGINES. OPERATIONSDR SWIA200210534Computer · faultyCAPTAIN SIDE FLIGHT DIRECTOR FLAGGED AND F/O'S FLT DIRECTOR PITCHES +/- 10 DEGREES. REMOVED AND REPLACED CAPTAIN'S AHARS COMPUTER. S/N OFF: 422.SDR SWIA200210548Lock · frozenMAIN CABIN DOOR WILL NOT OPEN SMOOTHLY. FOUND UPPER DOOR CENTERING PLATES TOO TIGHT. ADJUSTED AND FOUND AFT OVER CENTER LOCK FROZEN. REMOVED AFT SHAFT, CLEANED AND LUBED, REINSTALLED SHAFT. OPS CHECK GOOD IAW 52-11-00.SDR SWIA200210530Hydraulic Line · leakingLOST GREEN HYD SYSTEM. LEFT MAIN HYD PUMP LOW PRESS LIGHT ILLUMINATED. PER QRH, TURNED LEFT ELEC HYD PUMP ON. AFTER A FEW MINUTES, GREEN HYD QUANTITY DROPPED TO ZERO (EMPTY). EXTENDED GEAR MANUALLY AND MADE EMER LANDING. PRESSURE LINE TO HYDRAULIC RESERVOSDR SWIA200210529Wire Harness · faultyRT NP GAUGE FLUCTUATES IN FLIGHT. REMOVED AND REPLACED RIGHT ENGINE EEC WIRING HARNESS. OPS CHECKS GOOD.SDR SWIA200210541Seal · looseUNUSUAL LOUD POPPING SOUND OVERHEAD. FOUND LOOSE PROSEAL ON TOP EDGE OF CAPTAIN'S WINDSHIELD. APPLIED SPEED TAPE.SDR SWIA200210556Actuator · faultyAT 220 KTS IAS HAND FLYING VMC NON-ICING CONDITION AIRCRAFT LEVELED NOSE DOWN, TRIM AT 2.0 (NO MORE TRIM DOWN). EXCESSIVE FORWARD PRESSURE TO HOLD LEVEL FLIGHT. ONLY WAY TO HOLD ALT WAS WITH POWER REDUCTION. AIRCRAFT COULD NOT BE FLOWN ABOVE 210 KTS. UPON SDR SWIA200210547Comparator · faultyDURING FLIGHT, ATT DISPLAY ON MAP CAME ON. A/P DISCONNECTED, GYRO AND COMPUTER FLAGS ON COPILOT'S ADI, HDG FLAG ON COPILOT'S HSI. AFTER A/P DISCONNECT FLAGS WENT AWAY, BUT DURING TURNS F/O'S ATT IND STAYED STRAIGHT AND LVL. F/O COMMAND BARS SHOW BELOW AIRPLSDR SWIA200210540Comparator · failedF/O ADI WON'T DISPLAY A/C ATT TURNING GAUGES GYRO, COMP AND HDG FLAGS. REPLACED NR 2 AHC85 WITH SERVICEABLE UNIT. OPS CHECK GOOD ON TAXI. S/N OFF: 2731.SDR SWIA200210525Skin · crackedCRACK IN SKIN AROUND FWD CORNER OF RT SIDE COCKPIT SIDE WINDOW. DISCOVERED DURING ROUTINE LINE INSPECTION. INSTALLED REPAIR DOUBLER PER SB 120-053-0010.SDR SWIA200210517Control Panel · faultyAFTER DEPARTURE, BOTH THE EHSI AND THE NAVIGATION SCREENS WENT BLANK ON THE FIRST OFFICER'S SIDE. REMOVED AND REPLACED CTL32 (NR 2). OPS CHECKS GOOD ON GROUND.SDR SWIA200210550Control Panel · faultyF/O'S COMMAND BARS STUCK AT 14 DEGREES AND A/P WILL NOT ENGAGE. DURING FLIGHT, ATTITUDE DISPLAY ON MAP, YELLOW PIT ON BOTH CAPTAIN'S AND FIRST OFFICER'S EADIS. FIRST OFFICERS DELTA SYMBOL DISPLAYED 5 DEGREES HIGHER THAN CAPTAIN'S. CAPTAIN'S DELTA SYMBOL DISSDR SWIA200210513Actuator · faultyWHILE IN CRUISE, FLAP AND ASYMMETRY AND CONTROL FAULT WARNINGS. POSITIVE ROLL TO THE RIGHT. OUTBOARD PAIR OF LIGHTS FLASHING. MEGGED-OUT ALL WIRES TO FCU. FOUND NO DISCREPANCIES. UPON RETRACTION TEST FOUND LEFT OUTBOARD FLAP ACTUATOR TO EXTEND AND THEN RESDR SWIA200210518Computer · faultyON TAKEOFF THE FIRST OFFICER'S EADI AND EHIS WENT OUT. SAME OCCURRED ON LANDING. REPLACED K0394, K0396 AND NR 2 DPU. RAN AIRCRAFT AND CYCLED AUXILLARY GENERATORS ON LINE SEVERAL TIMES. EFIS SYSTEMS OPERATIONAL CHECK GOOD IAW MM 34-23-00.SDR SWIA200210516Indicator · defectiveON TAKEOFF, AT ABOUT 60 KIAS, GOT AN AURAL WARNING - HIGH SPEED. ABORTED TAKEOFF. REPLACED CAPTAIN'S AIRSPEED INDICATOR PER EMB MM 34-12-01. OPS CHECKS GOOD.SDR SWIA200210504Wire · chafedNR 2 DET INOP PIPE ZONE LIGHT ILLUMINATED. FOUND CHAFED WIRE W110-1114-20 NEAR CONNECTOR J0946. REPLACED WIRE AS NEEDED. OPS CHECK GOOD.SDR SWIA200210503Fcu · faultyWHILE EN ROUTE GOT FLAP WARNING ASYMMETRY ASSOCIATED WITH CONTROL FAULT AND ADVANCED SWS. FLAP PAIR LIGHT BARS ON OUTBOARD PAIR SHOW ASYMMETRY WARNING, ONLY ONE LIGHT SEGMENT. THERE WERE NO CONTROL PROBLEMS OR ROLL TENDENCIES. PERFORMED SYSTEM SELF-DIAG TESSDR SWIA200210500Connector · looseAT BEGINNING OF TAKEOFF ROLL, NR 1 EEC FAILED. WHITE 'MAN' LIGHT, RED `EEC` LIGHT AND AURAL WARNING SOUNDED. ABORTED TAKEOFF. FOUND LOOSE CANNON PLUG TO 1.8 SENSOR. CLEANED, OHM'S CHECKED AND TIGHTENED CANNON PLUG. ALSO OHM'S CHECKED NH & NP SENSORS AND ESDR SWIA200210506Pressure Switch · faultyABORTED TAKEOFF DUE TO OIL WARNING (AURAL) AND NR 1 OIL LIGHT BLINKING ON. OIL LEVELS WERE SATISFACTORY DURING PREFLIGHT. ABORT INITIATED AT APPROXIMATELY 80 KTS. REPLACED NR 1 ENGINE LOW OIL PRESSURE SWITCH. OPS CHECK AND LEAK CHECK GOOD ON GROUND RUNUP. SDR SWIA200210498Sequence Valve · out of adjUPON GEAR RETRACTION LEFT MAIN GEAR DID NOT COME UP. RED A/B LIGHTS WITH RED B-LIGHT. CYCLED GEAR 3 TIMES. EACH TIME GEAR UP LIGHT INDICATION DID NOT CHANGE. RETURNED AND LANDED. ADJUSTED LT MLG O/B SEQUENCE VALVE CONTROL STOP. OPS CHECK GOOD.SDR SWIA200210497Fire Loop · faultyON CLIMBOUT THROUGH APPROXIMATELY 11,000 FT, RIGHT ENGINE PIPE ZONE DET INOP LIGHT ILLUMINATED STEADY FOR APPROXIMATELY 15 MINUTES; THEREAFTER, THE LIGHT REMAINED ILLUMINATED INTERMITTENTLY AFTER DESCENDING BELOW 11,000 FT AND STAYED INTERMITTENT UNTIL LANDINGSDR SWIA200210486Warning System · activatedHIGH SPEED AURAL WARNING SOUNDED ON TAKEOFF. PERFORMED PITOT STATIC CHECK IAW MM 34-12-00. HIGH SPEED WARNING SOUNDED AT CORRECT TIME. COULD NOT DUPLICATE. CHECKS GOOD AT THIS TIME.SDR SWIA200110512Annunciator · malfunctionedOUTBOARD FLAP DISAGREEMENT UPON FLAP RETRACTION IN THE AIR, RESET USING QRH. OPERATES NORMALLY ON THE GROUND. REMOVED AND REPLACED FLAP ANNUNCIATOR UNIT IAW MM 27-50-00. CLEARED FAULTS. OPS CHECK GOOD AT THIS TIME.SDR SWIA200110509Propeller · faultyON ROLLING TAKEOFF, TORQUE ON LEFT ENGINE SHOT UP TO 134 PERCENT TQ. TAKEOFF AURAL WARNING AUTO FEATHER SOUNDED WITH SWITCH ON. ABORTED TAKEOFF. WHEN POWER LEVERS PULLED BACK TO GROUND IDLE, RT ENGINE READ 75 PERCENT TQ AND 53 PERCENT NH. WHEN AUTO FEATHERSDR SWIA200110511Wire · out of positionROW SIX OVERHEAD RECESSED EMERGENCY LIGHTS ARE TOO DIM. BATTERY PACKS NEED TO BE REPLACED ON THAT CIRCUIT, NOT CHARGING. POSITIONED WIRES ON RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT TO CORRECT POSITION. OPS CHECK GOOD.SDR SWIA200110493Control Box · faultyLANDING GEAR HANGING UP FOR MORE THAN AFTER TAKEOFF. REMOVED AND REPLACED LANDING GEAR CONTROL RELAY BOX PER EMB120 MM 32-31-02. SWUNG GEAR. OPS CHECK GOOD.SDR SWIA200110514Stringer · crackedSTRINGER NR 8 CRACKED AT LEFT WING NR 2 FUEL PANEL. REPAIRED STRINGER CRACK IAW EMB SRM 57-20-03.SDR SWIA200110510Display · malfunctionedDESCENDING THROUGH 16,000 LOST CAPTAIN'S EHSI. NOTICED STRONG BURNING ODOR, SMOKE, WHICH CLEARED ALMOST IMMEDIATELY. NO CIRCUIT BREAKERS POPPED. REMOVED AND REPLACED CAPTAIN'S ELECTRONIC FLIGHT DISPLAY IAW EMB MM 34-22-03. OPS CHECK GOOD.SDR SWIA200110489Warning System · malfunctionedON DEPARTURE CLIMB, RIGHT PIPE ZONE DET INOP LIGHT ILLUMINATED AND STAYED ON STEADY FOR 8-10 MINUTES, THEN ILLUMINATED INTERMITTENTLY FOR DURATION OF FLIGHT. INSPECTED RIGHT PIPE FIRE DETECTION SYSTEM, COULD NOT DUPLICATE FAULT.SDR SWIA200110481Pin · defectiveAFTER TAKEOFF FLAPS WOULD NOT COMPLETELY RETRACT. A FLAP DISAGREEMENT RESULTED. DID QRH PROCEDURE, IT DID NOT CLEAR. RETURNED TO LAND. AFTER LANDING FLAPS RETURNED OK. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR CONNECTOR PIN. CYCLED FLAPS NUMEROUS TSDR SWIA200110480Smoke · detectedDUE TO REPORT OF SMOKE IN THE LAV AREA AND SMOKE DETECTOR GOING OFF CONTINUOUSLY FOR THREE MINUTES INFLIGHT, INSPECT CABIN FOR SOURCE OF SMOKE AND CORRECT ANY DISCREPANCIES. LAV SMOKE DETECTOR ALARM SOUNDED DURING CRUISE. F/A AND PAX SMELLED SMOKE. ALARM SSDR SWIA200110478Switch · out of adjFORWARD DOOR LIGHT CAME ON DURING TAKEOFF ROLL. ABORTED TAKEOFF. ADJUSTED FORWARD DOOR MICROSWITCH. OPS CHECK GOOD.SDR SWIA200110488Fuse · misinstalledCAPTAIN AHRS FAILED INFLIGHT (RED HDG/ATT FLAGS) AND F/O'S RMI FAILED AS WELL. FAILED AGAIN INFLIGHT. REPLACED AHRS COMPUTER. OPS CHECK GOOD. FOUND AHRS FUSE F0029 NOT PROPERLY INSTALLED. RESECURED FUSE CAP. OPS CHECK GOOD.SDR SWIA200110485Window · lack of lubeDIRECT VISION WINDOW ON LEFT PILOT SIDE DOES NOT LOCK PROPERLY. LUBED LOCK ASSEMBLY ON DV WINDOW. LOCKED DV WINDOW SYSTEM. OPS CHECK GOOD.SDR SWIA200110482Indicator · faultyHIGH SPEED AURAL WARNING ON TAKEOFF. ABORTED TAKEOFF. REMOVED AND REPLACED NR 1 AIRSPEED INDICATOR. OPS CHECK GOOD IAW 34-12-01.SDR SWIA200110484Fastener · looseABORTED 2 TAKEOFFS FOR FLICKERING DOOR LIGHT, NO CHIME. TAXIED BACK. ONE FASTENER ON FUEL DOOR WAS LOOSE. RESECURED FUEL PANEL DOORS AS NEEDED.SDR SWIA200110490Switch · out of adjAUTO FEATHER SYSTEM WOULD NOT ARM DURING TAKEOFF. TESTED OK ON FIRST FLIGHT OF THE DAY CHECKS. CLEANED BOTH 62 DEGREE MICRO SWITCHES AND ADJUSTED RIGHT SWITCH IAW MM 76-10-01. OPS CHECK GOOD.SDR SWIA200110475Actuator · failedDURING CRUISE (23000) ELEVATOR TRIM FAILURE OCCURRED WITH CORRESPONDING STRONG PITCH UP TENDENCY. TRIM CONTROL REGAINED ON DESCENT. REMOVED AND REPLACED LEFT AND RIGHT ELEVATOR TRIM ACTUATORS IAW EMB 27-32-02. LT P/N ON 5299-1, S/N OFF 606, RT P/N ON 5299-1SDR C2XA01IA421Connector · looseIAH- DURING A-CHECK, NOTED THAT THE EMERGENCY LIGHT IN TRACK OUT AT SEATS 2A THRU 5A. MAINTENANCE RESECURED THE CONNECTOR ON THE EMERGENCY BATTERY PACK NUMBER 2, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED AND THE AIRCRAF
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